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  • arp-msg-upd
  • arp-msg-upd-old
  • main
  • pymavlink-js
  • required-by-segs
  • required-by-segs-lyra
  • rig-refactor
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  • rust-rig-dev
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  • avn/swd/mavlink/mavlink-skyward-lib
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  • arp-msg-upd
  • arp-msg-upd-old
  • main
  • pymavlink-js
  • required-by-segs
  • required-by-segs-lyra
  • rig-refactor
  • rust
  • rust-fixed
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  • rust-rig-dev
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.gitignore
View file @ 7abedf97
......@@ -34,3 +34,7 @@
# ide folder & virtual environments
.venv/
.vscode
# rust specific
target
Cargo.lock
README.md
View file @ 7abedf97
# mavlink_skyward_lib
Repo containing Skyward's implementation of the Mavlink protocol:
* `message_definitions` - XML files describing the available messages
* `mavlink_lib ` - corresponding C header files, generated with `pymavlink`
* `mavlink_rust` - Rust library of the Mavlink protocol
generate.sh
View file @ 7abedf97
cd mavlink
python3 -m pymavlink.tools.mavgen --lang=C --wire-protocol=1.0 --output=../mavlink_lib ../message_definitions/gemini.xml
python3 -m pymavlink.tools.mavgen --lang=C --wire-protocol=1.0 --output=../mavlink_lib ../message_definitions/lyra.xml
python3 -m pymavlink.tools.mavgen --lang=Python --wire-protocol=1.0 --output=../mavlink_lib ../message_definitions/lyra.xml
\ No newline at end of file
mavlink_lib.py 0 → 100644
View file @ 7abedf97
Source diff could not be displayed: it is too large. Options to address this: view the blob.
mavlink_lib/gemini/gemini.h
View file @ 7abedf97
......@@ -11,7 +11,7 @@
#endif
#undef MAVLINK_THIS_XML_HASH
#define MAVLINK_THIS_XML_HASH 5773125515893874178
#define MAVLINK_THIS_XML_HASH 1902963619411886953
#ifdef __cplusplus
extern "C" {
......@@ -20,11 +20,11 @@ extern "C" {
// MESSAGE LENGTHS AND CRCS
#ifndef MAVLINK_MESSAGE_LENGTHS
#define MAVLINK_MESSAGE_LENGTHS {0, 8, 1, 1, 1, 1, 5, 1, 1, 4, 4, 12, 8, 2, 4, 8, 1, 5, 5, 7, 4, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 2, 2, 74, 64, 32, 44, 32, 32, 32, 32, 56, 21, 5, 19, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 32, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 14, 14, 46, 28, 27, 53, 77, 9, 171, 162, 92, 76, 39, 26, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0}
#define MAVLINK_MESSAGE_LENGTHS {0, 8, 1, 1, 1, 1, 5, 1, 1, 4, 4, 12, 8, 2, 4, 8, 1, 5, 5, 7, 4, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 2, 2, 74, 64, 32, 60, 32, 32, 32, 32, 56, 21, 5, 19, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 52, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 14, 14, 46, 28, 27, 53, 77, 29, 176, 163, 92, 76, 42, 35, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0}
#endif
#ifndef MAVLINK_MESSAGE_CRCS
#define MAVLINK_MESSAGE_CRCS {0, 136, 198, 165, 248, 184, 215, 160, 226, 113, 38, 71, 67, 218, 44, 81, 181, 110, 22, 65, 79, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 50, 146, 57, 72, 87, 223, 245, 212, 140, 148, 6, 155, 87, 255, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 109, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 183, 242, 142, 108, 133, 234, 66, 122, 141, 6, 245, 115, 74, 241, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0}
#define MAVLINK_MESSAGE_CRCS {0, 136, 198, 165, 248, 184, 215, 160, 226, 113, 38, 71, 67, 218, 44, 81, 181, 110, 22, 65, 79, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 50, 146, 57, 72, 87, 229, 245, 212, 140, 148, 6, 155, 87, 255, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 117, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 183, 242, 142, 108, 133, 234, 66, 11, 214, 84, 245, 115, 63, 79, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0}
#endif
#include "../protocol.h"
......@@ -34,6 +34,19 @@ extern "C" {
// ENUM DEFINITIONS
/** @brief Enum that lists all the system IDs of the various devices */
#ifndef HAVE_ENUM_SysIDs
#define HAVE_ENUM_SysIDs
typedef enum SysIDs
{
MAV_SYSID_MAIN=1, /* | */
MAV_SYSID_PAYLOAD=2, /* | */
MAV_SYSID_RIG=3, /* | */
MAV_SYSID_GS=4, /* | */
SysIDs_ENUM_END=5, /* | */
} SysIDs;
#endif
/** @brief Enum list for all the telemetries that can be requested */
#ifndef HAVE_ENUM_SystemTMList
#define HAVE_ENUM_SystemTMList
......@@ -47,13 +60,13 @@ typedef enum SystemTMList
MAV_TASK_STATS_ID=6, /* Task scheduler statistics answer: n mavlink messages where n is the number of tasks | */
MAV_ADA_ID=7, /* ADA Status | */
MAV_NAS_ID=8, /* NavigationSystem data | */
MAV_CAN_ID=9, /* Canbus stats | */
MAV_FLIGHT_ID=10, /* Flight telemetry | */
MAV_STATS_ID=11, /* Satistics telemetry | */
MAV_SENSORS_STATE_ID=12, /* Sensors init state telemetry | */
MAV_GSE_ID=13, /* Ground Segnement Equipment | */
MAV_MOTOR_ID=14, /* Rocket Motor data | */
MAV_TARS_ID=15, /* TARS data | */
MAV_MEA_ID=9, /* MEA Status | */
MAV_CAN_ID=10, /* Canbus stats | */
MAV_FLIGHT_ID=11, /* Flight telemetry | */
MAV_STATS_ID=12, /* Satistics telemetry | */
MAV_SENSORS_STATE_ID=13, /* Sensors init state telemetry | */
MAV_GSE_ID=14, /* Ground Segnement Equipment | */
MAV_MOTOR_ID=15, /* Rocket Motor data | */
SystemTMList_ENUM_END=16, /* | */
} SystemTMList;
#endif
......@@ -67,7 +80,7 @@ typedef enum SensorsTMList
MAV_BMX160_ID=2, /* BMX160 IMU data | */
MAV_VN100_ID=3, /* VN100 IMU data | */
MAV_MPU9250_ID=4, /* MPU9250 IMU data | */
MAV_ADS_ID=5, /* ADS 4 channel ADC data | */
MAV_ADS_ID=5, /* ADS 8 channel ADC data | */
MAV_MS5803_ID=6, /* MS5803 barometer data | */
MAV_BME280_ID=7, /* BME280 barometer data | */
MAV_CURRENT_SENSE_ID=8, /* Electrical current sensors data | */
......@@ -102,20 +115,21 @@ typedef enum MavCommandList
MAV_CMD_ARM=1, /* Command to arm the rocket | */
MAV_CMD_DISARM=2, /* Command to disarm the rocket | */
MAV_CMD_CALIBRATE=3, /* Command to trigger the calibration | */
MAV_CMD_FORCE_INIT=4, /* Command to init the rocket | */
MAV_CMD_FORCE_LAUNCH=5, /* Command to force the launch state on the rocket | */
MAV_CMD_FORCE_LANDING=6, /* Command to communicate the end of the mission and close the file descriptors in the SD card | */
MAV_CMD_FORCE_APOGEE=7, /* Command to trigger the apogee event | */
MAV_CMD_FORCE_EXPULSION=8, /* Command to open the nosecone | */
MAV_CMD_FORCE_MAIN=9, /* Command to activate the thermal cutters and cut the drogue, activating both thermal cutters sequentially | */
MAV_CMD_START_LOGGING=10, /* Command to enable sensor logging | */
MAV_CMD_STOP_LOGGING=11, /* Command to permanently close the log file | */
MAV_CMD_FORCE_REBOOT=12, /* Command to reset the board from test status | */
MAV_CMD_ENTER_TEST_MODE=13, /* Command to enter the test mode | */
MAV_CMD_EXIT_TEST_MODE=14, /* Command to exit the test mode | */
MAV_CMD_START_RECORDING=15, /* Command to start the internal cameras recordings | */
MAV_CMD_STOP_RECORDING=16, /* Command to stop the internal cameras recordings | */
MavCommandList_ENUM_END=17, /* | */
MAV_CMD_SAVE_CALIBRATION=4, /* Command to save the current calibration into a file | */
MAV_CMD_FORCE_INIT=5, /* Command to init the rocket | */
MAV_CMD_FORCE_LAUNCH=6, /* Command to force the launch state on the rocket | */
MAV_CMD_FORCE_LANDING=7, /* Command to communicate the end of the mission and close the file descriptors in the SD card | */
MAV_CMD_FORCE_APOGEE=8, /* Command to trigger the apogee event | */
MAV_CMD_FORCE_EXPULSION=9, /* Command to open the nosecone | */
MAV_CMD_FORCE_DEPLOYMENT=10, /* Command to activate the thermal cutters and cut the drogue, activating both thermal cutters sequentially | */
MAV_CMD_START_LOGGING=11, /* Command to enable sensor logging | */
MAV_CMD_STOP_LOGGING=12, /* Command to permanently close the log file | */
MAV_CMD_FORCE_REBOOT=13, /* Command to reset the board from test status | */
MAV_CMD_ENTER_TEST_MODE=14, /* Command to enter the test mode | */
MAV_CMD_EXIT_TEST_MODE=15, /* Command to exit the test mode | */
MAV_CMD_START_RECORDING=16, /* Command to start the internal cameras recordings | */
MAV_CMD_STOP_RECORDING=17, /* Command to stop the internal cameras recordings | */
MavCommandList_ENUM_END=18, /* | */
} MavCommandList;
#endif
......@@ -145,7 +159,8 @@ typedef enum PinsList
LAUNCH_PIN=1, /* | */
NOSECONE_PIN=2, /* | */
DEPLOYMENT_PIN=3, /* | */
PinsList_ENUM_END=4, /* | */
QUICK_CONNECTOR_PIN=4, /* | */
PinsList_ENUM_END=5, /* | */
} PinsList;
#endif
......@@ -203,7 +218,7 @@ typedef enum PinsList
#include "./mavlink_msg_task_stats_tm.h"
#include "./mavlink_msg_ada_tm.h"
#include "./mavlink_msg_nas_tm.h"
#include "./mavlink_msg_tars_tm.h"
#include "./mavlink_msg_mea_tm.h"
#include "./mavlink_msg_rocket_flight_tm.h"
#include "./mavlink_msg_payload_flight_tm.h"
#include "./mavlink_msg_rocket_stats_tm.h"
......@@ -215,11 +230,11 @@ typedef enum PinsList
#undef MAVLINK_THIS_XML_HASH
#define MAVLINK_THIS_XML_HASH 5773125515893874178
#define MAVLINK_THIS_XML_HASH 1902963619411886953
#if MAVLINK_THIS_XML_HASH == MAVLINK_PRIMARY_XML_HASH
# define MAVLINK_MESSAGE_INFO {{"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_PING_TC, MAVLINK_MESSAGE_INFO_COMMAND_TC, MAVLINK_MESSAGE_INFO_SYSTEM_TM_REQUEST_TC, MAVLINK_MESSAGE_INFO_SENSOR_TM_REQUEST_TC, MAVLINK_MESSAGE_INFO_SERVO_TM_REQUEST_TC, MAVLINK_MESSAGE_INFO_SET_SERVO_ANGLE_TC, MAVLINK_MESSAGE_INFO_WIGGLE_SERVO_TC, MAVLINK_MESSAGE_INFO_RESET_SERVO_TC, MAVLINK_MESSAGE_INFO_SET_REFERENCE_ALTITUDE_TC, MAVLINK_MESSAGE_INFO_SET_REFERENCE_TEMPERATURE_TC, MAVLINK_MESSAGE_INFO_SET_ORIENTATION_TC, MAVLINK_MESSAGE_INFO_SET_COORDINATES_TC, MAVLINK_MESSAGE_INFO_RAW_EVENT_TC, MAVLINK_MESSAGE_INFO_SET_DEPLOYMENT_ALTITUDE_TC, MAVLINK_MESSAGE_INFO_SET_TARGET_COORDINATES_TC, MAVLINK_MESSAGE_INFO_SET_ALGORITHM_TC, MAVLINK_MESSAGE_INFO_SET_ATOMIC_VALVE_TIMING_TC, MAVLINK_MESSAGE_INFO_SET_VALVE_MAXIMUM_APERTURE_TC, MAVLINK_MESSAGE_INFO_CONRIG_STATE_TC, MAVLINK_MESSAGE_INFO_SET_IGNITION_TIME_TC, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_ACK_TM, MAVLINK_MESSAGE_INFO_NACK_TM, MAVLINK_MESSAGE_INFO_GPS_TM, MAVLINK_MESSAGE_INFO_IMU_TM, MAVLINK_MESSAGE_INFO_PRESSURE_TM, MAVLINK_MESSAGE_INFO_ADC_TM, MAVLINK_MESSAGE_INFO_VOLTAGE_TM, MAVLINK_MESSAGE_INFO_CURRENT_TM, MAVLINK_MESSAGE_INFO_TEMP_TM, MAVLINK_MESSAGE_INFO_LOAD_TM, MAVLINK_MESSAGE_INFO_ATTITUDE_TM, MAVLINK_MESSAGE_INFO_SENSOR_STATE_TM, MAVLINK_MESSAGE_INFO_SERVO_TM, MAVLINK_MESSAGE_INFO_PIN_TM, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_RECEIVER_TM, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_SYS_TM, MAVLINK_MESSAGE_INFO_FSM_TM, MAVLINK_MESSAGE_INFO_LOGGER_TM, MAVLINK_MESSAGE_INFO_MAVLINK_STATS_TM, MAVLINK_MESSAGE_INFO_TASK_STATS_TM, MAVLINK_MESSAGE_INFO_ADA_TM, MAVLINK_MESSAGE_INFO_NAS_TM, MAVLINK_MESSAGE_INFO_TARS_TM, MAVLINK_MESSAGE_INFO_ROCKET_FLIGHT_TM, MAVLINK_MESSAGE_INFO_PAYLOAD_FLIGHT_TM, MAVLINK_MESSAGE_INFO_ROCKET_STATS_TM, MAVLINK_MESSAGE_INFO_PAYLOAD_STATS_TM, MAVLINK_MESSAGE_INFO_GSE_TM, MAVLINK_MESSAGE_INFO_MOTOR_TM, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}}
# define MAVLINK_MESSAGE_NAMES {{ "ACK_TM", 100 }, { "ADA_TM", 205 }, { "ADC_TM", 105 }, { "ATTITUDE_TM", 110 }, { "COMMAND_TC", 2 }, { "CONRIG_STATE_TC", 19 }, { "CURRENT_TM", 107 }, { "FSM_TM", 201 }, { "GPS_TM", 102 }, { "GSE_TM", 212 }, { "IMU_TM", 103 }, { "LOAD_TM", 109 }, { "LOGGER_TM", 202 }, { "MAVLINK_STATS_TM", 203 }, { "MOTOR_TM", 213 }, { "NACK_TM", 101 }, { "NAS_TM", 206 }, { "PAYLOAD_FLIGHT_TM", 209 }, { "PAYLOAD_STATS_TM", 211 }, { "PING_TC", 1 }, { "PIN_TM", 113 }, { "PRESSURE_TM", 104 }, { "RAW_EVENT_TC", 13 }, { "RECEIVER_TM", 150 }, { "RESET_SERVO_TC", 8 }, { "ROCKET_FLIGHT_TM", 208 }, { "ROCKET_STATS_TM", 210 }, { "SENSOR_STATE_TM", 111 }, { "SENSOR_TM_REQUEST_TC", 4 }, { "SERVO_TM", 112 }, { "SERVO_TM_REQUEST_TC", 5 }, { "SET_ALGORITHM_TC", 16 }, { "SET_ATOMIC_VALVE_TIMING_TC", 17 }, { "SET_COORDINATES_TC", 12 }, { "SET_DEPLOYMENT_ALTITUDE_TC", 14 }, { "SET_IGNITION_TIME_TC", 20 }, { "SET_ORIENTATION_TC", 11 }, { "SET_REFERENCE_ALTITUDE_TC", 9 }, { "SET_REFERENCE_TEMPERATURE_TC", 10 }, { "SET_SERVO_ANGLE_TC", 6 }, { "SET_TARGET_COORDINATES_TC", 15 }, { "SET_VALVE_MAXIMUM_APERTURE_TC", 18 }, { "SYSTEM_TM_REQUEST_TC", 3 }, { "SYS_TM", 200 }, { "TARS_TM", 207 }, { "TASK_STATS_TM", 204 }, { "TEMP_TM", 108 }, { "VOLTAGE_TM", 106 }, { "WIGGLE_SERVO_TC", 7 }}
# define MAVLINK_MESSAGE_INFO {{"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_PING_TC, MAVLINK_MESSAGE_INFO_COMMAND_TC, MAVLINK_MESSAGE_INFO_SYSTEM_TM_REQUEST_TC, MAVLINK_MESSAGE_INFO_SENSOR_TM_REQUEST_TC, MAVLINK_MESSAGE_INFO_SERVO_TM_REQUEST_TC, MAVLINK_MESSAGE_INFO_SET_SERVO_ANGLE_TC, MAVLINK_MESSAGE_INFO_WIGGLE_SERVO_TC, MAVLINK_MESSAGE_INFO_RESET_SERVO_TC, MAVLINK_MESSAGE_INFO_SET_REFERENCE_ALTITUDE_TC, MAVLINK_MESSAGE_INFO_SET_REFERENCE_TEMPERATURE_TC, MAVLINK_MESSAGE_INFO_SET_ORIENTATION_TC, MAVLINK_MESSAGE_INFO_SET_COORDINATES_TC, MAVLINK_MESSAGE_INFO_RAW_EVENT_TC, MAVLINK_MESSAGE_INFO_SET_DEPLOYMENT_ALTITUDE_TC, MAVLINK_MESSAGE_INFO_SET_TARGET_COORDINATES_TC, MAVLINK_MESSAGE_INFO_SET_ALGORITHM_TC, MAVLINK_MESSAGE_INFO_SET_ATOMIC_VALVE_TIMING_TC, MAVLINK_MESSAGE_INFO_SET_VALVE_MAXIMUM_APERTURE_TC, MAVLINK_MESSAGE_INFO_CONRIG_STATE_TC, MAVLINK_MESSAGE_INFO_SET_IGNITION_TIME_TC, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_ACK_TM, MAVLINK_MESSAGE_INFO_NACK_TM, MAVLINK_MESSAGE_INFO_GPS_TM, MAVLINK_MESSAGE_INFO_IMU_TM, MAVLINK_MESSAGE_INFO_PRESSURE_TM, MAVLINK_MESSAGE_INFO_ADC_TM, MAVLINK_MESSAGE_INFO_VOLTAGE_TM, MAVLINK_MESSAGE_INFO_CURRENT_TM, MAVLINK_MESSAGE_INFO_TEMP_TM, MAVLINK_MESSAGE_INFO_LOAD_TM, MAVLINK_MESSAGE_INFO_ATTITUDE_TM, MAVLINK_MESSAGE_INFO_SENSOR_STATE_TM, MAVLINK_MESSAGE_INFO_SERVO_TM, MAVLINK_MESSAGE_INFO_PIN_TM, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_RECEIVER_TM, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_SYS_TM, MAVLINK_MESSAGE_INFO_FSM_TM, MAVLINK_MESSAGE_INFO_LOGGER_TM, MAVLINK_MESSAGE_INFO_MAVLINK_STATS_TM, MAVLINK_MESSAGE_INFO_TASK_STATS_TM, MAVLINK_MESSAGE_INFO_ADA_TM, MAVLINK_MESSAGE_INFO_NAS_TM, MAVLINK_MESSAGE_INFO_MEA_TM, MAVLINK_MESSAGE_INFO_ROCKET_FLIGHT_TM, MAVLINK_MESSAGE_INFO_PAYLOAD_FLIGHT_TM, MAVLINK_MESSAGE_INFO_ROCKET_STATS_TM, MAVLINK_MESSAGE_INFO_PAYLOAD_STATS_TM, MAVLINK_MESSAGE_INFO_GSE_TM, MAVLINK_MESSAGE_INFO_MOTOR_TM, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}}
# define MAVLINK_MESSAGE_NAMES {{ "ACK_TM", 100 }, { "ADA_TM", 205 }, { "ADC_TM", 105 }, { "ATTITUDE_TM", 110 }, { "COMMAND_TC", 2 }, { "CONRIG_STATE_TC", 19 }, { "CURRENT_TM", 107 }, { "FSM_TM", 201 }, { "GPS_TM", 102 }, { "GSE_TM", 212 }, { "IMU_TM", 103 }, { "LOAD_TM", 109 }, { "LOGGER_TM", 202 }, { "MAVLINK_STATS_TM", 203 }, { "MEA_TM", 207 }, { "MOTOR_TM", 213 }, { "NACK_TM", 101 }, { "NAS_TM", 206 }, { "PAYLOAD_FLIGHT_TM", 209 }, { "PAYLOAD_STATS_TM", 211 }, { "PING_TC", 1 }, { "PIN_TM", 113 }, { "PRESSURE_TM", 104 }, { "RAW_EVENT_TC", 13 }, { "RECEIVER_TM", 150 }, { "RESET_SERVO_TC", 8 }, { "ROCKET_FLIGHT_TM", 208 }, { "ROCKET_STATS_TM", 210 }, { "SENSOR_STATE_TM", 111 }, { "SENSOR_TM_REQUEST_TC", 4 }, { "SERVO_TM", 112 }, { "SERVO_TM_REQUEST_TC", 5 }, { "SET_ALGORITHM_TC", 16 }, { "SET_ATOMIC_VALVE_TIMING_TC", 17 }, { "SET_COORDINATES_TC", 12 }, { "SET_DEPLOYMENT_ALTITUDE_TC", 14 }, { "SET_IGNITION_TIME_TC", 20 }, { "SET_ORIENTATION_TC", 11 }, { "SET_REFERENCE_ALTITUDE_TC", 9 }, { "SET_REFERENCE_TEMPERATURE_TC", 10 }, { "SET_SERVO_ANGLE_TC", 6 }, { "SET_TARGET_COORDINATES_TC", 15 }, { "SET_VALVE_MAXIMUM_APERTURE_TC", 18 }, { "SYSTEM_TM_REQUEST_TC", 3 }, { "SYS_TM", 200 }, { "TASK_STATS_TM", 204 }, { "TEMP_TM", 108 }, { "VOLTAGE_TM", 106 }, { "WIGGLE_SERVO_TC", 7 }}
# if MAVLINK_COMMAND_24BIT
# include "../mavlink_get_info.h"
# endif
......
mavlink_lib/gemini/mavlink.h
View file @ 7abedf97
......@@ -6,7 +6,7 @@
#ifndef MAVLINK_H
#define MAVLINK_H
#define MAVLINK_PRIMARY_XML_HASH 5773125515893874178
#define MAVLINK_PRIMARY_XML_HASH 1902963619411886953
#ifndef MAVLINK_STX
#define MAVLINK_STX 254
......
mavlink_lib/gemini/mavlink_msg_adc_tm.h
View file @ 7abedf97
......@@ -10,16 +10,20 @@ typedef struct __mavlink_adc_tm_t {
float channel_1; /*< [V] ADC voltage measured on channel 1*/
float channel_2; /*< [V] ADC voltage measured on channel 2*/
float channel_3; /*< [V] ADC voltage measured on channel 3*/
float channel_4; /*< [V] ADC voltage measured on channel 4*/
float channel_5; /*< [V] ADC voltage measured on channel 5*/
float channel_6; /*< [V] ADC voltage measured on channel 6*/
float channel_7; /*< [V] ADC voltage measured on channel 7*/
char sensor_name[20]; /*< Sensor name*/
} mavlink_adc_tm_t;
#define MAVLINK_MSG_ID_ADC_TM_LEN 44
#define MAVLINK_MSG_ID_ADC_TM_MIN_LEN 44
#define MAVLINK_MSG_ID_105_LEN 44
#define MAVLINK_MSG_ID_105_MIN_LEN 44
#define MAVLINK_MSG_ID_ADC_TM_LEN 60
#define MAVLINK_MSG_ID_ADC_TM_MIN_LEN 60
#define MAVLINK_MSG_ID_105_LEN 60
#define MAVLINK_MSG_ID_105_MIN_LEN 60
#define MAVLINK_MSG_ID_ADC_TM_CRC 223
#define MAVLINK_MSG_ID_105_CRC 223
#define MAVLINK_MSG_ID_ADC_TM_CRC 229
#define MAVLINK_MSG_ID_105_CRC 229
#define MAVLINK_MSG_ADC_TM_FIELD_SENSOR_NAME_LEN 20
......@@ -27,25 +31,33 @@ typedef struct __mavlink_adc_tm_t {
#define MAVLINK_MESSAGE_INFO_ADC_TM { \
105, \
"ADC_TM", \
6, \
10, \
{ { "timestamp", NULL, MAVLINK_TYPE_UINT64_T, 0, 0, offsetof(mavlink_adc_tm_t, timestamp) }, \
{ "sensor_name", NULL, MAVLINK_TYPE_CHAR, 20, 24, offsetof(mavlink_adc_tm_t, sensor_name) }, \
{ "sensor_name", NULL, MAVLINK_TYPE_CHAR, 20, 40, offsetof(mavlink_adc_tm_t, sensor_name) }, \
{ "channel_0", NULL, MAVLINK_TYPE_FLOAT, 0, 8, offsetof(mavlink_adc_tm_t, channel_0) }, \
{ "channel_1", NULL, MAVLINK_TYPE_FLOAT, 0, 12, offsetof(mavlink_adc_tm_t, channel_1) }, \
{ "channel_2", NULL, MAVLINK_TYPE_FLOAT, 0, 16, offsetof(mavlink_adc_tm_t, channel_2) }, \
{ "channel_3", NULL, MAVLINK_TYPE_FLOAT, 0, 20, offsetof(mavlink_adc_tm_t, channel_3) }, \
{ "channel_4", NULL, MAVLINK_TYPE_FLOAT, 0, 24, offsetof(mavlink_adc_tm_t, channel_4) }, \
{ "channel_5", NULL, MAVLINK_TYPE_FLOAT, 0, 28, offsetof(mavlink_adc_tm_t, channel_5) }, \
{ "channel_6", NULL, MAVLINK_TYPE_FLOAT, 0, 32, offsetof(mavlink_adc_tm_t, channel_6) }, \
{ "channel_7", NULL, MAVLINK_TYPE_FLOAT, 0, 36, offsetof(mavlink_adc_tm_t, channel_7) }, \
} \
}
#else
#define MAVLINK_MESSAGE_INFO_ADC_TM { \
"ADC_TM", \
6, \
10, \
{ { "timestamp", NULL, MAVLINK_TYPE_UINT64_T, 0, 0, offsetof(mavlink_adc_tm_t, timestamp) }, \
{ "sensor_name", NULL, MAVLINK_TYPE_CHAR, 20, 24, offsetof(mavlink_adc_tm_t, sensor_name) }, \
{ "sensor_name", NULL, MAVLINK_TYPE_CHAR, 20, 40, offsetof(mavlink_adc_tm_t, sensor_name) }, \
{ "channel_0", NULL, MAVLINK_TYPE_FLOAT, 0, 8, offsetof(mavlink_adc_tm_t, channel_0) }, \
{ "channel_1", NULL, MAVLINK_TYPE_FLOAT, 0, 12, offsetof(mavlink_adc_tm_t, channel_1) }, \
{ "channel_2", NULL, MAVLINK_TYPE_FLOAT, 0, 16, offsetof(mavlink_adc_tm_t, channel_2) }, \
{ "channel_3", NULL, MAVLINK_TYPE_FLOAT, 0, 20, offsetof(mavlink_adc_tm_t, channel_3) }, \
{ "channel_4", NULL, MAVLINK_TYPE_FLOAT, 0, 24, offsetof(mavlink_adc_tm_t, channel_4) }, \
{ "channel_5", NULL, MAVLINK_TYPE_FLOAT, 0, 28, offsetof(mavlink_adc_tm_t, channel_5) }, \
{ "channel_6", NULL, MAVLINK_TYPE_FLOAT, 0, 32, offsetof(mavlink_adc_tm_t, channel_6) }, \
{ "channel_7", NULL, MAVLINK_TYPE_FLOAT, 0, 36, offsetof(mavlink_adc_tm_t, channel_7) }, \
} \
}
#endif
......@@ -62,10 +74,14 @@ typedef struct __mavlink_adc_tm_t {
* @param channel_1 [V] ADC voltage measured on channel 1
* @param channel_2 [V] ADC voltage measured on channel 2
* @param channel_3 [V] ADC voltage measured on channel 3
* @param channel_4 [V] ADC voltage measured on channel 4
* @param channel_5 [V] ADC voltage measured on channel 5
* @param channel_6 [V] ADC voltage measured on channel 6
* @param channel_7 [V] ADC voltage measured on channel 7
* @return length of the message in bytes (excluding serial stream start sign)
*/
static inline uint16_t mavlink_msg_adc_tm_pack(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg,
uint64_t timestamp, const char *sensor_name, float channel_0, float channel_1, float channel_2, float channel_3)
uint64_t timestamp, const char *sensor_name, float channel_0, float channel_1, float channel_2, float channel_3, float channel_4, float channel_5, float channel_6, float channel_7)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char buf[MAVLINK_MSG_ID_ADC_TM_LEN];
......@@ -74,7 +90,11 @@ static inline uint16_t mavlink_msg_adc_tm_pack(uint8_t system_id, uint8_t compon
_mav_put_float(buf, 12, channel_1);
_mav_put_float(buf, 16, channel_2);
_mav_put_float(buf, 20, channel_3);
_mav_put_char_array(buf, 24, sensor_name, 20);
_mav_put_float(buf, 24, channel_4);
_mav_put_float(buf, 28, channel_5);
_mav_put_float(buf, 32, channel_6);
_mav_put_float(buf, 36, channel_7);
_mav_put_char_array(buf, 40, sensor_name, 20);
memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_ADC_TM_LEN);
#else
mavlink_adc_tm_t packet;
......@@ -83,6 +103,10 @@ static inline uint16_t mavlink_msg_adc_tm_pack(uint8_t system_id, uint8_t compon
packet.channel_1 = channel_1;
packet.channel_2 = channel_2;
packet.channel_3 = channel_3;
packet.channel_4 = channel_4;
packet.channel_5 = channel_5;
packet.channel_6 = channel_6;
packet.channel_7 = channel_7;
mav_array_memcpy(packet.sensor_name, sensor_name, sizeof(char)*20);
memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_ADC_TM_LEN);
#endif
......@@ -103,11 +127,15 @@ static inline uint16_t mavlink_msg_adc_tm_pack(uint8_t system_id, uint8_t compon
* @param channel_1 [V] ADC voltage measured on channel 1
* @param channel_2 [V] ADC voltage measured on channel 2
* @param channel_3 [V] ADC voltage measured on channel 3
* @param channel_4 [V] ADC voltage measured on channel 4
* @param channel_5 [V] ADC voltage measured on channel 5
* @param channel_6 [V] ADC voltage measured on channel 6
* @param channel_7 [V] ADC voltage measured on channel 7
* @return length of the message in bytes (excluding serial stream start sign)
*/
static inline uint16_t mavlink_msg_adc_tm_pack_chan(uint8_t system_id, uint8_t component_id, uint8_t chan,
mavlink_message_t* msg,
uint64_t timestamp,const char *sensor_name,float channel_0,float channel_1,float channel_2,float channel_3)
uint64_t timestamp,const char *sensor_name,float channel_0,float channel_1,float channel_2,float channel_3,float channel_4,float channel_5,float channel_6,float channel_7)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char buf[MAVLINK_MSG_ID_ADC_TM_LEN];
......@@ -116,7 +144,11 @@ static inline uint16_t mavlink_msg_adc_tm_pack_chan(uint8_t system_id, uint8_t c
_mav_put_float(buf, 12, channel_1);
_mav_put_float(buf, 16, channel_2);
_mav_put_float(buf, 20, channel_3);
_mav_put_char_array(buf, 24, sensor_name, 20);
_mav_put_float(buf, 24, channel_4);
_mav_put_float(buf, 28, channel_5);
_mav_put_float(buf, 32, channel_6);
_mav_put_float(buf, 36, channel_7);
_mav_put_char_array(buf, 40, sensor_name, 20);
memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_ADC_TM_LEN);
#else
mavlink_adc_tm_t packet;
......@@ -125,6 +157,10 @@ static inline uint16_t mavlink_msg_adc_tm_pack_chan(uint8_t system_id, uint8_t c
packet.channel_1 = channel_1;
packet.channel_2 = channel_2;
packet.channel_3 = channel_3;
packet.channel_4 = channel_4;
packet.channel_5 = channel_5;
packet.channel_6 = channel_6;
packet.channel_7 = channel_7;
mav_array_memcpy(packet.sensor_name, sensor_name, sizeof(char)*20);
memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_ADC_TM_LEN);
#endif
......@@ -143,7 +179,7 @@ static inline uint16_t mavlink_msg_adc_tm_pack_chan(uint8_t system_id, uint8_t c
*/
static inline uint16_t mavlink_msg_adc_tm_encode(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg, const mavlink_adc_tm_t* adc_tm)
{
return mavlink_msg_adc_tm_pack(system_id, component_id, msg, adc_tm->timestamp, adc_tm->sensor_name, adc_tm->channel_0, adc_tm->channel_1, adc_tm->channel_2, adc_tm->channel_3);
return mavlink_msg_adc_tm_pack(system_id, component_id, msg, adc_tm->timestamp, adc_tm->sensor_name, adc_tm->channel_0, adc_tm->channel_1, adc_tm->channel_2, adc_tm->channel_3, adc_tm->channel_4, adc_tm->channel_5, adc_tm->channel_6, adc_tm->channel_7);
}
/**
......@@ -157,7 +193,7 @@ static inline uint16_t mavlink_msg_adc_tm_encode(uint8_t system_id, uint8_t comp
*/
static inline uint16_t mavlink_msg_adc_tm_encode_chan(uint8_t system_id, uint8_t component_id, uint8_t chan, mavlink_message_t* msg, const mavlink_adc_tm_t* adc_tm)
{
return mavlink_msg_adc_tm_pack_chan(system_id, component_id, chan, msg, adc_tm->timestamp, adc_tm->sensor_name, adc_tm->channel_0, adc_tm->channel_1, adc_tm->channel_2, adc_tm->channel_3);
return mavlink_msg_adc_tm_pack_chan(system_id, component_id, chan, msg, adc_tm->timestamp, adc_tm->sensor_name, adc_tm->channel_0, adc_tm->channel_1, adc_tm->channel_2, adc_tm->channel_3, adc_tm->channel_4, adc_tm->channel_5, adc_tm->channel_6, adc_tm->channel_7);
}
/**
......@@ -170,10 +206,14 @@ static inline uint16_t mavlink_msg_adc_tm_encode_chan(uint8_t system_id, uint8_t
* @param channel_1 [V] ADC voltage measured on channel 1
* @param channel_2 [V] ADC voltage measured on channel 2
* @param channel_3 [V] ADC voltage measured on channel 3
* @param channel_4 [V] ADC voltage measured on channel 4
* @param channel_5 [V] ADC voltage measured on channel 5
* @param channel_6 [V] ADC voltage measured on channel 6
* @param channel_7 [V] ADC voltage measured on channel 7
*/
#ifdef MAVLINK_USE_CONVENIENCE_FUNCTIONS
static inline void mavlink_msg_adc_tm_send(mavlink_channel_t chan, uint64_t timestamp, const char *sensor_name, float channel_0, float channel_1, float channel_2, float channel_3)
static inline void mavlink_msg_adc_tm_send(mavlink_channel_t chan, uint64_t timestamp, const char *sensor_name, float channel_0, float channel_1, float channel_2, float channel_3, float channel_4, float channel_5, float channel_6, float channel_7)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char buf[MAVLINK_MSG_ID_ADC_TM_LEN];
......@@ -182,7 +222,11 @@ static inline void mavlink_msg_adc_tm_send(mavlink_channel_t chan, uint64_t time
_mav_put_float(buf, 12, channel_1);
_mav_put_float(buf, 16, channel_2);
_mav_put_float(buf, 20, channel_3);
_mav_put_char_array(buf, 24, sensor_name, 20);
_mav_put_float(buf, 24, channel_4);
_mav_put_float(buf, 28, channel_5);
_mav_put_float(buf, 32, channel_6);
_mav_put_float(buf, 36, channel_7);
_mav_put_char_array(buf, 40, sensor_name, 20);
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_ADC_TM, buf, MAVLINK_MSG_ID_ADC_TM_MIN_LEN, MAVLINK_MSG_ID_ADC_TM_LEN, MAVLINK_MSG_ID_ADC_TM_CRC);
#else
mavlink_adc_tm_t packet;
......@@ -191,6 +235,10 @@ static inline void mavlink_msg_adc_tm_send(mavlink_channel_t chan, uint64_t time
packet.channel_1 = channel_1;
packet.channel_2 = channel_2;
packet.channel_3 = channel_3;
packet.channel_4 = channel_4;
packet.channel_5 = channel_5;
packet.channel_6 = channel_6;
packet.channel_7 = channel_7;
mav_array_memcpy(packet.sensor_name, sensor_name, sizeof(char)*20);
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_ADC_TM, (const char *)&packet, MAVLINK_MSG_ID_ADC_TM_MIN_LEN, MAVLINK_MSG_ID_ADC_TM_LEN, MAVLINK_MSG_ID_ADC_TM_CRC);
#endif
......@@ -204,7 +252,7 @@ static inline void mavlink_msg_adc_tm_send(mavlink_channel_t chan, uint64_t time
static inline void mavlink_msg_adc_tm_send_struct(mavlink_channel_t chan, const mavlink_adc_tm_t* adc_tm)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
mavlink_msg_adc_tm_send(chan, adc_tm->timestamp, adc_tm->sensor_name, adc_tm->channel_0, adc_tm->channel_1, adc_tm->channel_2, adc_tm->channel_3);
mavlink_msg_adc_tm_send(chan, adc_tm->timestamp, adc_tm->sensor_name, adc_tm->channel_0, adc_tm->channel_1, adc_tm->channel_2, adc_tm->channel_3, adc_tm->channel_4, adc_tm->channel_5, adc_tm->channel_6, adc_tm->channel_7);
#else
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_ADC_TM, (const char *)adc_tm, MAVLINK_MSG_ID_ADC_TM_MIN_LEN, MAVLINK_MSG_ID_ADC_TM_LEN, MAVLINK_MSG_ID_ADC_TM_CRC);
#endif
......@@ -218,7 +266,7 @@ static inline void mavlink_msg_adc_tm_send_struct(mavlink_channel_t chan, const
is usually the receive buffer for the channel, and allows a reply to an
incoming message with minimum stack space usage.
*/
static inline void mavlink_msg_adc_tm_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint64_t timestamp, const char *sensor_name, float channel_0, float channel_1, float channel_2, float channel_3)
static inline void mavlink_msg_adc_tm_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint64_t timestamp, const char *sensor_name, float channel_0, float channel_1, float channel_2, float channel_3, float channel_4, float channel_5, float channel_6, float channel_7)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char *buf = (char *)msgbuf;
......@@ -227,7 +275,11 @@ static inline void mavlink_msg_adc_tm_send_buf(mavlink_message_t *msgbuf, mavlin
_mav_put_float(buf, 12, channel_1);
_mav_put_float(buf, 16, channel_2);
_mav_put_float(buf, 20, channel_3);
_mav_put_char_array(buf, 24, sensor_name, 20);
_mav_put_float(buf, 24, channel_4);
_mav_put_float(buf, 28, channel_5);
_mav_put_float(buf, 32, channel_6);
_mav_put_float(buf, 36, channel_7);
_mav_put_char_array(buf, 40, sensor_name, 20);
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_ADC_TM, buf, MAVLINK_MSG_ID_ADC_TM_MIN_LEN, MAVLINK_MSG_ID_ADC_TM_LEN, MAVLINK_MSG_ID_ADC_TM_CRC);
#else
mavlink_adc_tm_t *packet = (mavlink_adc_tm_t *)msgbuf;
......@@ -236,6 +288,10 @@ static inline void mavlink_msg_adc_tm_send_buf(mavlink_message_t *msgbuf, mavlin
packet->channel_1 = channel_1;
packet->channel_2 = channel_2;
packet->channel_3 = channel_3;
packet->channel_4 = channel_4;
packet->channel_5 = channel_5;
packet->channel_6 = channel_6;
packet->channel_7 = channel_7;
mav_array_memcpy(packet->sensor_name, sensor_name, sizeof(char)*20);
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_ADC_TM, (const char *)packet, MAVLINK_MSG_ID_ADC_TM_MIN_LEN, MAVLINK_MSG_ID_ADC_TM_LEN, MAVLINK_MSG_ID_ADC_TM_CRC);
#endif
......@@ -264,7 +320,7 @@ static inline uint64_t mavlink_msg_adc_tm_get_timestamp(const mavlink_message_t*
*/
static inline uint16_t mavlink_msg_adc_tm_get_sensor_name(const mavlink_message_t* msg, char *sensor_name)
{
return _MAV_RETURN_char_array(msg, sensor_name, 20, 24);
return _MAV_RETURN_char_array(msg, sensor_name, 20, 40);
}
/**
......@@ -307,6 +363,46 @@ static inline float mavlink_msg_adc_tm_get_channel_3(const mavlink_message_t* ms
return _MAV_RETURN_float(msg, 20);
}
/**
* @brief Get field channel_4 from adc_tm message
*
* @return [V] ADC voltage measured on channel 4
*/
static inline float mavlink_msg_adc_tm_get_channel_4(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 24);
}
/**
* @brief Get field channel_5 from adc_tm message
*
* @return [V] ADC voltage measured on channel 5
*/
static inline float mavlink_msg_adc_tm_get_channel_5(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 28);
}
/**
* @brief Get field channel_6 from adc_tm message
*
* @return [V] ADC voltage measured on channel 6
*/
static inline float mavlink_msg_adc_tm_get_channel_6(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 32);
}
/**
* @brief Get field channel_7 from adc_tm message
*
* @return [V] ADC voltage measured on channel 7
*/
static inline float mavlink_msg_adc_tm_get_channel_7(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 36);
}
/**
* @brief Decode a adc_tm message into a struct
*
......@@ -321,6 +417,10 @@ static inline void mavlink_msg_adc_tm_decode(const mavlink_message_t* msg, mavli
adc_tm->channel_1 = mavlink_msg_adc_tm_get_channel_1(msg);
adc_tm->channel_2 = mavlink_msg_adc_tm_get_channel_2(msg);
adc_tm->channel_3 = mavlink_msg_adc_tm_get_channel_3(msg);
adc_tm->channel_4 = mavlink_msg_adc_tm_get_channel_4(msg);
adc_tm->channel_5 = mavlink_msg_adc_tm_get_channel_5(msg);
adc_tm->channel_6 = mavlink_msg_adc_tm_get_channel_6(msg);
adc_tm->channel_7 = mavlink_msg_adc_tm_get_channel_7(msg);
mavlink_msg_adc_tm_get_sensor_name(msg, adc_tm->sensor_name);
#else
uint8_t len = msg->len < MAVLINK_MSG_ID_ADC_TM_LEN? msg->len : MAVLINK_MSG_ID_ADC_TM_LEN;
......
mavlink_lib/gemini/mavlink_msg_gse_tm.h
View file @ 7abedf97
......@@ -6,7 +6,7 @@
typedef struct __mavlink_gse_tm_t {
uint64_t timestamp; /*< [us] Timestamp in microseconds*/
float loadcell_tank; /*< [kg] Rocket weight*/
float loadcell_rocket; /*< [kg] Rocket weight*/
float loadcell_vessel; /*< [kg] External tank weight*/
float filling_pressure; /*< [Bar] Refueling line pressure*/
float vessel_pressure; /*< [Bar] Vessel tank pressure*/
......@@ -19,15 +19,18 @@ typedef struct __mavlink_gse_tm_t {
uint8_t main_valve_state; /*< 1 If the main valve is open */
uint8_t ignition_state; /*< 1 If the RIG is in ignition process*/
uint8_t tars_state; /*< 1 If the TARS algorithm is running*/
uint8_t main_board_status; /*< MAIN board status [0: not present, 1: online, 2: armed]*/
uint8_t payload_board_status; /*< PAYLOAD board status [0: not present, 1: online, 2: armed]*/
uint8_t motor_board_status; /*< MOTOR board status [0: not present, 1: online, 2: armed]*/
} mavlink_gse_tm_t;
#define MAVLINK_MSG_ID_GSE_TM_LEN 39
#define MAVLINK_MSG_ID_GSE_TM_MIN_LEN 39
#define MAVLINK_MSG_ID_212_LEN 39
#define MAVLINK_MSG_ID_212_MIN_LEN 39
#define MAVLINK_MSG_ID_GSE_TM_LEN 42
#define MAVLINK_MSG_ID_GSE_TM_MIN_LEN 42
#define MAVLINK_MSG_ID_212_LEN 42
#define MAVLINK_MSG_ID_212_MIN_LEN 42
#define MAVLINK_MSG_ID_GSE_TM_CRC 74
#define MAVLINK_MSG_ID_212_CRC 74
#define MAVLINK_MSG_ID_GSE_TM_CRC 63
#define MAVLINK_MSG_ID_212_CRC 63
......@@ -35,9 +38,9 @@ typedef struct __mavlink_gse_tm_t {
#define MAVLINK_MESSAGE_INFO_GSE_TM { \
212, \
"GSE_TM", \
14, \
17, \
{ { "timestamp", NULL, MAVLINK_TYPE_UINT64_T, 0, 0, offsetof(mavlink_gse_tm_t, timestamp) }, \
{ "loadcell_tank", NULL, MAVLINK_TYPE_FLOAT, 0, 8, offsetof(mavlink_gse_tm_t, loadcell_tank) }, \
{ "loadcell_rocket", NULL, MAVLINK_TYPE_FLOAT, 0, 8, offsetof(mavlink_gse_tm_t, loadcell_rocket) }, \
{ "loadcell_vessel", NULL, MAVLINK_TYPE_FLOAT, 0, 12, offsetof(mavlink_gse_tm_t, loadcell_vessel) }, \
{ "filling_pressure", NULL, MAVLINK_TYPE_FLOAT, 0, 16, offsetof(mavlink_gse_tm_t, filling_pressure) }, \
{ "vessel_pressure", NULL, MAVLINK_TYPE_FLOAT, 0, 20, offsetof(mavlink_gse_tm_t, vessel_pressure) }, \
......@@ -50,14 +53,17 @@ typedef struct __mavlink_gse_tm_t {
{ "tars_state", NULL, MAVLINK_TYPE_UINT8_T, 0, 38, offsetof(mavlink_gse_tm_t, tars_state) }, \
{ "battery_voltage", NULL, MAVLINK_TYPE_FLOAT, 0, 24, offsetof(mavlink_gse_tm_t, battery_voltage) }, \
{ "current_consumption", NULL, MAVLINK_TYPE_FLOAT, 0, 28, offsetof(mavlink_gse_tm_t, current_consumption) }, \
{ "main_board_status", NULL, MAVLINK_TYPE_UINT8_T, 0, 39, offsetof(mavlink_gse_tm_t, main_board_status) }, \
{ "payload_board_status", NULL, MAVLINK_TYPE_UINT8_T, 0, 40, offsetof(mavlink_gse_tm_t, payload_board_status) }, \
{ "motor_board_status", NULL, MAVLINK_TYPE_UINT8_T, 0, 41, offsetof(mavlink_gse_tm_t, motor_board_status) }, \
} \
}
#else
#define MAVLINK_MESSAGE_INFO_GSE_TM { \
"GSE_TM", \
14, \
17, \
{ { "timestamp", NULL, MAVLINK_TYPE_UINT64_T, 0, 0, offsetof(mavlink_gse_tm_t, timestamp) }, \
{ "loadcell_tank", NULL, MAVLINK_TYPE_FLOAT, 0, 8, offsetof(mavlink_gse_tm_t, loadcell_tank) }, \
{ "loadcell_rocket", NULL, MAVLINK_TYPE_FLOAT, 0, 8, offsetof(mavlink_gse_tm_t, loadcell_rocket) }, \
{ "loadcell_vessel", NULL, MAVLINK_TYPE_FLOAT, 0, 12, offsetof(mavlink_gse_tm_t, loadcell_vessel) }, \
{ "filling_pressure", NULL, MAVLINK_TYPE_FLOAT, 0, 16, offsetof(mavlink_gse_tm_t, filling_pressure) }, \
{ "vessel_pressure", NULL, MAVLINK_TYPE_FLOAT, 0, 20, offsetof(mavlink_gse_tm_t, vessel_pressure) }, \
......@@ -70,6 +76,9 @@ typedef struct __mavlink_gse_tm_t {
{ "tars_state", NULL, MAVLINK_TYPE_UINT8_T, 0, 38, offsetof(mavlink_gse_tm_t, tars_state) }, \
{ "battery_voltage", NULL, MAVLINK_TYPE_FLOAT, 0, 24, offsetof(mavlink_gse_tm_t, battery_voltage) }, \
{ "current_consumption", NULL, MAVLINK_TYPE_FLOAT, 0, 28, offsetof(mavlink_gse_tm_t, current_consumption) }, \
{ "main_board_status", NULL, MAVLINK_TYPE_UINT8_T, 0, 39, offsetof(mavlink_gse_tm_t, main_board_status) }, \
{ "payload_board_status", NULL, MAVLINK_TYPE_UINT8_T, 0, 40, offsetof(mavlink_gse_tm_t, payload_board_status) }, \
{ "motor_board_status", NULL, MAVLINK_TYPE_UINT8_T, 0, 41, offsetof(mavlink_gse_tm_t, motor_board_status) }, \
} \
}
#endif
......@@ -81,7 +90,7 @@ typedef struct __mavlink_gse_tm_t {
* @param msg The MAVLink message to compress the data into
*
* @param timestamp [us] Timestamp in microseconds
* @param loadcell_tank [kg] Rocket weight
* @param loadcell_rocket [kg] Rocket weight
* @param loadcell_vessel [kg] External tank weight
* @param filling_pressure [Bar] Refueling line pressure
* @param vessel_pressure [Bar] Vessel tank pressure
......@@ -94,15 +103,18 @@ typedef struct __mavlink_gse_tm_t {
* @param tars_state 1 If the TARS algorithm is running
* @param battery_voltage Battery voltage
* @param current_consumption RIG current
* @param main_board_status MAIN board status [0: not present, 1: online, 2: armed]
* @param payload_board_status PAYLOAD board status [0: not present, 1: online, 2: armed]
* @param motor_board_status MOTOR board status [0: not present, 1: online, 2: armed]
* @return length of the message in bytes (excluding serial stream start sign)
*/
static inline uint16_t mavlink_msg_gse_tm_pack(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg,
uint64_t timestamp, float loadcell_tank, float loadcell_vessel, float filling_pressure, float vessel_pressure, uint8_t arming_state, uint8_t filling_valve_state, uint8_t venting_valve_state, uint8_t release_valve_state, uint8_t main_valve_state, uint8_t ignition_state, uint8_t tars_state, float battery_voltage, float current_consumption)
uint64_t timestamp, float loadcell_rocket, float loadcell_vessel, float filling_pressure, float vessel_pressure, uint8_t arming_state, uint8_t filling_valve_state, uint8_t venting_valve_state, uint8_t release_valve_state, uint8_t main_valve_state, uint8_t ignition_state, uint8_t tars_state, float battery_voltage, float current_consumption, uint8_t main_board_status, uint8_t payload_board_status, uint8_t motor_board_status)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char buf[MAVLINK_MSG_ID_GSE_TM_LEN];
_mav_put_uint64_t(buf, 0, timestamp);
_mav_put_float(buf, 8, loadcell_tank);
_mav_put_float(buf, 8, loadcell_rocket);
_mav_put_float(buf, 12, loadcell_vessel);
_mav_put_float(buf, 16, filling_pressure);
_mav_put_float(buf, 20, vessel_pressure);
......@@ -115,12 +127,15 @@ static inline uint16_t mavlink_msg_gse_tm_pack(uint8_t system_id, uint8_t compon
_mav_put_uint8_t(buf, 36, main_valve_state);
_mav_put_uint8_t(buf, 37, ignition_state);
_mav_put_uint8_t(buf, 38, tars_state);
_mav_put_uint8_t(buf, 39, main_board_status);
_mav_put_uint8_t(buf, 40, payload_board_status);
_mav_put_uint8_t(buf, 41, motor_board_status);
memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_GSE_TM_LEN);
#else
mavlink_gse_tm_t packet;
packet.timestamp = timestamp;
packet.loadcell_tank = loadcell_tank;
packet.loadcell_rocket = loadcell_rocket;
packet.loadcell_vessel = loadcell_vessel;
packet.filling_pressure = filling_pressure;
packet.vessel_pressure = vessel_pressure;
......@@ -133,6 +148,9 @@ static inline uint16_t mavlink_msg_gse_tm_pack(uint8_t system_id, uint8_t compon
packet.main_valve_state = main_valve_state;
packet.ignition_state = ignition_state;
packet.tars_state = tars_state;
packet.main_board_status = main_board_status;
packet.payload_board_status = payload_board_status;
packet.motor_board_status = motor_board_status;
memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_GSE_TM_LEN);
#endif
......@@ -148,7 +166,7 @@ static inline uint16_t mavlink_msg_gse_tm_pack(uint8_t system_id, uint8_t compon
* @param chan The MAVLink channel this message will be sent over
* @param msg The MAVLink message to compress the data into
* @param timestamp [us] Timestamp in microseconds
* @param loadcell_tank [kg] Rocket weight
* @param loadcell_rocket [kg] Rocket weight
* @param loadcell_vessel [kg] External tank weight
* @param filling_pressure [Bar] Refueling line pressure
* @param vessel_pressure [Bar] Vessel tank pressure
......@@ -161,16 +179,19 @@ static inline uint16_t mavlink_msg_gse_tm_pack(uint8_t system_id, uint8_t compon
* @param tars_state 1 If the TARS algorithm is running
* @param battery_voltage Battery voltage
* @param current_consumption RIG current
* @param main_board_status MAIN board status [0: not present, 1: online, 2: armed]
* @param payload_board_status PAYLOAD board status [0: not present, 1: online, 2: armed]
* @param motor_board_status MOTOR board status [0: not present, 1: online, 2: armed]
* @return length of the message in bytes (excluding serial stream start sign)
*/
static inline uint16_t mavlink_msg_gse_tm_pack_chan(uint8_t system_id, uint8_t component_id, uint8_t chan,
mavlink_message_t* msg,
uint64_t timestamp,float loadcell_tank,float loadcell_vessel,float filling_pressure,float vessel_pressure,uint8_t arming_state,uint8_t filling_valve_state,uint8_t venting_valve_state,uint8_t release_valve_state,uint8_t main_valve_state,uint8_t ignition_state,uint8_t tars_state,float battery_voltage,float current_consumption)
uint64_t timestamp,float loadcell_rocket,float loadcell_vessel,float filling_pressure,float vessel_pressure,uint8_t arming_state,uint8_t filling_valve_state,uint8_t venting_valve_state,uint8_t release_valve_state,uint8_t main_valve_state,uint8_t ignition_state,uint8_t tars_state,float battery_voltage,float current_consumption,uint8_t main_board_status,uint8_t payload_board_status,uint8_t motor_board_status)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char buf[MAVLINK_MSG_ID_GSE_TM_LEN];
_mav_put_uint64_t(buf, 0, timestamp);
_mav_put_float(buf, 8, loadcell_tank);
_mav_put_float(buf, 8, loadcell_rocket);
_mav_put_float(buf, 12, loadcell_vessel);
_mav_put_float(buf, 16, filling_pressure);
_mav_put_float(buf, 20, vessel_pressure);
......@@ -183,12 +204,15 @@ static inline uint16_t mavlink_msg_gse_tm_pack_chan(uint8_t system_id, uint8_t c
_mav_put_uint8_t(buf, 36, main_valve_state);
_mav_put_uint8_t(buf, 37, ignition_state);
_mav_put_uint8_t(buf, 38, tars_state);
_mav_put_uint8_t(buf, 39, main_board_status);
_mav_put_uint8_t(buf, 40, payload_board_status);
_mav_put_uint8_t(buf, 41, motor_board_status);
memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_GSE_TM_LEN);
#else
mavlink_gse_tm_t packet;
packet.timestamp = timestamp;
packet.loadcell_tank = loadcell_tank;
packet.loadcell_rocket = loadcell_rocket;
packet.loadcell_vessel = loadcell_vessel;
packet.filling_pressure = filling_pressure;
packet.vessel_pressure = vessel_pressure;
......@@ -201,6 +225,9 @@ static inline uint16_t mavlink_msg_gse_tm_pack_chan(uint8_t system_id, uint8_t c
packet.main_valve_state = main_valve_state;
packet.ignition_state = ignition_state;
packet.tars_state = tars_state;
packet.main_board_status = main_board_status;
packet.payload_board_status = payload_board_status;
packet.motor_board_status = motor_board_status;
memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_GSE_TM_LEN);
#endif
......@@ -219,7 +246,7 @@ static inline uint16_t mavlink_msg_gse_tm_pack_chan(uint8_t system_id, uint8_t c
*/
static inline uint16_t mavlink_msg_gse_tm_encode(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg, const mavlink_gse_tm_t* gse_tm)
{
return mavlink_msg_gse_tm_pack(system_id, component_id, msg, gse_tm->timestamp, gse_tm->loadcell_tank, gse_tm->loadcell_vessel, gse_tm->filling_pressure, gse_tm->vessel_pressure, gse_tm->arming_state, gse_tm->filling_valve_state, gse_tm->venting_valve_state, gse_tm->release_valve_state, gse_tm->main_valve_state, gse_tm->ignition_state, gse_tm->tars_state, gse_tm->battery_voltage, gse_tm->current_consumption);
return mavlink_msg_gse_tm_pack(system_id, component_id, msg, gse_tm->timestamp, gse_tm->loadcell_rocket, gse_tm->loadcell_vessel, gse_tm->filling_pressure, gse_tm->vessel_pressure, gse_tm->arming_state, gse_tm->filling_valve_state, gse_tm->venting_valve_state, gse_tm->release_valve_state, gse_tm->main_valve_state, gse_tm->ignition_state, gse_tm->tars_state, gse_tm->battery_voltage, gse_tm->current_consumption, gse_tm->main_board_status, gse_tm->payload_board_status, gse_tm->motor_board_status);
}
/**
......@@ -233,7 +260,7 @@ static inline uint16_t mavlink_msg_gse_tm_encode(uint8_t system_id, uint8_t comp
*/
static inline uint16_t mavlink_msg_gse_tm_encode_chan(uint8_t system_id, uint8_t component_id, uint8_t chan, mavlink_message_t* msg, const mavlink_gse_tm_t* gse_tm)
{
return mavlink_msg_gse_tm_pack_chan(system_id, component_id, chan, msg, gse_tm->timestamp, gse_tm->loadcell_tank, gse_tm->loadcell_vessel, gse_tm->filling_pressure, gse_tm->vessel_pressure, gse_tm->arming_state, gse_tm->filling_valve_state, gse_tm->venting_valve_state, gse_tm->release_valve_state, gse_tm->main_valve_state, gse_tm->ignition_state, gse_tm->tars_state, gse_tm->battery_voltage, gse_tm->current_consumption);
return mavlink_msg_gse_tm_pack_chan(system_id, component_id, chan, msg, gse_tm->timestamp, gse_tm->loadcell_rocket, gse_tm->loadcell_vessel, gse_tm->filling_pressure, gse_tm->vessel_pressure, gse_tm->arming_state, gse_tm->filling_valve_state, gse_tm->venting_valve_state, gse_tm->release_valve_state, gse_tm->main_valve_state, gse_tm->ignition_state, gse_tm->tars_state, gse_tm->battery_voltage, gse_tm->current_consumption, gse_tm->main_board_status, gse_tm->payload_board_status, gse_tm->motor_board_status);
}
/**
......@@ -241,7 +268,7 @@ static inline uint16_t mavlink_msg_gse_tm_encode_chan(uint8_t system_id, uint8_t
* @param chan MAVLink channel to send the message
*
* @param timestamp [us] Timestamp in microseconds
* @param loadcell_tank [kg] Rocket weight
* @param loadcell_rocket [kg] Rocket weight
* @param loadcell_vessel [kg] External tank weight
* @param filling_pressure [Bar] Refueling line pressure
* @param vessel_pressure [Bar] Vessel tank pressure
......@@ -254,15 +281,18 @@ static inline uint16_t mavlink_msg_gse_tm_encode_chan(uint8_t system_id, uint8_t
* @param tars_state 1 If the TARS algorithm is running
* @param battery_voltage Battery voltage
* @param current_consumption RIG current
* @param main_board_status MAIN board status [0: not present, 1: online, 2: armed]
* @param payload_board_status PAYLOAD board status [0: not present, 1: online, 2: armed]
* @param motor_board_status MOTOR board status [0: not present, 1: online, 2: armed]
*/
#ifdef MAVLINK_USE_CONVENIENCE_FUNCTIONS
static inline void mavlink_msg_gse_tm_send(mavlink_channel_t chan, uint64_t timestamp, float loadcell_tank, float loadcell_vessel, float filling_pressure, float vessel_pressure, uint8_t arming_state, uint8_t filling_valve_state, uint8_t venting_valve_state, uint8_t release_valve_state, uint8_t main_valve_state, uint8_t ignition_state, uint8_t tars_state, float battery_voltage, float current_consumption)
static inline void mavlink_msg_gse_tm_send(mavlink_channel_t chan, uint64_t timestamp, float loadcell_rocket, float loadcell_vessel, float filling_pressure, float vessel_pressure, uint8_t arming_state, uint8_t filling_valve_state, uint8_t venting_valve_state, uint8_t release_valve_state, uint8_t main_valve_state, uint8_t ignition_state, uint8_t tars_state, float battery_voltage, float current_consumption, uint8_t main_board_status, uint8_t payload_board_status, uint8_t motor_board_status)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char buf[MAVLINK_MSG_ID_GSE_TM_LEN];
_mav_put_uint64_t(buf, 0, timestamp);
_mav_put_float(buf, 8, loadcell_tank);
_mav_put_float(buf, 8, loadcell_rocket);
_mav_put_float(buf, 12, loadcell_vessel);
_mav_put_float(buf, 16, filling_pressure);
_mav_put_float(buf, 20, vessel_pressure);
......@@ -275,12 +305,15 @@ static inline void mavlink_msg_gse_tm_send(mavlink_channel_t chan, uint64_t time
_mav_put_uint8_t(buf, 36, main_valve_state);
_mav_put_uint8_t(buf, 37, ignition_state);
_mav_put_uint8_t(buf, 38, tars_state);
_mav_put_uint8_t(buf, 39, main_board_status);
_mav_put_uint8_t(buf, 40, payload_board_status);
_mav_put_uint8_t(buf, 41, motor_board_status);
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_GSE_TM, buf, MAVLINK_MSG_ID_GSE_TM_MIN_LEN, MAVLINK_MSG_ID_GSE_TM_LEN, MAVLINK_MSG_ID_GSE_TM_CRC);
#else
mavlink_gse_tm_t packet;
packet.timestamp = timestamp;
packet.loadcell_tank = loadcell_tank;
packet.loadcell_rocket = loadcell_rocket;
packet.loadcell_vessel = loadcell_vessel;
packet.filling_pressure = filling_pressure;
packet.vessel_pressure = vessel_pressure;
......@@ -293,6 +326,9 @@ static inline void mavlink_msg_gse_tm_send(mavlink_channel_t chan, uint64_t time
packet.main_valve_state = main_valve_state;
packet.ignition_state = ignition_state;
packet.tars_state = tars_state;
packet.main_board_status = main_board_status;
packet.payload_board_status = payload_board_status;
packet.motor_board_status = motor_board_status;
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_GSE_TM, (const char *)&packet, MAVLINK_MSG_ID_GSE_TM_MIN_LEN, MAVLINK_MSG_ID_GSE_TM_LEN, MAVLINK_MSG_ID_GSE_TM_CRC);
#endif
......@@ -306,7 +342,7 @@ static inline void mavlink_msg_gse_tm_send(mavlink_channel_t chan, uint64_t time
static inline void mavlink_msg_gse_tm_send_struct(mavlink_channel_t chan, const mavlink_gse_tm_t* gse_tm)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
mavlink_msg_gse_tm_send(chan, gse_tm->timestamp, gse_tm->loadcell_tank, gse_tm->loadcell_vessel, gse_tm->filling_pressure, gse_tm->vessel_pressure, gse_tm->arming_state, gse_tm->filling_valve_state, gse_tm->venting_valve_state, gse_tm->release_valve_state, gse_tm->main_valve_state, gse_tm->ignition_state, gse_tm->tars_state, gse_tm->battery_voltage, gse_tm->current_consumption);
mavlink_msg_gse_tm_send(chan, gse_tm->timestamp, gse_tm->loadcell_rocket, gse_tm->loadcell_vessel, gse_tm->filling_pressure, gse_tm->vessel_pressure, gse_tm->arming_state, gse_tm->filling_valve_state, gse_tm->venting_valve_state, gse_tm->release_valve_state, gse_tm->main_valve_state, gse_tm->ignition_state, gse_tm->tars_state, gse_tm->battery_voltage, gse_tm->current_consumption, gse_tm->main_board_status, gse_tm->payload_board_status, gse_tm->motor_board_status);
#else
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_GSE_TM, (const char *)gse_tm, MAVLINK_MSG_ID_GSE_TM_MIN_LEN, MAVLINK_MSG_ID_GSE_TM_LEN, MAVLINK_MSG_ID_GSE_TM_CRC);
#endif
......@@ -320,12 +356,12 @@ static inline void mavlink_msg_gse_tm_send_struct(mavlink_channel_t chan, const
is usually the receive buffer for the channel, and allows a reply to an
incoming message with minimum stack space usage.
*/
static inline void mavlink_msg_gse_tm_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint64_t timestamp, float loadcell_tank, float loadcell_vessel, float filling_pressure, float vessel_pressure, uint8_t arming_state, uint8_t filling_valve_state, uint8_t venting_valve_state, uint8_t release_valve_state, uint8_t main_valve_state, uint8_t ignition_state, uint8_t tars_state, float battery_voltage, float current_consumption)
static inline void mavlink_msg_gse_tm_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint64_t timestamp, float loadcell_rocket, float loadcell_vessel, float filling_pressure, float vessel_pressure, uint8_t arming_state, uint8_t filling_valve_state, uint8_t venting_valve_state, uint8_t release_valve_state, uint8_t main_valve_state, uint8_t ignition_state, uint8_t tars_state, float battery_voltage, float current_consumption, uint8_t main_board_status, uint8_t payload_board_status, uint8_t motor_board_status)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char *buf = (char *)msgbuf;
_mav_put_uint64_t(buf, 0, timestamp);
_mav_put_float(buf, 8, loadcell_tank);
_mav_put_float(buf, 8, loadcell_rocket);
_mav_put_float(buf, 12, loadcell_vessel);
_mav_put_float(buf, 16, filling_pressure);
_mav_put_float(buf, 20, vessel_pressure);
......@@ -338,12 +374,15 @@ static inline void mavlink_msg_gse_tm_send_buf(mavlink_message_t *msgbuf, mavlin
_mav_put_uint8_t(buf, 36, main_valve_state);
_mav_put_uint8_t(buf, 37, ignition_state);
_mav_put_uint8_t(buf, 38, tars_state);
_mav_put_uint8_t(buf, 39, main_board_status);
_mav_put_uint8_t(buf, 40, payload_board_status);
_mav_put_uint8_t(buf, 41, motor_board_status);
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_GSE_TM, buf, MAVLINK_MSG_ID_GSE_TM_MIN_LEN, MAVLINK_MSG_ID_GSE_TM_LEN, MAVLINK_MSG_ID_GSE_TM_CRC);
#else
mavlink_gse_tm_t *packet = (mavlink_gse_tm_t *)msgbuf;
packet->timestamp = timestamp;
packet->loadcell_tank = loadcell_tank;
packet->loadcell_rocket = loadcell_rocket;
packet->loadcell_vessel = loadcell_vessel;
packet->filling_pressure = filling_pressure;
packet->vessel_pressure = vessel_pressure;
......@@ -356,6 +395,9 @@ static inline void mavlink_msg_gse_tm_send_buf(mavlink_message_t *msgbuf, mavlin
packet->main_valve_state = main_valve_state;
packet->ignition_state = ignition_state;
packet->tars_state = tars_state;
packet->main_board_status = main_board_status;
packet->payload_board_status = payload_board_status;
packet->motor_board_status = motor_board_status;
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_GSE_TM, (const char *)packet, MAVLINK_MSG_ID_GSE_TM_MIN_LEN, MAVLINK_MSG_ID_GSE_TM_LEN, MAVLINK_MSG_ID_GSE_TM_CRC);
#endif
......@@ -378,11 +420,11 @@ static inline uint64_t mavlink_msg_gse_tm_get_timestamp(const mavlink_message_t*
}
/**
* @brief Get field loadcell_tank from gse_tm message
* @brief Get field loadcell_rocket from gse_tm message
*
* @return [kg] Rocket weight
*/
static inline float mavlink_msg_gse_tm_get_loadcell_tank(const mavlink_message_t* msg)
static inline float mavlink_msg_gse_tm_get_loadcell_rocket(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 8);
}
......@@ -507,6 +549,36 @@ static inline float mavlink_msg_gse_tm_get_current_consumption(const mavlink_mes
return _MAV_RETURN_float(msg, 28);
}
/**
* @brief Get field main_board_status from gse_tm message
*
* @return MAIN board status [0: not present, 1: online, 2: armed]
*/
static inline uint8_t mavlink_msg_gse_tm_get_main_board_status(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint8_t(msg, 39);
}
/**
* @brief Get field payload_board_status from gse_tm message
*
* @return PAYLOAD board status [0: not present, 1: online, 2: armed]
*/
static inline uint8_t mavlink_msg_gse_tm_get_payload_board_status(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint8_t(msg, 40);
}
/**
* @brief Get field motor_board_status from gse_tm message
*
* @return MOTOR board status [0: not present, 1: online, 2: armed]
*/
static inline uint8_t mavlink_msg_gse_tm_get_motor_board_status(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint8_t(msg, 41);
}
/**
* @brief Decode a gse_tm message into a struct
*
......@@ -517,7 +589,7 @@ static inline void mavlink_msg_gse_tm_decode(const mavlink_message_t* msg, mavli
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
gse_tm->timestamp = mavlink_msg_gse_tm_get_timestamp(msg);
gse_tm->loadcell_tank = mavlink_msg_gse_tm_get_loadcell_tank(msg);
gse_tm->loadcell_rocket = mavlink_msg_gse_tm_get_loadcell_rocket(msg);
gse_tm->loadcell_vessel = mavlink_msg_gse_tm_get_loadcell_vessel(msg);
gse_tm->filling_pressure = mavlink_msg_gse_tm_get_filling_pressure(msg);
gse_tm->vessel_pressure = mavlink_msg_gse_tm_get_vessel_pressure(msg);
......@@ -530,6 +602,9 @@ static inline void mavlink_msg_gse_tm_decode(const mavlink_message_t* msg, mavli
gse_tm->main_valve_state = mavlink_msg_gse_tm_get_main_valve_state(msg);
gse_tm->ignition_state = mavlink_msg_gse_tm_get_ignition_state(msg);
gse_tm->tars_state = mavlink_msg_gse_tm_get_tars_state(msg);
gse_tm->main_board_status = mavlink_msg_gse_tm_get_main_board_status(msg);
gse_tm->payload_board_status = mavlink_msg_gse_tm_get_payload_board_status(msg);
gse_tm->motor_board_status = mavlink_msg_gse_tm_get_motor_board_status(msg);
#else
uint8_t len = msg->len < MAVLINK_MSG_ID_GSE_TM_LEN? msg->len : MAVLINK_MSG_ID_GSE_TM_LEN;
memset(gse_tm, 0, MAVLINK_MSG_ID_GSE_TM_LEN);
......
mavlink_lib/gemini/mavlink_msg_mea_tm.h 0 → 100644
View file @ 7abedf97
#pragma once
// MESSAGE MEA_TM PACKING
#define MAVLINK_MSG_ID_MEA_TM 207
typedef struct __mavlink_mea_tm_t {
uint64_t timestamp; /*< [us] When was this logged*/
float kalman_x0; /*< Kalman state variable 0 (corrected pressure)*/
float kalman_x1; /*< Kalman state variable 1 */
float kalman_x2; /*< Kalman state variable 2 (mass)*/
float mass; /*< [kg] Mass estimated*/
float corrected_pressure; /*< [kg] Corrected pressure*/
uint8_t state; /*< MEA current state*/
} mavlink_mea_tm_t;
#define MAVLINK_MSG_ID_MEA_TM_LEN 29
#define MAVLINK_MSG_ID_MEA_TM_MIN_LEN 29
#define MAVLINK_MSG_ID_207_LEN 29
#define MAVLINK_MSG_ID_207_MIN_LEN 29
#define MAVLINK_MSG_ID_MEA_TM_CRC 11
#define MAVLINK_MSG_ID_207_CRC 11
#if MAVLINK_COMMAND_24BIT
#define MAVLINK_MESSAGE_INFO_MEA_TM { \
207, \
"MEA_TM", \
7, \
{ { "timestamp", NULL, MAVLINK_TYPE_UINT64_T, 0, 0, offsetof(mavlink_mea_tm_t, timestamp) }, \
{ "state", NULL, MAVLINK_TYPE_UINT8_T, 0, 28, offsetof(mavlink_mea_tm_t, state) }, \
{ "kalman_x0", NULL, MAVLINK_TYPE_FLOAT, 0, 8, offsetof(mavlink_mea_tm_t, kalman_x0) }, \
{ "kalman_x1", NULL, MAVLINK_TYPE_FLOAT, 0, 12, offsetof(mavlink_mea_tm_t, kalman_x1) }, \
{ "kalman_x2", NULL, MAVLINK_TYPE_FLOAT, 0, 16, offsetof(mavlink_mea_tm_t, kalman_x2) }, \
{ "mass", NULL, MAVLINK_TYPE_FLOAT, 0, 20, offsetof(mavlink_mea_tm_t, mass) }, \
{ "corrected_pressure", NULL, MAVLINK_TYPE_FLOAT, 0, 24, offsetof(mavlink_mea_tm_t, corrected_pressure) }, \
} \
}
#else
#define MAVLINK_MESSAGE_INFO_MEA_TM { \
"MEA_TM", \
7, \
{ { "timestamp", NULL, MAVLINK_TYPE_UINT64_T, 0, 0, offsetof(mavlink_mea_tm_t, timestamp) }, \
{ "state", NULL, MAVLINK_TYPE_UINT8_T, 0, 28, offsetof(mavlink_mea_tm_t, state) }, \
{ "kalman_x0", NULL, MAVLINK_TYPE_FLOAT, 0, 8, offsetof(mavlink_mea_tm_t, kalman_x0) }, \
{ "kalman_x1", NULL, MAVLINK_TYPE_FLOAT, 0, 12, offsetof(mavlink_mea_tm_t, kalman_x1) }, \
{ "kalman_x2", NULL, MAVLINK_TYPE_FLOAT, 0, 16, offsetof(mavlink_mea_tm_t, kalman_x2) }, \
{ "mass", NULL, MAVLINK_TYPE_FLOAT, 0, 20, offsetof(mavlink_mea_tm_t, mass) }, \
{ "corrected_pressure", NULL, MAVLINK_TYPE_FLOAT, 0, 24, offsetof(mavlink_mea_tm_t, corrected_pressure) }, \
} \
}
#endif
/**
* @brief Pack a mea_tm message
* @param system_id ID of this system
* @param component_id ID of this component (e.g. 200 for IMU)
* @param msg The MAVLink message to compress the data into
*
* @param timestamp [us] When was this logged
* @param state MEA current state
* @param kalman_x0 Kalman state variable 0 (corrected pressure)
* @param kalman_x1 Kalman state variable 1
* @param kalman_x2 Kalman state variable 2 (mass)
* @param mass [kg] Mass estimated
* @param corrected_pressure [kg] Corrected pressure
* @return length of the message in bytes (excluding serial stream start sign)
*/
static inline uint16_t mavlink_msg_mea_tm_pack(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg,
uint64_t timestamp, uint8_t state, float kalman_x0, float kalman_x1, float kalman_x2, float mass, float corrected_pressure)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char buf[MAVLINK_MSG_ID_MEA_TM_LEN];
_mav_put_uint64_t(buf, 0, timestamp);
_mav_put_float(buf, 8, kalman_x0);
_mav_put_float(buf, 12, kalman_x1);
_mav_put_float(buf, 16, kalman_x2);
_mav_put_float(buf, 20, mass);
_mav_put_float(buf, 24, corrected_pressure);
_mav_put_uint8_t(buf, 28, state);
memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_MEA_TM_LEN);
#else
mavlink_mea_tm_t packet;
packet.timestamp = timestamp;
packet.kalman_x0 = kalman_x0;
packet.kalman_x1 = kalman_x1;
packet.kalman_x2 = kalman_x2;
packet.mass = mass;
packet.corrected_pressure = corrected_pressure;
packet.state = state;
memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_MEA_TM_LEN);
#endif
msg->msgid = MAVLINK_MSG_ID_MEA_TM;
return mavlink_finalize_message(msg, system_id, component_id, MAVLINK_MSG_ID_MEA_TM_MIN_LEN, MAVLINK_MSG_ID_MEA_TM_LEN, MAVLINK_MSG_ID_MEA_TM_CRC);
}
/**
* @brief Pack a mea_tm message on a channel
* @param system_id ID of this system
* @param component_id ID of this component (e.g. 200 for IMU)
* @param chan The MAVLink channel this message will be sent over
* @param msg The MAVLink message to compress the data into
* @param timestamp [us] When was this logged
* @param state MEA current state
* @param kalman_x0 Kalman state variable 0 (corrected pressure)
* @param kalman_x1 Kalman state variable 1
* @param kalman_x2 Kalman state variable 2 (mass)
* @param mass [kg] Mass estimated
* @param corrected_pressure [kg] Corrected pressure
* @return length of the message in bytes (excluding serial stream start sign)
*/
static inline uint16_t mavlink_msg_mea_tm_pack_chan(uint8_t system_id, uint8_t component_id, uint8_t chan,
mavlink_message_t* msg,
uint64_t timestamp,uint8_t state,float kalman_x0,float kalman_x1,float kalman_x2,float mass,float corrected_pressure)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char buf[MAVLINK_MSG_ID_MEA_TM_LEN];
_mav_put_uint64_t(buf, 0, timestamp);
_mav_put_float(buf, 8, kalman_x0);
_mav_put_float(buf, 12, kalman_x1);
_mav_put_float(buf, 16, kalman_x2);
_mav_put_float(buf, 20, mass);
_mav_put_float(buf, 24, corrected_pressure);
_mav_put_uint8_t(buf, 28, state);
memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_MEA_TM_LEN);
#else
mavlink_mea_tm_t packet;
packet.timestamp = timestamp;
packet.kalman_x0 = kalman_x0;
packet.kalman_x1 = kalman_x1;
packet.kalman_x2 = kalman_x2;
packet.mass = mass;
packet.corrected_pressure = corrected_pressure;
packet.state = state;
memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_MEA_TM_LEN);
#endif
msg->msgid = MAVLINK_MSG_ID_MEA_TM;
return mavlink_finalize_message_chan(msg, system_id, component_id, chan, MAVLINK_MSG_ID_MEA_TM_MIN_LEN, MAVLINK_MSG_ID_MEA_TM_LEN, MAVLINK_MSG_ID_MEA_TM_CRC);
}
/**
* @brief Encode a mea_tm struct
*
* @param system_id ID of this system
* @param component_id ID of this component (e.g. 200 for IMU)
* @param msg The MAVLink message to compress the data into
* @param mea_tm C-struct to read the message contents from
*/
static inline uint16_t mavlink_msg_mea_tm_encode(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg, const mavlink_mea_tm_t* mea_tm)
{
return mavlink_msg_mea_tm_pack(system_id, component_id, msg, mea_tm->timestamp, mea_tm->state, mea_tm->kalman_x0, mea_tm->kalman_x1, mea_tm->kalman_x2, mea_tm->mass, mea_tm->corrected_pressure);
}
/**
* @brief Encode a mea_tm struct on a channel
*
* @param system_id ID of this system
* @param component_id ID of this component (e.g. 200 for IMU)
* @param chan The MAVLink channel this message will be sent over
* @param msg The MAVLink message to compress the data into
* @param mea_tm C-struct to read the message contents from
*/
static inline uint16_t mavlink_msg_mea_tm_encode_chan(uint8_t system_id, uint8_t component_id, uint8_t chan, mavlink_message_t* msg, const mavlink_mea_tm_t* mea_tm)
{
return mavlink_msg_mea_tm_pack_chan(system_id, component_id, chan, msg, mea_tm->timestamp, mea_tm->state, mea_tm->kalman_x0, mea_tm->kalman_x1, mea_tm->kalman_x2, mea_tm->mass, mea_tm->corrected_pressure);
}
/**
* @brief Send a mea_tm message
* @param chan MAVLink channel to send the message
*
* @param timestamp [us] When was this logged
* @param state MEA current state
* @param kalman_x0 Kalman state variable 0 (corrected pressure)
* @param kalman_x1 Kalman state variable 1
* @param kalman_x2 Kalman state variable 2 (mass)
* @param mass [kg] Mass estimated
* @param corrected_pressure [kg] Corrected pressure
*/
#ifdef MAVLINK_USE_CONVENIENCE_FUNCTIONS
static inline void mavlink_msg_mea_tm_send(mavlink_channel_t chan, uint64_t timestamp, uint8_t state, float kalman_x0, float kalman_x1, float kalman_x2, float mass, float corrected_pressure)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char buf[MAVLINK_MSG_ID_MEA_TM_LEN];
_mav_put_uint64_t(buf, 0, timestamp);
_mav_put_float(buf, 8, kalman_x0);
_mav_put_float(buf, 12, kalman_x1);
_mav_put_float(buf, 16, kalman_x2);
_mav_put_float(buf, 20, mass);
_mav_put_float(buf, 24, corrected_pressure);
_mav_put_uint8_t(buf, 28, state);
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MEA_TM, buf, MAVLINK_MSG_ID_MEA_TM_MIN_LEN, MAVLINK_MSG_ID_MEA_TM_LEN, MAVLINK_MSG_ID_MEA_TM_CRC);
#else
mavlink_mea_tm_t packet;
packet.timestamp = timestamp;
packet.kalman_x0 = kalman_x0;
packet.kalman_x1 = kalman_x1;
packet.kalman_x2 = kalman_x2;
packet.mass = mass;
packet.corrected_pressure = corrected_pressure;
packet.state = state;
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MEA_TM, (const char *)&packet, MAVLINK_MSG_ID_MEA_TM_MIN_LEN, MAVLINK_MSG_ID_MEA_TM_LEN, MAVLINK_MSG_ID_MEA_TM_CRC);
#endif
}
/**
* @brief Send a mea_tm message
* @param chan MAVLink channel to send the message
* @param struct The MAVLink struct to serialize
*/
static inline void mavlink_msg_mea_tm_send_struct(mavlink_channel_t chan, const mavlink_mea_tm_t* mea_tm)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
mavlink_msg_mea_tm_send(chan, mea_tm->timestamp, mea_tm->state, mea_tm->kalman_x0, mea_tm->kalman_x1, mea_tm->kalman_x2, mea_tm->mass, mea_tm->corrected_pressure);
#else
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MEA_TM, (const char *)mea_tm, MAVLINK_MSG_ID_MEA_TM_MIN_LEN, MAVLINK_MSG_ID_MEA_TM_LEN, MAVLINK_MSG_ID_MEA_TM_CRC);
#endif
}
#if MAVLINK_MSG_ID_MEA_TM_LEN <= MAVLINK_MAX_PAYLOAD_LEN
/*
This variant of _send() can be used to save stack space by re-using
memory from the receive buffer. The caller provides a
mavlink_message_t which is the size of a full mavlink message. This
is usually the receive buffer for the channel, and allows a reply to an
incoming message with minimum stack space usage.
*/
static inline void mavlink_msg_mea_tm_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint64_t timestamp, uint8_t state, float kalman_x0, float kalman_x1, float kalman_x2, float mass, float corrected_pressure)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char *buf = (char *)msgbuf;
_mav_put_uint64_t(buf, 0, timestamp);
_mav_put_float(buf, 8, kalman_x0);
_mav_put_float(buf, 12, kalman_x1);
_mav_put_float(buf, 16, kalman_x2);
_mav_put_float(buf, 20, mass);
_mav_put_float(buf, 24, corrected_pressure);
_mav_put_uint8_t(buf, 28, state);
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MEA_TM, buf, MAVLINK_MSG_ID_MEA_TM_MIN_LEN, MAVLINK_MSG_ID_MEA_TM_LEN, MAVLINK_MSG_ID_MEA_TM_CRC);
#else
mavlink_mea_tm_t *packet = (mavlink_mea_tm_t *)msgbuf;
packet->timestamp = timestamp;
packet->kalman_x0 = kalman_x0;
packet->kalman_x1 = kalman_x1;
packet->kalman_x2 = kalman_x2;
packet->mass = mass;
packet->corrected_pressure = corrected_pressure;
packet->state = state;
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MEA_TM, (const char *)packet, MAVLINK_MSG_ID_MEA_TM_MIN_LEN, MAVLINK_MSG_ID_MEA_TM_LEN, MAVLINK_MSG_ID_MEA_TM_CRC);
#endif
}
#endif
#endif
// MESSAGE MEA_TM UNPACKING
/**
* @brief Get field timestamp from mea_tm message
*
* @return [us] When was this logged
*/
static inline uint64_t mavlink_msg_mea_tm_get_timestamp(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint64_t(msg, 0);
}
/**
* @brief Get field state from mea_tm message
*
* @return MEA current state
*/
static inline uint8_t mavlink_msg_mea_tm_get_state(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint8_t(msg, 28);
}
/**
* @brief Get field kalman_x0 from mea_tm message
*
* @return Kalman state variable 0 (corrected pressure)
*/
static inline float mavlink_msg_mea_tm_get_kalman_x0(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 8);
}
/**
* @brief Get field kalman_x1 from mea_tm message
*
* @return Kalman state variable 1
*/
static inline float mavlink_msg_mea_tm_get_kalman_x1(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 12);
}
/**
* @brief Get field kalman_x2 from mea_tm message
*
* @return Kalman state variable 2 (mass)
*/
static inline float mavlink_msg_mea_tm_get_kalman_x2(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 16);
}
/**
* @brief Get field mass from mea_tm message
*
* @return [kg] Mass estimated
*/
static inline float mavlink_msg_mea_tm_get_mass(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 20);
}
/**
* @brief Get field corrected_pressure from mea_tm message
*
* @return [kg] Corrected pressure
*/
static inline float mavlink_msg_mea_tm_get_corrected_pressure(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 24);
}
/**
* @brief Decode a mea_tm message into a struct
*
* @param msg The message to decode
* @param mea_tm C-struct to decode the message contents into
*/
static inline void mavlink_msg_mea_tm_decode(const mavlink_message_t* msg, mavlink_mea_tm_t* mea_tm)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
mea_tm->timestamp = mavlink_msg_mea_tm_get_timestamp(msg);
mea_tm->kalman_x0 = mavlink_msg_mea_tm_get_kalman_x0(msg);
mea_tm->kalman_x1 = mavlink_msg_mea_tm_get_kalman_x1(msg);
mea_tm->kalman_x2 = mavlink_msg_mea_tm_get_kalman_x2(msg);
mea_tm->mass = mavlink_msg_mea_tm_get_mass(msg);
mea_tm->corrected_pressure = mavlink_msg_mea_tm_get_corrected_pressure(msg);
mea_tm->state = mavlink_msg_mea_tm_get_state(msg);
#else
uint8_t len = msg->len < MAVLINK_MSG_ID_MEA_TM_LEN? msg->len : MAVLINK_MSG_ID_MEA_TM_LEN;
memset(mea_tm, 0, MAVLINK_MSG_ID_MEA_TM_LEN);
memcpy(mea_tm, _MAV_PAYLOAD(msg), len);
#endif
}
mavlink_lib/gemini/mavlink_msg_motor_tm.h
View file @ 7abedf97
......@@ -10,17 +10,20 @@ typedef struct __mavlink_motor_tm_t {
float bottom_tank_pressure; /*< [Bar] Tank bottom pressure*/
float combustion_chamber_pressure; /*< [Bar] Pressure inside the combustion chamber used for automatic shutdown*/
float tank_temperature; /*< Tank temperature*/
float battery_voltage; /*< [V] Battery voltage*/
float current_consumption; /*< [A] Current drained from the battery*/
uint8_t floating_level; /*< Floating level in tank*/
uint8_t main_valve_state; /*< 1 If the main valve is open */
uint8_t venting_valve_state; /*< 1 If the venting valve is open */
} mavlink_motor_tm_t;
#define MAVLINK_MSG_ID_MOTOR_TM_LEN 26
#define MAVLINK_MSG_ID_MOTOR_TM_MIN_LEN 26
#define MAVLINK_MSG_ID_213_LEN 26
#define MAVLINK_MSG_ID_213_MIN_LEN 26
#define MAVLINK_MSG_ID_MOTOR_TM_LEN 35
#define MAVLINK_MSG_ID_MOTOR_TM_MIN_LEN 35
#define MAVLINK_MSG_ID_213_LEN 35
#define MAVLINK_MSG_ID_213_MIN_LEN 35
#define MAVLINK_MSG_ID_MOTOR_TM_CRC 241
#define MAVLINK_MSG_ID_213_CRC 241
#define MAVLINK_MSG_ID_MOTOR_TM_CRC 79
#define MAVLINK_MSG_ID_213_CRC 79
......@@ -28,27 +31,33 @@ typedef struct __mavlink_motor_tm_t {
#define MAVLINK_MESSAGE_INFO_MOTOR_TM { \
213, \
"MOTOR_TM", \
7, \
10, \
{ { "timestamp", NULL, MAVLINK_TYPE_UINT64_T, 0, 0, offsetof(mavlink_motor_tm_t, timestamp) }, \
{ "top_tank_pressure", NULL, MAVLINK_TYPE_FLOAT, 0, 8, offsetof(mavlink_motor_tm_t, top_tank_pressure) }, \
{ "bottom_tank_pressure", NULL, MAVLINK_TYPE_FLOAT, 0, 12, offsetof(mavlink_motor_tm_t, bottom_tank_pressure) }, \
{ "combustion_chamber_pressure", NULL, MAVLINK_TYPE_FLOAT, 0, 16, offsetof(mavlink_motor_tm_t, combustion_chamber_pressure) }, \
{ "floating_level", NULL, MAVLINK_TYPE_UINT8_T, 0, 24, offsetof(mavlink_motor_tm_t, floating_level) }, \
{ "floating_level", NULL, MAVLINK_TYPE_UINT8_T, 0, 32, offsetof(mavlink_motor_tm_t, floating_level) }, \
{ "tank_temperature", NULL, MAVLINK_TYPE_FLOAT, 0, 20, offsetof(mavlink_motor_tm_t, tank_temperature) }, \
{ "main_valve_state", NULL, MAVLINK_TYPE_UINT8_T, 0, 25, offsetof(mavlink_motor_tm_t, main_valve_state) }, \
{ "main_valve_state", NULL, MAVLINK_TYPE_UINT8_T, 0, 33, offsetof(mavlink_motor_tm_t, main_valve_state) }, \
{ "venting_valve_state", NULL, MAVLINK_TYPE_UINT8_T, 0, 34, offsetof(mavlink_motor_tm_t, venting_valve_state) }, \
{ "battery_voltage", NULL, MAVLINK_TYPE_FLOAT, 0, 24, offsetof(mavlink_motor_tm_t, battery_voltage) }, \
{ "current_consumption", NULL, MAVLINK_TYPE_FLOAT, 0, 28, offsetof(mavlink_motor_tm_t, current_consumption) }, \
} \
}
#else
#define MAVLINK_MESSAGE_INFO_MOTOR_TM { \
"MOTOR_TM", \
7, \
10, \
{ { "timestamp", NULL, MAVLINK_TYPE_UINT64_T, 0, 0, offsetof(mavlink_motor_tm_t, timestamp) }, \
{ "top_tank_pressure", NULL, MAVLINK_TYPE_FLOAT, 0, 8, offsetof(mavlink_motor_tm_t, top_tank_pressure) }, \
{ "bottom_tank_pressure", NULL, MAVLINK_TYPE_FLOAT, 0, 12, offsetof(mavlink_motor_tm_t, bottom_tank_pressure) }, \
{ "combustion_chamber_pressure", NULL, MAVLINK_TYPE_FLOAT, 0, 16, offsetof(mavlink_motor_tm_t, combustion_chamber_pressure) }, \
{ "floating_level", NULL, MAVLINK_TYPE_UINT8_T, 0, 24, offsetof(mavlink_motor_tm_t, floating_level) }, \
{ "floating_level", NULL, MAVLINK_TYPE_UINT8_T, 0, 32, offsetof(mavlink_motor_tm_t, floating_level) }, \
{ "tank_temperature", NULL, MAVLINK_TYPE_FLOAT, 0, 20, offsetof(mavlink_motor_tm_t, tank_temperature) }, \
{ "main_valve_state", NULL, MAVLINK_TYPE_UINT8_T, 0, 25, offsetof(mavlink_motor_tm_t, main_valve_state) }, \
{ "main_valve_state", NULL, MAVLINK_TYPE_UINT8_T, 0, 33, offsetof(mavlink_motor_tm_t, main_valve_state) }, \
{ "venting_valve_state", NULL, MAVLINK_TYPE_UINT8_T, 0, 34, offsetof(mavlink_motor_tm_t, venting_valve_state) }, \
{ "battery_voltage", NULL, MAVLINK_TYPE_FLOAT, 0, 24, offsetof(mavlink_motor_tm_t, battery_voltage) }, \
{ "current_consumption", NULL, MAVLINK_TYPE_FLOAT, 0, 28, offsetof(mavlink_motor_tm_t, current_consumption) }, \
} \
}
#endif
......@@ -66,10 +75,13 @@ typedef struct __mavlink_motor_tm_t {
* @param floating_level Floating level in tank
* @param tank_temperature Tank temperature
* @param main_valve_state 1 If the main valve is open
* @param venting_valve_state 1 If the venting valve is open
* @param battery_voltage [V] Battery voltage
* @param current_consumption [A] Current drained from the battery
* @return length of the message in bytes (excluding serial stream start sign)
*/
static inline uint16_t mavlink_msg_motor_tm_pack(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg,
uint64_t timestamp, float top_tank_pressure, float bottom_tank_pressure, float combustion_chamber_pressure, uint8_t floating_level, float tank_temperature, uint8_t main_valve_state)
uint64_t timestamp, float top_tank_pressure, float bottom_tank_pressure, float combustion_chamber_pressure, uint8_t floating_level, float tank_temperature, uint8_t main_valve_state, uint8_t venting_valve_state, float battery_voltage, float current_consumption)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char buf[MAVLINK_MSG_ID_MOTOR_TM_LEN];
......@@ -78,8 +90,11 @@ static inline uint16_t mavlink_msg_motor_tm_pack(uint8_t system_id, uint8_t comp
_mav_put_float(buf, 12, bottom_tank_pressure);
_mav_put_float(buf, 16, combustion_chamber_pressure);
_mav_put_float(buf, 20, tank_temperature);
_mav_put_uint8_t(buf, 24, floating_level);
_mav_put_uint8_t(buf, 25, main_valve_state);
_mav_put_float(buf, 24, battery_voltage);
_mav_put_float(buf, 28, current_consumption);
_mav_put_uint8_t(buf, 32, floating_level);
_mav_put_uint8_t(buf, 33, main_valve_state);
_mav_put_uint8_t(buf, 34, venting_valve_state);
memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_MOTOR_TM_LEN);
#else
......@@ -89,8 +104,11 @@ static inline uint16_t mavlink_msg_motor_tm_pack(uint8_t system_id, uint8_t comp
packet.bottom_tank_pressure = bottom_tank_pressure;
packet.combustion_chamber_pressure = combustion_chamber_pressure;
packet.tank_temperature = tank_temperature;
packet.battery_voltage = battery_voltage;
packet.current_consumption = current_consumption;
packet.floating_level = floating_level;
packet.main_valve_state = main_valve_state;
packet.venting_valve_state = venting_valve_state;
memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_MOTOR_TM_LEN);
#endif
......@@ -112,11 +130,14 @@ static inline uint16_t mavlink_msg_motor_tm_pack(uint8_t system_id, uint8_t comp
* @param floating_level Floating level in tank
* @param tank_temperature Tank temperature
* @param main_valve_state 1 If the main valve is open
* @param venting_valve_state 1 If the venting valve is open
* @param battery_voltage [V] Battery voltage
* @param current_consumption [A] Current drained from the battery
* @return length of the message in bytes (excluding serial stream start sign)
*/
static inline uint16_t mavlink_msg_motor_tm_pack_chan(uint8_t system_id, uint8_t component_id, uint8_t chan,
mavlink_message_t* msg,
uint64_t timestamp,float top_tank_pressure,float bottom_tank_pressure,float combustion_chamber_pressure,uint8_t floating_level,float tank_temperature,uint8_t main_valve_state)
uint64_t timestamp,float top_tank_pressure,float bottom_tank_pressure,float combustion_chamber_pressure,uint8_t floating_level,float tank_temperature,uint8_t main_valve_state,uint8_t venting_valve_state,float battery_voltage,float current_consumption)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char buf[MAVLINK_MSG_ID_MOTOR_TM_LEN];
......@@ -125,8 +146,11 @@ static inline uint16_t mavlink_msg_motor_tm_pack_chan(uint8_t system_id, uint8_t
_mav_put_float(buf, 12, bottom_tank_pressure);
_mav_put_float(buf, 16, combustion_chamber_pressure);
_mav_put_float(buf, 20, tank_temperature);
_mav_put_uint8_t(buf, 24, floating_level);
_mav_put_uint8_t(buf, 25, main_valve_state);
_mav_put_float(buf, 24, battery_voltage);
_mav_put_float(buf, 28, current_consumption);
_mav_put_uint8_t(buf, 32, floating_level);
_mav_put_uint8_t(buf, 33, main_valve_state);
_mav_put_uint8_t(buf, 34, venting_valve_state);
memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_MOTOR_TM_LEN);
#else
......@@ -136,8 +160,11 @@ static inline uint16_t mavlink_msg_motor_tm_pack_chan(uint8_t system_id, uint8_t
packet.bottom_tank_pressure = bottom_tank_pressure;
packet.combustion_chamber_pressure = combustion_chamber_pressure;
packet.tank_temperature = tank_temperature;
packet.battery_voltage = battery_voltage;
packet.current_consumption = current_consumption;
packet.floating_level = floating_level;
packet.main_valve_state = main_valve_state;
packet.venting_valve_state = venting_valve_state;
memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_MOTOR_TM_LEN);
#endif
......@@ -156,7 +183,7 @@ static inline uint16_t mavlink_msg_motor_tm_pack_chan(uint8_t system_id, uint8_t
*/
static inline uint16_t mavlink_msg_motor_tm_encode(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg, const mavlink_motor_tm_t* motor_tm)
{
return mavlink_msg_motor_tm_pack(system_id, component_id, msg, motor_tm->timestamp, motor_tm->top_tank_pressure, motor_tm->bottom_tank_pressure, motor_tm->combustion_chamber_pressure, motor_tm->floating_level, motor_tm->tank_temperature, motor_tm->main_valve_state);
return mavlink_msg_motor_tm_pack(system_id, component_id, msg, motor_tm->timestamp, motor_tm->top_tank_pressure, motor_tm->bottom_tank_pressure, motor_tm->combustion_chamber_pressure, motor_tm->floating_level, motor_tm->tank_temperature, motor_tm->main_valve_state, motor_tm->venting_valve_state, motor_tm->battery_voltage, motor_tm->current_consumption);
}
/**
......@@ -170,7 +197,7 @@ static inline uint16_t mavlink_msg_motor_tm_encode(uint8_t system_id, uint8_t co
*/
static inline uint16_t mavlink_msg_motor_tm_encode_chan(uint8_t system_id, uint8_t component_id, uint8_t chan, mavlink_message_t* msg, const mavlink_motor_tm_t* motor_tm)
{
return mavlink_msg_motor_tm_pack_chan(system_id, component_id, chan, msg, motor_tm->timestamp, motor_tm->top_tank_pressure, motor_tm->bottom_tank_pressure, motor_tm->combustion_chamber_pressure, motor_tm->floating_level, motor_tm->tank_temperature, motor_tm->main_valve_state);
return mavlink_msg_motor_tm_pack_chan(system_id, component_id, chan, msg, motor_tm->timestamp, motor_tm->top_tank_pressure, motor_tm->bottom_tank_pressure, motor_tm->combustion_chamber_pressure, motor_tm->floating_level, motor_tm->tank_temperature, motor_tm->main_valve_state, motor_tm->venting_valve_state, motor_tm->battery_voltage, motor_tm->current_consumption);
}
/**
......@@ -184,10 +211,13 @@ static inline uint16_t mavlink_msg_motor_tm_encode_chan(uint8_t system_id, uint8
* @param floating_level Floating level in tank
* @param tank_temperature Tank temperature
* @param main_valve_state 1 If the main valve is open
* @param venting_valve_state 1 If the venting valve is open
* @param battery_voltage [V] Battery voltage
* @param current_consumption [A] Current drained from the battery
*/
#ifdef MAVLINK_USE_CONVENIENCE_FUNCTIONS
static inline void mavlink_msg_motor_tm_send(mavlink_channel_t chan, uint64_t timestamp, float top_tank_pressure, float bottom_tank_pressure, float combustion_chamber_pressure, uint8_t floating_level, float tank_temperature, uint8_t main_valve_state)
static inline void mavlink_msg_motor_tm_send(mavlink_channel_t chan, uint64_t timestamp, float top_tank_pressure, float bottom_tank_pressure, float combustion_chamber_pressure, uint8_t floating_level, float tank_temperature, uint8_t main_valve_state, uint8_t venting_valve_state, float battery_voltage, float current_consumption)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char buf[MAVLINK_MSG_ID_MOTOR_TM_LEN];
......@@ -196,8 +226,11 @@ static inline void mavlink_msg_motor_tm_send(mavlink_channel_t chan, uint64_t ti
_mav_put_float(buf, 12, bottom_tank_pressure);
_mav_put_float(buf, 16, combustion_chamber_pressure);
_mav_put_float(buf, 20, tank_temperature);
_mav_put_uint8_t(buf, 24, floating_level);
_mav_put_uint8_t(buf, 25, main_valve_state);
_mav_put_float(buf, 24, battery_voltage);
_mav_put_float(buf, 28, current_consumption);
_mav_put_uint8_t(buf, 32, floating_level);
_mav_put_uint8_t(buf, 33, main_valve_state);
_mav_put_uint8_t(buf, 34, venting_valve_state);
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MOTOR_TM, buf, MAVLINK_MSG_ID_MOTOR_TM_MIN_LEN, MAVLINK_MSG_ID_MOTOR_TM_LEN, MAVLINK_MSG_ID_MOTOR_TM_CRC);
#else
......@@ -207,8 +240,11 @@ static inline void mavlink_msg_motor_tm_send(mavlink_channel_t chan, uint64_t ti
packet.bottom_tank_pressure = bottom_tank_pressure;
packet.combustion_chamber_pressure = combustion_chamber_pressure;
packet.tank_temperature = tank_temperature;
packet.battery_voltage = battery_voltage;
packet.current_consumption = current_consumption;
packet.floating_level = floating_level;
packet.main_valve_state = main_valve_state;
packet.venting_valve_state = venting_valve_state;
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MOTOR_TM, (const char *)&packet, MAVLINK_MSG_ID_MOTOR_TM_MIN_LEN, MAVLINK_MSG_ID_MOTOR_TM_LEN, MAVLINK_MSG_ID_MOTOR_TM_CRC);
#endif
......@@ -222,7 +258,7 @@ static inline void mavlink_msg_motor_tm_send(mavlink_channel_t chan, uint64_t ti
static inline void mavlink_msg_motor_tm_send_struct(mavlink_channel_t chan, const mavlink_motor_tm_t* motor_tm)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
mavlink_msg_motor_tm_send(chan, motor_tm->timestamp, motor_tm->top_tank_pressure, motor_tm->bottom_tank_pressure, motor_tm->combustion_chamber_pressure, motor_tm->floating_level, motor_tm->tank_temperature, motor_tm->main_valve_state);
mavlink_msg_motor_tm_send(chan, motor_tm->timestamp, motor_tm->top_tank_pressure, motor_tm->bottom_tank_pressure, motor_tm->combustion_chamber_pressure, motor_tm->floating_level, motor_tm->tank_temperature, motor_tm->main_valve_state, motor_tm->venting_valve_state, motor_tm->battery_voltage, motor_tm->current_consumption);
#else
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MOTOR_TM, (const char *)motor_tm, MAVLINK_MSG_ID_MOTOR_TM_MIN_LEN, MAVLINK_MSG_ID_MOTOR_TM_LEN, MAVLINK_MSG_ID_MOTOR_TM_CRC);
#endif
......@@ -236,7 +272,7 @@ static inline void mavlink_msg_motor_tm_send_struct(mavlink_channel_t chan, cons
is usually the receive buffer for the channel, and allows a reply to an
incoming message with minimum stack space usage.
*/
static inline void mavlink_msg_motor_tm_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint64_t timestamp, float top_tank_pressure, float bottom_tank_pressure, float combustion_chamber_pressure, uint8_t floating_level, float tank_temperature, uint8_t main_valve_state)
static inline void mavlink_msg_motor_tm_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint64_t timestamp, float top_tank_pressure, float bottom_tank_pressure, float combustion_chamber_pressure, uint8_t floating_level, float tank_temperature, uint8_t main_valve_state, uint8_t venting_valve_state, float battery_voltage, float current_consumption)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char *buf = (char *)msgbuf;
......@@ -245,8 +281,11 @@ static inline void mavlink_msg_motor_tm_send_buf(mavlink_message_t *msgbuf, mavl
_mav_put_float(buf, 12, bottom_tank_pressure);
_mav_put_float(buf, 16, combustion_chamber_pressure);
_mav_put_float(buf, 20, tank_temperature);
_mav_put_uint8_t(buf, 24, floating_level);
_mav_put_uint8_t(buf, 25, main_valve_state);
_mav_put_float(buf, 24, battery_voltage);
_mav_put_float(buf, 28, current_consumption);
_mav_put_uint8_t(buf, 32, floating_level);
_mav_put_uint8_t(buf, 33, main_valve_state);
_mav_put_uint8_t(buf, 34, venting_valve_state);
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MOTOR_TM, buf, MAVLINK_MSG_ID_MOTOR_TM_MIN_LEN, MAVLINK_MSG_ID_MOTOR_TM_LEN, MAVLINK_MSG_ID_MOTOR_TM_CRC);
#else
......@@ -256,8 +295,11 @@ static inline void mavlink_msg_motor_tm_send_buf(mavlink_message_t *msgbuf, mavl
packet->bottom_tank_pressure = bottom_tank_pressure;
packet->combustion_chamber_pressure = combustion_chamber_pressure;
packet->tank_temperature = tank_temperature;
packet->battery_voltage = battery_voltage;
packet->current_consumption = current_consumption;
packet->floating_level = floating_level;
packet->main_valve_state = main_valve_state;
packet->venting_valve_state = venting_valve_state;
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_MOTOR_TM, (const char *)packet, MAVLINK_MSG_ID_MOTOR_TM_MIN_LEN, MAVLINK_MSG_ID_MOTOR_TM_LEN, MAVLINK_MSG_ID_MOTOR_TM_CRC);
#endif
......@@ -316,7 +358,7 @@ static inline float mavlink_msg_motor_tm_get_combustion_chamber_pressure(const m
*/
static inline uint8_t mavlink_msg_motor_tm_get_floating_level(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint8_t(msg, 24);
return _MAV_RETURN_uint8_t(msg, 32);
}
/**
......@@ -336,7 +378,37 @@ static inline float mavlink_msg_motor_tm_get_tank_temperature(const mavlink_mess
*/
static inline uint8_t mavlink_msg_motor_tm_get_main_valve_state(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint8_t(msg, 25);
return _MAV_RETURN_uint8_t(msg, 33);
}
/**
* @brief Get field venting_valve_state from motor_tm message
*
* @return 1 If the venting valve is open
*/
static inline uint8_t mavlink_msg_motor_tm_get_venting_valve_state(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint8_t(msg, 34);
}
/**
* @brief Get field battery_voltage from motor_tm message
*
* @return [V] Battery voltage
*/
static inline float mavlink_msg_motor_tm_get_battery_voltage(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 24);
}
/**
* @brief Get field current_consumption from motor_tm message
*
* @return [A] Current drained from the battery
*/
static inline float mavlink_msg_motor_tm_get_current_consumption(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 28);
}
/**
......@@ -353,8 +425,11 @@ static inline void mavlink_msg_motor_tm_decode(const mavlink_message_t* msg, mav
motor_tm->bottom_tank_pressure = mavlink_msg_motor_tm_get_bottom_tank_pressure(msg);
motor_tm->combustion_chamber_pressure = mavlink_msg_motor_tm_get_combustion_chamber_pressure(msg);
motor_tm->tank_temperature = mavlink_msg_motor_tm_get_tank_temperature(msg);
motor_tm->battery_voltage = mavlink_msg_motor_tm_get_battery_voltage(msg);
motor_tm->current_consumption = mavlink_msg_motor_tm_get_current_consumption(msg);
motor_tm->floating_level = mavlink_msg_motor_tm_get_floating_level(msg);
motor_tm->main_valve_state = mavlink_msg_motor_tm_get_main_valve_state(msg);
motor_tm->venting_valve_state = mavlink_msg_motor_tm_get_venting_valve_state(msg);
#else
uint8_t len = msg->len < MAVLINK_MSG_ID_MOTOR_TM_LEN? msg->len : MAVLINK_MSG_ID_MOTOR_TM_LEN;
memset(motor_tm, 0, MAVLINK_MSG_ID_MOTOR_TM_LEN);
......
mavlink_lib/gemini/mavlink_msg_payload_flight_tm.h
View file @ 7abedf97
......@@ -8,7 +8,6 @@ typedef struct __mavlink_payload_flight_tm_t {
uint64_t timestamp; /*< [us] Timestamp in microseconds*/
float pressure_digi; /*< [Pa] Pressure from digital sensor*/
float pressure_static; /*< [Pa] Pressure from static port*/
float pressure_dpl; /*< [Pa] Pressure from deployment vane sensor*/
float airspeed_pitot; /*< [m/s] Pitot airspeed*/
float altitude_agl; /*< [m] Altitude above ground level*/
float acc_x; /*< [m/s^2] Acceleration on X axis (body)*/
......@@ -40,24 +39,26 @@ typedef struct __mavlink_payload_flight_tm_t {
float nas_bias_z; /*< Navigation system gyroscope bias on z axis*/
float wes_n; /*< [m/s] Wind estimated north velocity*/
float wes_e; /*< [m/s] Wind estimated east velocity*/
float vbat; /*< [V] Battery voltage*/
float vsupply_5v; /*< [V] Power supply 5V*/
float battery_voltage; /*< [V] Battery voltage*/
float cam_battery_voltage; /*< [V] Camera battery voltage*/
float current_consumption; /*< [A] Battery current*/
float temperature; /*< [degC] Temperature*/
uint8_t fmm_state; /*< Flight Mode Manager State*/
uint8_t nas_state; /*< Navigation System FSM State*/
uint8_t wes_state; /*< Wind Estimation System FSM State*/
uint8_t gps_fix; /*< GPS fix (1 = fix, 0 = no fix)*/
uint8_t pin_nosecone; /*< Nosecone pin status (1 = connected, 0 = disconnected)*/
uint8_t cutter_presence; /*< Cutter presence status (1 = present, 0 = missing)*/
int8_t logger_error; /*< Logger error (0 = no error)*/
} mavlink_payload_flight_tm_t;
#define MAVLINK_MSG_ID_PAYLOAD_FLIGHT_TM_LEN 162
#define MAVLINK_MSG_ID_PAYLOAD_FLIGHT_TM_MIN_LEN 162
#define MAVLINK_MSG_ID_209_LEN 162
#define MAVLINK_MSG_ID_209_MIN_LEN 162
#define MAVLINK_MSG_ID_PAYLOAD_FLIGHT_TM_LEN 163
#define MAVLINK_MSG_ID_PAYLOAD_FLIGHT_TM_MIN_LEN 163
#define MAVLINK_MSG_ID_209_LEN 163
#define MAVLINK_MSG_ID_209_MIN_LEN 163
#define MAVLINK_MSG_ID_PAYLOAD_FLIGHT_TM_CRC 6
#define MAVLINK_MSG_ID_209_CRC 6
#define MAVLINK_MSG_ID_PAYLOAD_FLIGHT_TM_CRC 84
#define MAVLINK_MSG_ID_209_CRC 84
......@@ -65,101 +66,103 @@ typedef struct __mavlink_payload_flight_tm_t {
#define MAVLINK_MESSAGE_INFO_PAYLOAD_FLIGHT_TM { \
209, \
"PAYLOAD_FLIGHT_TM", \
44, \
45, \
{ { "timestamp", NULL, MAVLINK_TYPE_UINT64_T, 0, 0, offsetof(mavlink_payload_flight_tm_t, timestamp) }, \
{ "fmm_state", NULL, MAVLINK_TYPE_UINT8_T, 0, 156, offsetof(mavlink_payload_flight_tm_t, fmm_state) }, \
{ "nas_state", NULL, MAVLINK_TYPE_UINT8_T, 0, 157, offsetof(mavlink_payload_flight_tm_t, nas_state) }, \
{ "wes_state", NULL, MAVLINK_TYPE_UINT8_T, 0, 158, offsetof(mavlink_payload_flight_tm_t, wes_state) }, \
{ "pressure_digi", NULL, MAVLINK_TYPE_FLOAT, 0, 8, offsetof(mavlink_payload_flight_tm_t, pressure_digi) }, \
{ "pressure_static", NULL, MAVLINK_TYPE_FLOAT, 0, 12, offsetof(mavlink_payload_flight_tm_t, pressure_static) }, \
{ "pressure_dpl", NULL, MAVLINK_TYPE_FLOAT, 0, 16, offsetof(mavlink_payload_flight_tm_t, pressure_dpl) }, \
{ "airspeed_pitot", NULL, MAVLINK_TYPE_FLOAT, 0, 20, offsetof(mavlink_payload_flight_tm_t, airspeed_pitot) }, \
{ "altitude_agl", NULL, MAVLINK_TYPE_FLOAT, 0, 24, offsetof(mavlink_payload_flight_tm_t, altitude_agl) }, \
{ "acc_x", NULL, MAVLINK_TYPE_FLOAT, 0, 28, offsetof(mavlink_payload_flight_tm_t, acc_x) }, \
{ "acc_y", NULL, MAVLINK_TYPE_FLOAT, 0, 32, offsetof(mavlink_payload_flight_tm_t, acc_y) }, \
{ "acc_z", NULL, MAVLINK_TYPE_FLOAT, 0, 36, offsetof(mavlink_payload_flight_tm_t, acc_z) }, \
{ "gyro_x", NULL, MAVLINK_TYPE_FLOAT, 0, 40, offsetof(mavlink_payload_flight_tm_t, gyro_x) }, \
{ "gyro_y", NULL, MAVLINK_TYPE_FLOAT, 0, 44, offsetof(mavlink_payload_flight_tm_t, gyro_y) }, \
{ "gyro_z", NULL, MAVLINK_TYPE_FLOAT, 0, 48, offsetof(mavlink_payload_flight_tm_t, gyro_z) }, \
{ "mag_x", NULL, MAVLINK_TYPE_FLOAT, 0, 52, offsetof(mavlink_payload_flight_tm_t, mag_x) }, \
{ "mag_y", NULL, MAVLINK_TYPE_FLOAT, 0, 56, offsetof(mavlink_payload_flight_tm_t, mag_y) }, \
{ "mag_z", NULL, MAVLINK_TYPE_FLOAT, 0, 60, offsetof(mavlink_payload_flight_tm_t, mag_z) }, \
{ "airspeed_pitot", NULL, MAVLINK_TYPE_FLOAT, 0, 16, offsetof(mavlink_payload_flight_tm_t, airspeed_pitot) }, \
{ "altitude_agl", NULL, MAVLINK_TYPE_FLOAT, 0, 20, offsetof(mavlink_payload_flight_tm_t, altitude_agl) }, \
{ "acc_x", NULL, MAVLINK_TYPE_FLOAT, 0, 24, offsetof(mavlink_payload_flight_tm_t, acc_x) }, \
{ "acc_y", NULL, MAVLINK_TYPE_FLOAT, 0, 28, offsetof(mavlink_payload_flight_tm_t, acc_y) }, \
{ "acc_z", NULL, MAVLINK_TYPE_FLOAT, 0, 32, offsetof(mavlink_payload_flight_tm_t, acc_z) }, \
{ "gyro_x", NULL, MAVLINK_TYPE_FLOAT, 0, 36, offsetof(mavlink_payload_flight_tm_t, gyro_x) }, \
{ "gyro_y", NULL, MAVLINK_TYPE_FLOAT, 0, 40, offsetof(mavlink_payload_flight_tm_t, gyro_y) }, \
{ "gyro_z", NULL, MAVLINK_TYPE_FLOAT, 0, 44, offsetof(mavlink_payload_flight_tm_t, gyro_z) }, \
{ "mag_x", NULL, MAVLINK_TYPE_FLOAT, 0, 48, offsetof(mavlink_payload_flight_tm_t, mag_x) }, \
{ "mag_y", NULL, MAVLINK_TYPE_FLOAT, 0, 52, offsetof(mavlink_payload_flight_tm_t, mag_y) }, \
{ "mag_z", NULL, MAVLINK_TYPE_FLOAT, 0, 56, offsetof(mavlink_payload_flight_tm_t, mag_z) }, \
{ "gps_fix", NULL, MAVLINK_TYPE_UINT8_T, 0, 159, offsetof(mavlink_payload_flight_tm_t, gps_fix) }, \
{ "gps_lat", NULL, MAVLINK_TYPE_FLOAT, 0, 64, offsetof(mavlink_payload_flight_tm_t, gps_lat) }, \
{ "gps_lon", NULL, MAVLINK_TYPE_FLOAT, 0, 68, offsetof(mavlink_payload_flight_tm_t, gps_lon) }, \
{ "gps_alt", NULL, MAVLINK_TYPE_FLOAT, 0, 72, offsetof(mavlink_payload_flight_tm_t, gps_alt) }, \
{ "left_servo_angle", NULL, MAVLINK_TYPE_FLOAT, 0, 76, offsetof(mavlink_payload_flight_tm_t, left_servo_angle) }, \
{ "right_servo_angle", NULL, MAVLINK_TYPE_FLOAT, 0, 80, offsetof(mavlink_payload_flight_tm_t, right_servo_angle) }, \
{ "nas_n", NULL, MAVLINK_TYPE_FLOAT, 0, 84, offsetof(mavlink_payload_flight_tm_t, nas_n) }, \
{ "nas_e", NULL, MAVLINK_TYPE_FLOAT, 0, 88, offsetof(mavlink_payload_flight_tm_t, nas_e) }, \
{ "nas_d", NULL, MAVLINK_TYPE_FLOAT, 0, 92, offsetof(mavlink_payload_flight_tm_t, nas_d) }, \
{ "nas_vn", NULL, MAVLINK_TYPE_FLOAT, 0, 96, offsetof(mavlink_payload_flight_tm_t, nas_vn) }, \
{ "nas_ve", NULL, MAVLINK_TYPE_FLOAT, 0, 100, offsetof(mavlink_payload_flight_tm_t, nas_ve) }, \
{ "nas_vd", NULL, MAVLINK_TYPE_FLOAT, 0, 104, offsetof(mavlink_payload_flight_tm_t, nas_vd) }, \
{ "nas_qx", NULL, MAVLINK_TYPE_FLOAT, 0, 108, offsetof(mavlink_payload_flight_tm_t, nas_qx) }, \
{ "nas_qy", NULL, MAVLINK_TYPE_FLOAT, 0, 112, offsetof(mavlink_payload_flight_tm_t, nas_qy) }, \
{ "nas_qz", NULL, MAVLINK_TYPE_FLOAT, 0, 116, offsetof(mavlink_payload_flight_tm_t, nas_qz) }, \
{ "nas_qw", NULL, MAVLINK_TYPE_FLOAT, 0, 120, offsetof(mavlink_payload_flight_tm_t, nas_qw) }, \
{ "nas_bias_x", NULL, MAVLINK_TYPE_FLOAT, 0, 124, offsetof(mavlink_payload_flight_tm_t, nas_bias_x) }, \
{ "nas_bias_y", NULL, MAVLINK_TYPE_FLOAT, 0, 128, offsetof(mavlink_payload_flight_tm_t, nas_bias_y) }, \
{ "nas_bias_z", NULL, MAVLINK_TYPE_FLOAT, 0, 132, offsetof(mavlink_payload_flight_tm_t, nas_bias_z) }, \
{ "wes_n", NULL, MAVLINK_TYPE_FLOAT, 0, 136, offsetof(mavlink_payload_flight_tm_t, wes_n) }, \
{ "wes_e", NULL, MAVLINK_TYPE_FLOAT, 0, 140, offsetof(mavlink_payload_flight_tm_t, wes_e) }, \
{ "gps_lat", NULL, MAVLINK_TYPE_FLOAT, 0, 60, offsetof(mavlink_payload_flight_tm_t, gps_lat) }, \
{ "gps_lon", NULL, MAVLINK_TYPE_FLOAT, 0, 64, offsetof(mavlink_payload_flight_tm_t, gps_lon) }, \
{ "gps_alt", NULL, MAVLINK_TYPE_FLOAT, 0, 68, offsetof(mavlink_payload_flight_tm_t, gps_alt) }, \
{ "left_servo_angle", NULL, MAVLINK_TYPE_FLOAT, 0, 72, offsetof(mavlink_payload_flight_tm_t, left_servo_angle) }, \
{ "right_servo_angle", NULL, MAVLINK_TYPE_FLOAT, 0, 76, offsetof(mavlink_payload_flight_tm_t, right_servo_angle) }, \
{ "nas_n", NULL, MAVLINK_TYPE_FLOAT, 0, 80, offsetof(mavlink_payload_flight_tm_t, nas_n) }, \
{ "nas_e", NULL, MAVLINK_TYPE_FLOAT, 0, 84, offsetof(mavlink_payload_flight_tm_t, nas_e) }, \
{ "nas_d", NULL, MAVLINK_TYPE_FLOAT, 0, 88, offsetof(mavlink_payload_flight_tm_t, nas_d) }, \
{ "nas_vn", NULL, MAVLINK_TYPE_FLOAT, 0, 92, offsetof(mavlink_payload_flight_tm_t, nas_vn) }, \
{ "nas_ve", NULL, MAVLINK_TYPE_FLOAT, 0, 96, offsetof(mavlink_payload_flight_tm_t, nas_ve) }, \
{ "nas_vd", NULL, MAVLINK_TYPE_FLOAT, 0, 100, offsetof(mavlink_payload_flight_tm_t, nas_vd) }, \
{ "nas_qx", NULL, MAVLINK_TYPE_FLOAT, 0, 104, offsetof(mavlink_payload_flight_tm_t, nas_qx) }, \
{ "nas_qy", NULL, MAVLINK_TYPE_FLOAT, 0, 108, offsetof(mavlink_payload_flight_tm_t, nas_qy) }, \
{ "nas_qz", NULL, MAVLINK_TYPE_FLOAT, 0, 112, offsetof(mavlink_payload_flight_tm_t, nas_qz) }, \
{ "nas_qw", NULL, MAVLINK_TYPE_FLOAT, 0, 116, offsetof(mavlink_payload_flight_tm_t, nas_qw) }, \
{ "nas_bias_x", NULL, MAVLINK_TYPE_FLOAT, 0, 120, offsetof(mavlink_payload_flight_tm_t, nas_bias_x) }, \
{ "nas_bias_y", NULL, MAVLINK_TYPE_FLOAT, 0, 124, offsetof(mavlink_payload_flight_tm_t, nas_bias_y) }, \
{ "nas_bias_z", NULL, MAVLINK_TYPE_FLOAT, 0, 128, offsetof(mavlink_payload_flight_tm_t, nas_bias_z) }, \
{ "wes_n", NULL, MAVLINK_TYPE_FLOAT, 0, 132, offsetof(mavlink_payload_flight_tm_t, wes_n) }, \
{ "wes_e", NULL, MAVLINK_TYPE_FLOAT, 0, 136, offsetof(mavlink_payload_flight_tm_t, wes_e) }, \
{ "pin_nosecone", NULL, MAVLINK_TYPE_UINT8_T, 0, 160, offsetof(mavlink_payload_flight_tm_t, pin_nosecone) }, \
{ "vbat", NULL, MAVLINK_TYPE_FLOAT, 0, 144, offsetof(mavlink_payload_flight_tm_t, vbat) }, \
{ "vsupply_5v", NULL, MAVLINK_TYPE_FLOAT, 0, 148, offsetof(mavlink_payload_flight_tm_t, vsupply_5v) }, \
{ "battery_voltage", NULL, MAVLINK_TYPE_FLOAT, 0, 140, offsetof(mavlink_payload_flight_tm_t, battery_voltage) }, \
{ "cam_battery_voltage", NULL, MAVLINK_TYPE_FLOAT, 0, 144, offsetof(mavlink_payload_flight_tm_t, cam_battery_voltage) }, \
{ "current_consumption", NULL, MAVLINK_TYPE_FLOAT, 0, 148, offsetof(mavlink_payload_flight_tm_t, current_consumption) }, \
{ "cutter_presence", NULL, MAVLINK_TYPE_UINT8_T, 0, 161, offsetof(mavlink_payload_flight_tm_t, cutter_presence) }, \
{ "temperature", NULL, MAVLINK_TYPE_FLOAT, 0, 152, offsetof(mavlink_payload_flight_tm_t, temperature) }, \
{ "logger_error", NULL, MAVLINK_TYPE_INT8_T, 0, 161, offsetof(mavlink_payload_flight_tm_t, logger_error) }, \
{ "logger_error", NULL, MAVLINK_TYPE_INT8_T, 0, 162, offsetof(mavlink_payload_flight_tm_t, logger_error) }, \
} \
}
#else
#define MAVLINK_MESSAGE_INFO_PAYLOAD_FLIGHT_TM { \
"PAYLOAD_FLIGHT_TM", \
44, \
45, \
{ { "timestamp", NULL, MAVLINK_TYPE_UINT64_T, 0, 0, offsetof(mavlink_payload_flight_tm_t, timestamp) }, \
{ "fmm_state", NULL, MAVLINK_TYPE_UINT8_T, 0, 156, offsetof(mavlink_payload_flight_tm_t, fmm_state) }, \
{ "nas_state", NULL, MAVLINK_TYPE_UINT8_T, 0, 157, offsetof(mavlink_payload_flight_tm_t, nas_state) }, \
{ "wes_state", NULL, MAVLINK_TYPE_UINT8_T, 0, 158, offsetof(mavlink_payload_flight_tm_t, wes_state) }, \
{ "pressure_digi", NULL, MAVLINK_TYPE_FLOAT, 0, 8, offsetof(mavlink_payload_flight_tm_t, pressure_digi) }, \
{ "pressure_static", NULL, MAVLINK_TYPE_FLOAT, 0, 12, offsetof(mavlink_payload_flight_tm_t, pressure_static) }, \
{ "pressure_dpl", NULL, MAVLINK_TYPE_FLOAT, 0, 16, offsetof(mavlink_payload_flight_tm_t, pressure_dpl) }, \
{ "airspeed_pitot", NULL, MAVLINK_TYPE_FLOAT, 0, 20, offsetof(mavlink_payload_flight_tm_t, airspeed_pitot) }, \
{ "altitude_agl", NULL, MAVLINK_TYPE_FLOAT, 0, 24, offsetof(mavlink_payload_flight_tm_t, altitude_agl) }, \
{ "acc_x", NULL, MAVLINK_TYPE_FLOAT, 0, 28, offsetof(mavlink_payload_flight_tm_t, acc_x) }, \
{ "acc_y", NULL, MAVLINK_TYPE_FLOAT, 0, 32, offsetof(mavlink_payload_flight_tm_t, acc_y) }, \
{ "acc_z", NULL, MAVLINK_TYPE_FLOAT, 0, 36, offsetof(mavlink_payload_flight_tm_t, acc_z) }, \
{ "gyro_x", NULL, MAVLINK_TYPE_FLOAT, 0, 40, offsetof(mavlink_payload_flight_tm_t, gyro_x) }, \
{ "gyro_y", NULL, MAVLINK_TYPE_FLOAT, 0, 44, offsetof(mavlink_payload_flight_tm_t, gyro_y) }, \
{ "gyro_z", NULL, MAVLINK_TYPE_FLOAT, 0, 48, offsetof(mavlink_payload_flight_tm_t, gyro_z) }, \
{ "mag_x", NULL, MAVLINK_TYPE_FLOAT, 0, 52, offsetof(mavlink_payload_flight_tm_t, mag_x) }, \
{ "mag_y", NULL, MAVLINK_TYPE_FLOAT, 0, 56, offsetof(mavlink_payload_flight_tm_t, mag_y) }, \
{ "mag_z", NULL, MAVLINK_TYPE_FLOAT, 0, 60, offsetof(mavlink_payload_flight_tm_t, mag_z) }, \
{ "airspeed_pitot", NULL, MAVLINK_TYPE_FLOAT, 0, 16, offsetof(mavlink_payload_flight_tm_t, airspeed_pitot) }, \
{ "altitude_agl", NULL, MAVLINK_TYPE_FLOAT, 0, 20, offsetof(mavlink_payload_flight_tm_t, altitude_agl) }, \
{ "acc_x", NULL, MAVLINK_TYPE_FLOAT, 0, 24, offsetof(mavlink_payload_flight_tm_t, acc_x) }, \
{ "acc_y", NULL, MAVLINK_TYPE_FLOAT, 0, 28, offsetof(mavlink_payload_flight_tm_t, acc_y) }, \
{ "acc_z", NULL, MAVLINK_TYPE_FLOAT, 0, 32, offsetof(mavlink_payload_flight_tm_t, acc_z) }, \
{ "gyro_x", NULL, MAVLINK_TYPE_FLOAT, 0, 36, offsetof(mavlink_payload_flight_tm_t, gyro_x) }, \
{ "gyro_y", NULL, MAVLINK_TYPE_FLOAT, 0, 40, offsetof(mavlink_payload_flight_tm_t, gyro_y) }, \
{ "gyro_z", NULL, MAVLINK_TYPE_FLOAT, 0, 44, offsetof(mavlink_payload_flight_tm_t, gyro_z) }, \
{ "mag_x", NULL, MAVLINK_TYPE_FLOAT, 0, 48, offsetof(mavlink_payload_flight_tm_t, mag_x) }, \
{ "mag_y", NULL, MAVLINK_TYPE_FLOAT, 0, 52, offsetof(mavlink_payload_flight_tm_t, mag_y) }, \
{ "mag_z", NULL, MAVLINK_TYPE_FLOAT, 0, 56, offsetof(mavlink_payload_flight_tm_t, mag_z) }, \
{ "gps_fix", NULL, MAVLINK_TYPE_UINT8_T, 0, 159, offsetof(mavlink_payload_flight_tm_t, gps_fix) }, \
{ "gps_lat", NULL, MAVLINK_TYPE_FLOAT, 0, 64, offsetof(mavlink_payload_flight_tm_t, gps_lat) }, \
{ "gps_lon", NULL, MAVLINK_TYPE_FLOAT, 0, 68, offsetof(mavlink_payload_flight_tm_t, gps_lon) }, \
{ "gps_alt", NULL, MAVLINK_TYPE_FLOAT, 0, 72, offsetof(mavlink_payload_flight_tm_t, gps_alt) }, \
{ "left_servo_angle", NULL, MAVLINK_TYPE_FLOAT, 0, 76, offsetof(mavlink_payload_flight_tm_t, left_servo_angle) }, \
{ "right_servo_angle", NULL, MAVLINK_TYPE_FLOAT, 0, 80, offsetof(mavlink_payload_flight_tm_t, right_servo_angle) }, \
{ "nas_n", NULL, MAVLINK_TYPE_FLOAT, 0, 84, offsetof(mavlink_payload_flight_tm_t, nas_n) }, \
{ "nas_e", NULL, MAVLINK_TYPE_FLOAT, 0, 88, offsetof(mavlink_payload_flight_tm_t, nas_e) }, \
{ "nas_d", NULL, MAVLINK_TYPE_FLOAT, 0, 92, offsetof(mavlink_payload_flight_tm_t, nas_d) }, \
{ "nas_vn", NULL, MAVLINK_TYPE_FLOAT, 0, 96, offsetof(mavlink_payload_flight_tm_t, nas_vn) }, \
{ "nas_ve", NULL, MAVLINK_TYPE_FLOAT, 0, 100, offsetof(mavlink_payload_flight_tm_t, nas_ve) }, \
{ "nas_vd", NULL, MAVLINK_TYPE_FLOAT, 0, 104, offsetof(mavlink_payload_flight_tm_t, nas_vd) }, \
{ "nas_qx", NULL, MAVLINK_TYPE_FLOAT, 0, 108, offsetof(mavlink_payload_flight_tm_t, nas_qx) }, \
{ "nas_qy", NULL, MAVLINK_TYPE_FLOAT, 0, 112, offsetof(mavlink_payload_flight_tm_t, nas_qy) }, \
{ "nas_qz", NULL, MAVLINK_TYPE_FLOAT, 0, 116, offsetof(mavlink_payload_flight_tm_t, nas_qz) }, \
{ "nas_qw", NULL, MAVLINK_TYPE_FLOAT, 0, 120, offsetof(mavlink_payload_flight_tm_t, nas_qw) }, \
{ "nas_bias_x", NULL, MAVLINK_TYPE_FLOAT, 0, 124, offsetof(mavlink_payload_flight_tm_t, nas_bias_x) }, \
{ "nas_bias_y", NULL, MAVLINK_TYPE_FLOAT, 0, 128, offsetof(mavlink_payload_flight_tm_t, nas_bias_y) }, \
{ "nas_bias_z", NULL, MAVLINK_TYPE_FLOAT, 0, 132, offsetof(mavlink_payload_flight_tm_t, nas_bias_z) }, \
{ "wes_n", NULL, MAVLINK_TYPE_FLOAT, 0, 136, offsetof(mavlink_payload_flight_tm_t, wes_n) }, \
{ "wes_e", NULL, MAVLINK_TYPE_FLOAT, 0, 140, offsetof(mavlink_payload_flight_tm_t, wes_e) }, \
{ "gps_lat", NULL, MAVLINK_TYPE_FLOAT, 0, 60, offsetof(mavlink_payload_flight_tm_t, gps_lat) }, \
{ "gps_lon", NULL, MAVLINK_TYPE_FLOAT, 0, 64, offsetof(mavlink_payload_flight_tm_t, gps_lon) }, \
{ "gps_alt", NULL, MAVLINK_TYPE_FLOAT, 0, 68, offsetof(mavlink_payload_flight_tm_t, gps_alt) }, \
{ "left_servo_angle", NULL, MAVLINK_TYPE_FLOAT, 0, 72, offsetof(mavlink_payload_flight_tm_t, left_servo_angle) }, \
{ "right_servo_angle", NULL, MAVLINK_TYPE_FLOAT, 0, 76, offsetof(mavlink_payload_flight_tm_t, right_servo_angle) }, \
{ "nas_n", NULL, MAVLINK_TYPE_FLOAT, 0, 80, offsetof(mavlink_payload_flight_tm_t, nas_n) }, \
{ "nas_e", NULL, MAVLINK_TYPE_FLOAT, 0, 84, offsetof(mavlink_payload_flight_tm_t, nas_e) }, \
{ "nas_d", NULL, MAVLINK_TYPE_FLOAT, 0, 88, offsetof(mavlink_payload_flight_tm_t, nas_d) }, \
{ "nas_vn", NULL, MAVLINK_TYPE_FLOAT, 0, 92, offsetof(mavlink_payload_flight_tm_t, nas_vn) }, \
{ "nas_ve", NULL, MAVLINK_TYPE_FLOAT, 0, 96, offsetof(mavlink_payload_flight_tm_t, nas_ve) }, \
{ "nas_vd", NULL, MAVLINK_TYPE_FLOAT, 0, 100, offsetof(mavlink_payload_flight_tm_t, nas_vd) }, \
{ "nas_qx", NULL, MAVLINK_TYPE_FLOAT, 0, 104, offsetof(mavlink_payload_flight_tm_t, nas_qx) }, \
{ "nas_qy", NULL, MAVLINK_TYPE_FLOAT, 0, 108, offsetof(mavlink_payload_flight_tm_t, nas_qy) }, \
{ "nas_qz", NULL, MAVLINK_TYPE_FLOAT, 0, 112, offsetof(mavlink_payload_flight_tm_t, nas_qz) }, \
{ "nas_qw", NULL, MAVLINK_TYPE_FLOAT, 0, 116, offsetof(mavlink_payload_flight_tm_t, nas_qw) }, \
{ "nas_bias_x", NULL, MAVLINK_TYPE_FLOAT, 0, 120, offsetof(mavlink_payload_flight_tm_t, nas_bias_x) }, \
{ "nas_bias_y", NULL, MAVLINK_TYPE_FLOAT, 0, 124, offsetof(mavlink_payload_flight_tm_t, nas_bias_y) }, \
{ "nas_bias_z", NULL, MAVLINK_TYPE_FLOAT, 0, 128, offsetof(mavlink_payload_flight_tm_t, nas_bias_z) }, \
{ "wes_n", NULL, MAVLINK_TYPE_FLOAT, 0, 132, offsetof(mavlink_payload_flight_tm_t, wes_n) }, \
{ "wes_e", NULL, MAVLINK_TYPE_FLOAT, 0, 136, offsetof(mavlink_payload_flight_tm_t, wes_e) }, \
{ "pin_nosecone", NULL, MAVLINK_TYPE_UINT8_T, 0, 160, offsetof(mavlink_payload_flight_tm_t, pin_nosecone) }, \
{ "vbat", NULL, MAVLINK_TYPE_FLOAT, 0, 144, offsetof(mavlink_payload_flight_tm_t, vbat) }, \
{ "vsupply_5v", NULL, MAVLINK_TYPE_FLOAT, 0, 148, offsetof(mavlink_payload_flight_tm_t, vsupply_5v) }, \
{ "battery_voltage", NULL, MAVLINK_TYPE_FLOAT, 0, 140, offsetof(mavlink_payload_flight_tm_t, battery_voltage) }, \
{ "cam_battery_voltage", NULL, MAVLINK_TYPE_FLOAT, 0, 144, offsetof(mavlink_payload_flight_tm_t, cam_battery_voltage) }, \
{ "current_consumption", NULL, MAVLINK_TYPE_FLOAT, 0, 148, offsetof(mavlink_payload_flight_tm_t, current_consumption) }, \
{ "cutter_presence", NULL, MAVLINK_TYPE_UINT8_T, 0, 161, offsetof(mavlink_payload_flight_tm_t, cutter_presence) }, \
{ "temperature", NULL, MAVLINK_TYPE_FLOAT, 0, 152, offsetof(mavlink_payload_flight_tm_t, temperature) }, \
{ "logger_error", NULL, MAVLINK_TYPE_INT8_T, 0, 161, offsetof(mavlink_payload_flight_tm_t, logger_error) }, \
{ "logger_error", NULL, MAVLINK_TYPE_INT8_T, 0, 162, offsetof(mavlink_payload_flight_tm_t, logger_error) }, \
} \
}
#endif
......@@ -176,7 +179,6 @@ typedef struct __mavlink_payload_flight_tm_t {
* @param wes_state Wind Estimation System FSM State
* @param pressure_digi [Pa] Pressure from digital sensor
* @param pressure_static [Pa] Pressure from static port
* @param pressure_dpl [Pa] Pressure from deployment vane sensor
* @param airspeed_pitot [m/s] Pitot airspeed
* @param altitude_agl [m] Altitude above ground level
* @param acc_x [m/s^2] Acceleration on X axis (body)
......@@ -210,61 +212,64 @@ typedef struct __mavlink_payload_flight_tm_t {
* @param wes_n [m/s] Wind estimated north velocity
* @param wes_e [m/s] Wind estimated east velocity
* @param pin_nosecone Nosecone pin status (1 = connected, 0 = disconnected)
* @param vbat [V] Battery voltage
* @param vsupply_5v [V] Power supply 5V
* @param battery_voltage [V] Battery voltage
* @param cam_battery_voltage [V] Camera battery voltage
* @param current_consumption [A] Battery current
* @param cutter_presence Cutter presence status (1 = present, 0 = missing)
* @param temperature [degC] Temperature
* @param logger_error Logger error (0 = no error)
* @return length of the message in bytes (excluding serial stream start sign)
*/
static inline uint16_t mavlink_msg_payload_flight_tm_pack(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg,
uint64_t timestamp, uint8_t fmm_state, uint8_t nas_state, uint8_t wes_state, float pressure_digi, float pressure_static, float pressure_dpl, float airspeed_pitot, float altitude_agl, float acc_x, float acc_y, float acc_z, float gyro_x, float gyro_y, float gyro_z, float mag_x, float mag_y, float mag_z, uint8_t gps_fix, float gps_lat, float gps_lon, float gps_alt, float left_servo_angle, float right_servo_angle, float nas_n, float nas_e, float nas_d, float nas_vn, float nas_ve, float nas_vd, float nas_qx, float nas_qy, float nas_qz, float nas_qw, float nas_bias_x, float nas_bias_y, float nas_bias_z, float wes_n, float wes_e, uint8_t pin_nosecone, float vbat, float vsupply_5v, float temperature, int8_t logger_error)
uint64_t timestamp, uint8_t fmm_state, uint8_t nas_state, uint8_t wes_state, float pressure_digi, float pressure_static, float airspeed_pitot, float altitude_agl, float acc_x, float acc_y, float acc_z, float gyro_x, float gyro_y, float gyro_z, float mag_x, float mag_y, float mag_z, uint8_t gps_fix, float gps_lat, float gps_lon, float gps_alt, float left_servo_angle, float right_servo_angle, float nas_n, float nas_e, float nas_d, float nas_vn, float nas_ve, float nas_vd, float nas_qx, float nas_qy, float nas_qz, float nas_qw, float nas_bias_x, float nas_bias_y, float nas_bias_z, float wes_n, float wes_e, uint8_t pin_nosecone, float battery_voltage, float cam_battery_voltage, float current_consumption, uint8_t cutter_presence, float temperature, int8_t logger_error)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char buf[MAVLINK_MSG_ID_PAYLOAD_FLIGHT_TM_LEN];
_mav_put_uint64_t(buf, 0, timestamp);
_mav_put_float(buf, 8, pressure_digi);
_mav_put_float(buf, 12, pressure_static);
_mav_put_float(buf, 16, pressure_dpl);
_mav_put_float(buf, 20, airspeed_pitot);
_mav_put_float(buf, 24, altitude_agl);
_mav_put_float(buf, 28, acc_x);
_mav_put_float(buf, 32, acc_y);
_mav_put_float(buf, 36, acc_z);
_mav_put_float(buf, 40, gyro_x);
_mav_put_float(buf, 44, gyro_y);
_mav_put_float(buf, 48, gyro_z);
_mav_put_float(buf, 52, mag_x);
_mav_put_float(buf, 56, mag_y);
_mav_put_float(buf, 60, mag_z);
_mav_put_float(buf, 64, gps_lat);
_mav_put_float(buf, 68, gps_lon);
_mav_put_float(buf, 72, gps_alt);
_mav_put_float(buf, 76, left_servo_angle);
_mav_put_float(buf, 80, right_servo_angle);
_mav_put_float(buf, 84, nas_n);
_mav_put_float(buf, 88, nas_e);
_mav_put_float(buf, 92, nas_d);
_mav_put_float(buf, 96, nas_vn);
_mav_put_float(buf, 100, nas_ve);
_mav_put_float(buf, 104, nas_vd);
_mav_put_float(buf, 108, nas_qx);
_mav_put_float(buf, 112, nas_qy);
_mav_put_float(buf, 116, nas_qz);
_mav_put_float(buf, 120, nas_qw);
_mav_put_float(buf, 124, nas_bias_x);
_mav_put_float(buf, 128, nas_bias_y);
_mav_put_float(buf, 132, nas_bias_z);
_mav_put_float(buf, 136, wes_n);
_mav_put_float(buf, 140, wes_e);
_mav_put_float(buf, 144, vbat);
_mav_put_float(buf, 148, vsupply_5v);
_mav_put_float(buf, 16, airspeed_pitot);
_mav_put_float(buf, 20, altitude_agl);
_mav_put_float(buf, 24, acc_x);
_mav_put_float(buf, 28, acc_y);
_mav_put_float(buf, 32, acc_z);
_mav_put_float(buf, 36, gyro_x);
_mav_put_float(buf, 40, gyro_y);
_mav_put_float(buf, 44, gyro_z);
_mav_put_float(buf, 48, mag_x);
_mav_put_float(buf, 52, mag_y);
_mav_put_float(buf, 56, mag_z);
_mav_put_float(buf, 60, gps_lat);
_mav_put_float(buf, 64, gps_lon);
_mav_put_float(buf, 68, gps_alt);
_mav_put_float(buf, 72, left_servo_angle);
_mav_put_float(buf, 76, right_servo_angle);
_mav_put_float(buf, 80, nas_n);
_mav_put_float(buf, 84, nas_e);
_mav_put_float(buf, 88, nas_d);
_mav_put_float(buf, 92, nas_vn);
_mav_put_float(buf, 96, nas_ve);
_mav_put_float(buf, 100, nas_vd);
_mav_put_float(buf, 104, nas_qx);
_mav_put_float(buf, 108, nas_qy);
_mav_put_float(buf, 112, nas_qz);
_mav_put_float(buf, 116, nas_qw);
_mav_put_float(buf, 120, nas_bias_x);
_mav_put_float(buf, 124, nas_bias_y);
_mav_put_float(buf, 128, nas_bias_z);
_mav_put_float(buf, 132, wes_n);
_mav_put_float(buf, 136, wes_e);
_mav_put_float(buf, 140, battery_voltage);
_mav_put_float(buf, 144, cam_battery_voltage);
_mav_put_float(buf, 148, current_consumption);
_mav_put_float(buf, 152, temperature);
_mav_put_uint8_t(buf, 156, fmm_state);
_mav_put_uint8_t(buf, 157, nas_state);
_mav_put_uint8_t(buf, 158, wes_state);
_mav_put_uint8_t(buf, 159, gps_fix);
_mav_put_uint8_t(buf, 160, pin_nosecone);
_mav_put_int8_t(buf, 161, logger_error);
_mav_put_uint8_t(buf, 161, cutter_presence);
_mav_put_int8_t(buf, 162, logger_error);
memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_PAYLOAD_FLIGHT_TM_LEN);
#else
......@@ -272,7 +277,6 @@ static inline uint16_t mavlink_msg_payload_flight_tm_pack(uint8_t system_id, uin
packet.timestamp = timestamp;
packet.pressure_digi = pressure_digi;
packet.pressure_static = pressure_static;
packet.pressure_dpl = pressure_dpl;
packet.airspeed_pitot = airspeed_pitot;
packet.altitude_agl = altitude_agl;
packet.acc_x = acc_x;
......@@ -304,14 +308,16 @@ static inline uint16_t mavlink_msg_payload_flight_tm_pack(uint8_t system_id, uin
packet.nas_bias_z = nas_bias_z;
packet.wes_n = wes_n;
packet.wes_e = wes_e;
packet.vbat = vbat;
packet.vsupply_5v = vsupply_5v;
packet.battery_voltage = battery_voltage;
packet.cam_battery_voltage = cam_battery_voltage;
packet.current_consumption = current_consumption;
packet.temperature = temperature;
packet.fmm_state = fmm_state;
packet.nas_state = nas_state;
packet.wes_state = wes_state;
packet.gps_fix = gps_fix;
packet.pin_nosecone = pin_nosecone;
packet.cutter_presence = cutter_presence;
packet.logger_error = logger_error;
memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_PAYLOAD_FLIGHT_TM_LEN);
......@@ -333,7 +339,6 @@ static inline uint16_t mavlink_msg_payload_flight_tm_pack(uint8_t system_id, uin
* @param wes_state Wind Estimation System FSM State
* @param pressure_digi [Pa] Pressure from digital sensor
* @param pressure_static [Pa] Pressure from static port
* @param pressure_dpl [Pa] Pressure from deployment vane sensor
* @param airspeed_pitot [m/s] Pitot airspeed
* @param altitude_agl [m] Altitude above ground level
* @param acc_x [m/s^2] Acceleration on X axis (body)
......@@ -367,62 +372,65 @@ static inline uint16_t mavlink_msg_payload_flight_tm_pack(uint8_t system_id, uin
* @param wes_n [m/s] Wind estimated north velocity
* @param wes_e [m/s] Wind estimated east velocity
* @param pin_nosecone Nosecone pin status (1 = connected, 0 = disconnected)
* @param vbat [V] Battery voltage
* @param vsupply_5v [V] Power supply 5V
* @param battery_voltage [V] Battery voltage
* @param cam_battery_voltage [V] Camera battery voltage
* @param current_consumption [A] Battery current
* @param cutter_presence Cutter presence status (1 = present, 0 = missing)
* @param temperature [degC] Temperature
* @param logger_error Logger error (0 = no error)
* @return length of the message in bytes (excluding serial stream start sign)
*/
static inline uint16_t mavlink_msg_payload_flight_tm_pack_chan(uint8_t system_id, uint8_t component_id, uint8_t chan,
mavlink_message_t* msg,
uint64_t timestamp,uint8_t fmm_state,uint8_t nas_state,uint8_t wes_state,float pressure_digi,float pressure_static,float pressure_dpl,float airspeed_pitot,float altitude_agl,float acc_x,float acc_y,float acc_z,float gyro_x,float gyro_y,float gyro_z,float mag_x,float mag_y,float mag_z,uint8_t gps_fix,float gps_lat,float gps_lon,float gps_alt,float left_servo_angle,float right_servo_angle,float nas_n,float nas_e,float nas_d,float nas_vn,float nas_ve,float nas_vd,float nas_qx,float nas_qy,float nas_qz,float nas_qw,float nas_bias_x,float nas_bias_y,float nas_bias_z,float wes_n,float wes_e,uint8_t pin_nosecone,float vbat,float vsupply_5v,float temperature,int8_t logger_error)
uint64_t timestamp,uint8_t fmm_state,uint8_t nas_state,uint8_t wes_state,float pressure_digi,float pressure_static,float airspeed_pitot,float altitude_agl,float acc_x,float acc_y,float acc_z,float gyro_x,float gyro_y,float gyro_z,float mag_x,float mag_y,float mag_z,uint8_t gps_fix,float gps_lat,float gps_lon,float gps_alt,float left_servo_angle,float right_servo_angle,float nas_n,float nas_e,float nas_d,float nas_vn,float nas_ve,float nas_vd,float nas_qx,float nas_qy,float nas_qz,float nas_qw,float nas_bias_x,float nas_bias_y,float nas_bias_z,float wes_n,float wes_e,uint8_t pin_nosecone,float battery_voltage,float cam_battery_voltage,float current_consumption,uint8_t cutter_presence,float temperature,int8_t logger_error)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char buf[MAVLINK_MSG_ID_PAYLOAD_FLIGHT_TM_LEN];
_mav_put_uint64_t(buf, 0, timestamp);
_mav_put_float(buf, 8, pressure_digi);
_mav_put_float(buf, 12, pressure_static);
_mav_put_float(buf, 16, pressure_dpl);
_mav_put_float(buf, 20, airspeed_pitot);
_mav_put_float(buf, 24, altitude_agl);
_mav_put_float(buf, 28, acc_x);
_mav_put_float(buf, 32, acc_y);
_mav_put_float(buf, 36, acc_z);
_mav_put_float(buf, 40, gyro_x);
_mav_put_float(buf, 44, gyro_y);
_mav_put_float(buf, 48, gyro_z);
_mav_put_float(buf, 52, mag_x);
_mav_put_float(buf, 56, mag_y);
_mav_put_float(buf, 60, mag_z);
_mav_put_float(buf, 64, gps_lat);
_mav_put_float(buf, 68, gps_lon);
_mav_put_float(buf, 72, gps_alt);
_mav_put_float(buf, 76, left_servo_angle);
_mav_put_float(buf, 80, right_servo_angle);
_mav_put_float(buf, 84, nas_n);
_mav_put_float(buf, 88, nas_e);
_mav_put_float(buf, 92, nas_d);
_mav_put_float(buf, 96, nas_vn);
_mav_put_float(buf, 100, nas_ve);
_mav_put_float(buf, 104, nas_vd);
_mav_put_float(buf, 108, nas_qx);
_mav_put_float(buf, 112, nas_qy);
_mav_put_float(buf, 116, nas_qz);
_mav_put_float(buf, 120, nas_qw);
_mav_put_float(buf, 124, nas_bias_x);
_mav_put_float(buf, 128, nas_bias_y);
_mav_put_float(buf, 132, nas_bias_z);
_mav_put_float(buf, 136, wes_n);
_mav_put_float(buf, 140, wes_e);
_mav_put_float(buf, 144, vbat);
_mav_put_float(buf, 148, vsupply_5v);
_mav_put_float(buf, 16, airspeed_pitot);
_mav_put_float(buf, 20, altitude_agl);
_mav_put_float(buf, 24, acc_x);
_mav_put_float(buf, 28, acc_y);
_mav_put_float(buf, 32, acc_z);
_mav_put_float(buf, 36, gyro_x);
_mav_put_float(buf, 40, gyro_y);
_mav_put_float(buf, 44, gyro_z);
_mav_put_float(buf, 48, mag_x);
_mav_put_float(buf, 52, mag_y);
_mav_put_float(buf, 56, mag_z);
_mav_put_float(buf, 60, gps_lat);
_mav_put_float(buf, 64, gps_lon);
_mav_put_float(buf, 68, gps_alt);
_mav_put_float(buf, 72, left_servo_angle);
_mav_put_float(buf, 76, right_servo_angle);
_mav_put_float(buf, 80, nas_n);
_mav_put_float(buf, 84, nas_e);
_mav_put_float(buf, 88, nas_d);
_mav_put_float(buf, 92, nas_vn);
_mav_put_float(buf, 96, nas_ve);
_mav_put_float(buf, 100, nas_vd);
_mav_put_float(buf, 104, nas_qx);
_mav_put_float(buf, 108, nas_qy);
_mav_put_float(buf, 112, nas_qz);
_mav_put_float(buf, 116, nas_qw);
_mav_put_float(buf, 120, nas_bias_x);
_mav_put_float(buf, 124, nas_bias_y);
_mav_put_float(buf, 128, nas_bias_z);
_mav_put_float(buf, 132, wes_n);
_mav_put_float(buf, 136, wes_e);
_mav_put_float(buf, 140, battery_voltage);
_mav_put_float(buf, 144, cam_battery_voltage);
_mav_put_float(buf, 148, current_consumption);
_mav_put_float(buf, 152, temperature);
_mav_put_uint8_t(buf, 156, fmm_state);
_mav_put_uint8_t(buf, 157, nas_state);
_mav_put_uint8_t(buf, 158, wes_state);
_mav_put_uint8_t(buf, 159, gps_fix);
_mav_put_uint8_t(buf, 160, pin_nosecone);
_mav_put_int8_t(buf, 161, logger_error);
_mav_put_uint8_t(buf, 161, cutter_presence);
_mav_put_int8_t(buf, 162, logger_error);
memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_PAYLOAD_FLIGHT_TM_LEN);
#else
......@@ -430,7 +438,6 @@ static inline uint16_t mavlink_msg_payload_flight_tm_pack_chan(uint8_t system_id
packet.timestamp = timestamp;
packet.pressure_digi = pressure_digi;
packet.pressure_static = pressure_static;
packet.pressure_dpl = pressure_dpl;
packet.airspeed_pitot = airspeed_pitot;
packet.altitude_agl = altitude_agl;
packet.acc_x = acc_x;
......@@ -462,14 +469,16 @@ static inline uint16_t mavlink_msg_payload_flight_tm_pack_chan(uint8_t system_id
packet.nas_bias_z = nas_bias_z;
packet.wes_n = wes_n;
packet.wes_e = wes_e;
packet.vbat = vbat;
packet.vsupply_5v = vsupply_5v;
packet.battery_voltage = battery_voltage;
packet.cam_battery_voltage = cam_battery_voltage;
packet.current_consumption = current_consumption;
packet.temperature = temperature;
packet.fmm_state = fmm_state;
packet.nas_state = nas_state;
packet.wes_state = wes_state;
packet.gps_fix = gps_fix;
packet.pin_nosecone = pin_nosecone;
packet.cutter_presence = cutter_presence;
packet.logger_error = logger_error;
memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_PAYLOAD_FLIGHT_TM_LEN);
......@@ -489,7 +498,7 @@ static inline uint16_t mavlink_msg_payload_flight_tm_pack_chan(uint8_t system_id
*/
static inline uint16_t mavlink_msg_payload_flight_tm_encode(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg, const mavlink_payload_flight_tm_t* payload_flight_tm)
{
return mavlink_msg_payload_flight_tm_pack(system_id, component_id, msg, payload_flight_tm->timestamp, payload_flight_tm->fmm_state, payload_flight_tm->nas_state, payload_flight_tm->wes_state, payload_flight_tm->pressure_digi, payload_flight_tm->pressure_static, payload_flight_tm->pressure_dpl, payload_flight_tm->airspeed_pitot, payload_flight_tm->altitude_agl, payload_flight_tm->acc_x, payload_flight_tm->acc_y, payload_flight_tm->acc_z, payload_flight_tm->gyro_x, payload_flight_tm->gyro_y, payload_flight_tm->gyro_z, payload_flight_tm->mag_x, payload_flight_tm->mag_y, payload_flight_tm->mag_z, payload_flight_tm->gps_fix, payload_flight_tm->gps_lat, payload_flight_tm->gps_lon, payload_flight_tm->gps_alt, payload_flight_tm->left_servo_angle, payload_flight_tm->right_servo_angle, payload_flight_tm->nas_n, payload_flight_tm->nas_e, payload_flight_tm->nas_d, payload_flight_tm->nas_vn, payload_flight_tm->nas_ve, payload_flight_tm->nas_vd, payload_flight_tm->nas_qx, payload_flight_tm->nas_qy, payload_flight_tm->nas_qz, payload_flight_tm->nas_qw, payload_flight_tm->nas_bias_x, payload_flight_tm->nas_bias_y, payload_flight_tm->nas_bias_z, payload_flight_tm->wes_n, payload_flight_tm->wes_e, payload_flight_tm->pin_nosecone, payload_flight_tm->vbat, payload_flight_tm->vsupply_5v, payload_flight_tm->temperature, payload_flight_tm->logger_error);
return mavlink_msg_payload_flight_tm_pack(system_id, component_id, msg, payload_flight_tm->timestamp, payload_flight_tm->fmm_state, payload_flight_tm->nas_state, payload_flight_tm->wes_state, payload_flight_tm->pressure_digi, payload_flight_tm->pressure_static, payload_flight_tm->airspeed_pitot, payload_flight_tm->altitude_agl, payload_flight_tm->acc_x, payload_flight_tm->acc_y, payload_flight_tm->acc_z, payload_flight_tm->gyro_x, payload_flight_tm->gyro_y, payload_flight_tm->gyro_z, payload_flight_tm->mag_x, payload_flight_tm->mag_y, payload_flight_tm->mag_z, payload_flight_tm->gps_fix, payload_flight_tm->gps_lat, payload_flight_tm->gps_lon, payload_flight_tm->gps_alt, payload_flight_tm->left_servo_angle, payload_flight_tm->right_servo_angle, payload_flight_tm->nas_n, payload_flight_tm->nas_e, payload_flight_tm->nas_d, payload_flight_tm->nas_vn, payload_flight_tm->nas_ve, payload_flight_tm->nas_vd, payload_flight_tm->nas_qx, payload_flight_tm->nas_qy, payload_flight_tm->nas_qz, payload_flight_tm->nas_qw, payload_flight_tm->nas_bias_x, payload_flight_tm->nas_bias_y, payload_flight_tm->nas_bias_z, payload_flight_tm->wes_n, payload_flight_tm->wes_e, payload_flight_tm->pin_nosecone, payload_flight_tm->battery_voltage, payload_flight_tm->cam_battery_voltage, payload_flight_tm->current_consumption, payload_flight_tm->cutter_presence, payload_flight_tm->temperature, payload_flight_tm->logger_error);
}
/**
......@@ -503,7 +512,7 @@ static inline uint16_t mavlink_msg_payload_flight_tm_encode(uint8_t system_id, u
*/
static inline uint16_t mavlink_msg_payload_flight_tm_encode_chan(uint8_t system_id, uint8_t component_id, uint8_t chan, mavlink_message_t* msg, const mavlink_payload_flight_tm_t* payload_flight_tm)
{
return mavlink_msg_payload_flight_tm_pack_chan(system_id, component_id, chan, msg, payload_flight_tm->timestamp, payload_flight_tm->fmm_state, payload_flight_tm->nas_state, payload_flight_tm->wes_state, payload_flight_tm->pressure_digi, payload_flight_tm->pressure_static, payload_flight_tm->pressure_dpl, payload_flight_tm->airspeed_pitot, payload_flight_tm->altitude_agl, payload_flight_tm->acc_x, payload_flight_tm->acc_y, payload_flight_tm->acc_z, payload_flight_tm->gyro_x, payload_flight_tm->gyro_y, payload_flight_tm->gyro_z, payload_flight_tm->mag_x, payload_flight_tm->mag_y, payload_flight_tm->mag_z, payload_flight_tm->gps_fix, payload_flight_tm->gps_lat, payload_flight_tm->gps_lon, payload_flight_tm->gps_alt, payload_flight_tm->left_servo_angle, payload_flight_tm->right_servo_angle, payload_flight_tm->nas_n, payload_flight_tm->nas_e, payload_flight_tm->nas_d, payload_flight_tm->nas_vn, payload_flight_tm->nas_ve, payload_flight_tm->nas_vd, payload_flight_tm->nas_qx, payload_flight_tm->nas_qy, payload_flight_tm->nas_qz, payload_flight_tm->nas_qw, payload_flight_tm->nas_bias_x, payload_flight_tm->nas_bias_y, payload_flight_tm->nas_bias_z, payload_flight_tm->wes_n, payload_flight_tm->wes_e, payload_flight_tm->pin_nosecone, payload_flight_tm->vbat, payload_flight_tm->vsupply_5v, payload_flight_tm->temperature, payload_flight_tm->logger_error);
return mavlink_msg_payload_flight_tm_pack_chan(system_id, component_id, chan, msg, payload_flight_tm->timestamp, payload_flight_tm->fmm_state, payload_flight_tm->nas_state, payload_flight_tm->wes_state, payload_flight_tm->pressure_digi, payload_flight_tm->pressure_static, payload_flight_tm->airspeed_pitot, payload_flight_tm->altitude_agl, payload_flight_tm->acc_x, payload_flight_tm->acc_y, payload_flight_tm->acc_z, payload_flight_tm->gyro_x, payload_flight_tm->gyro_y, payload_flight_tm->gyro_z, payload_flight_tm->mag_x, payload_flight_tm->mag_y, payload_flight_tm->mag_z, payload_flight_tm->gps_fix, payload_flight_tm->gps_lat, payload_flight_tm->gps_lon, payload_flight_tm->gps_alt, payload_flight_tm->left_servo_angle, payload_flight_tm->right_servo_angle, payload_flight_tm->nas_n, payload_flight_tm->nas_e, payload_flight_tm->nas_d, payload_flight_tm->nas_vn, payload_flight_tm->nas_ve, payload_flight_tm->nas_vd, payload_flight_tm->nas_qx, payload_flight_tm->nas_qy, payload_flight_tm->nas_qz, payload_flight_tm->nas_qw, payload_flight_tm->nas_bias_x, payload_flight_tm->nas_bias_y, payload_flight_tm->nas_bias_z, payload_flight_tm->wes_n, payload_flight_tm->wes_e, payload_flight_tm->pin_nosecone, payload_flight_tm->battery_voltage, payload_flight_tm->cam_battery_voltage, payload_flight_tm->current_consumption, payload_flight_tm->cutter_presence, payload_flight_tm->temperature, payload_flight_tm->logger_error);
}
/**
......@@ -516,7 +525,6 @@ static inline uint16_t mavlink_msg_payload_flight_tm_encode_chan(uint8_t system_
* @param wes_state Wind Estimation System FSM State
* @param pressure_digi [Pa] Pressure from digital sensor
* @param pressure_static [Pa] Pressure from static port
* @param pressure_dpl [Pa] Pressure from deployment vane sensor
* @param airspeed_pitot [m/s] Pitot airspeed
* @param altitude_agl [m] Altitude above ground level
* @param acc_x [m/s^2] Acceleration on X axis (body)
......@@ -550,61 +558,64 @@ static inline uint16_t mavlink_msg_payload_flight_tm_encode_chan(uint8_t system_
* @param wes_n [m/s] Wind estimated north velocity
* @param wes_e [m/s] Wind estimated east velocity
* @param pin_nosecone Nosecone pin status (1 = connected, 0 = disconnected)
* @param vbat [V] Battery voltage
* @param vsupply_5v [V] Power supply 5V
* @param battery_voltage [V] Battery voltage
* @param cam_battery_voltage [V] Camera battery voltage
* @param current_consumption [A] Battery current
* @param cutter_presence Cutter presence status (1 = present, 0 = missing)
* @param temperature [degC] Temperature
* @param logger_error Logger error (0 = no error)
*/
#ifdef MAVLINK_USE_CONVENIENCE_FUNCTIONS
static inline void mavlink_msg_payload_flight_tm_send(mavlink_channel_t chan, uint64_t timestamp, uint8_t fmm_state, uint8_t nas_state, uint8_t wes_state, float pressure_digi, float pressure_static, float pressure_dpl, float airspeed_pitot, float altitude_agl, float acc_x, float acc_y, float acc_z, float gyro_x, float gyro_y, float gyro_z, float mag_x, float mag_y, float mag_z, uint8_t gps_fix, float gps_lat, float gps_lon, float gps_alt, float left_servo_angle, float right_servo_angle, float nas_n, float nas_e, float nas_d, float nas_vn, float nas_ve, float nas_vd, float nas_qx, float nas_qy, float nas_qz, float nas_qw, float nas_bias_x, float nas_bias_y, float nas_bias_z, float wes_n, float wes_e, uint8_t pin_nosecone, float vbat, float vsupply_5v, float temperature, int8_t logger_error)
static inline void mavlink_msg_payload_flight_tm_send(mavlink_channel_t chan, uint64_t timestamp, uint8_t fmm_state, uint8_t nas_state, uint8_t wes_state, float pressure_digi, float pressure_static, float airspeed_pitot, float altitude_agl, float acc_x, float acc_y, float acc_z, float gyro_x, float gyro_y, float gyro_z, float mag_x, float mag_y, float mag_z, uint8_t gps_fix, float gps_lat, float gps_lon, float gps_alt, float left_servo_angle, float right_servo_angle, float nas_n, float nas_e, float nas_d, float nas_vn, float nas_ve, float nas_vd, float nas_qx, float nas_qy, float nas_qz, float nas_qw, float nas_bias_x, float nas_bias_y, float nas_bias_z, float wes_n, float wes_e, uint8_t pin_nosecone, float battery_voltage, float cam_battery_voltage, float current_consumption, uint8_t cutter_presence, float temperature, int8_t logger_error)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char buf[MAVLINK_MSG_ID_PAYLOAD_FLIGHT_TM_LEN];
_mav_put_uint64_t(buf, 0, timestamp);
_mav_put_float(buf, 8, pressure_digi);
_mav_put_float(buf, 12, pressure_static);
_mav_put_float(buf, 16, pressure_dpl);
_mav_put_float(buf, 20, airspeed_pitot);
_mav_put_float(buf, 24, altitude_agl);
_mav_put_float(buf, 28, acc_x);
_mav_put_float(buf, 32, acc_y);
_mav_put_float(buf, 36, acc_z);
_mav_put_float(buf, 40, gyro_x);
_mav_put_float(buf, 44, gyro_y);
_mav_put_float(buf, 48, gyro_z);
_mav_put_float(buf, 52, mag_x);
_mav_put_float(buf, 56, mag_y);
_mav_put_float(buf, 60, mag_z);
_mav_put_float(buf, 64, gps_lat);
_mav_put_float(buf, 68, gps_lon);
_mav_put_float(buf, 72, gps_alt);
_mav_put_float(buf, 76, left_servo_angle);
_mav_put_float(buf, 80, right_servo_angle);
_mav_put_float(buf, 84, nas_n);
_mav_put_float(buf, 88, nas_e);
_mav_put_float(buf, 92, nas_d);
_mav_put_float(buf, 96, nas_vn);
_mav_put_float(buf, 100, nas_ve);
_mav_put_float(buf, 104, nas_vd);
_mav_put_float(buf, 108, nas_qx);
_mav_put_float(buf, 112, nas_qy);
_mav_put_float(buf, 116, nas_qz);
_mav_put_float(buf, 120, nas_qw);
_mav_put_float(buf, 124, nas_bias_x);
_mav_put_float(buf, 128, nas_bias_y);
_mav_put_float(buf, 132, nas_bias_z);
_mav_put_float(buf, 136, wes_n);
_mav_put_float(buf, 140, wes_e);
_mav_put_float(buf, 144, vbat);
_mav_put_float(buf, 148, vsupply_5v);
_mav_put_float(buf, 16, airspeed_pitot);
_mav_put_float(buf, 20, altitude_agl);
_mav_put_float(buf, 24, acc_x);
_mav_put_float(buf, 28, acc_y);
_mav_put_float(buf, 32, acc_z);
_mav_put_float(buf, 36, gyro_x);
_mav_put_float(buf, 40, gyro_y);
_mav_put_float(buf, 44, gyro_z);
_mav_put_float(buf, 48, mag_x);
_mav_put_float(buf, 52, mag_y);
_mav_put_float(buf, 56, mag_z);
_mav_put_float(buf, 60, gps_lat);
_mav_put_float(buf, 64, gps_lon);
_mav_put_float(buf, 68, gps_alt);
_mav_put_float(buf, 72, left_servo_angle);
_mav_put_float(buf, 76, right_servo_angle);
_mav_put_float(buf, 80, nas_n);
_mav_put_float(buf, 84, nas_e);
_mav_put_float(buf, 88, nas_d);
_mav_put_float(buf, 92, nas_vn);
_mav_put_float(buf, 96, nas_ve);
_mav_put_float(buf, 100, nas_vd);
_mav_put_float(buf, 104, nas_qx);
_mav_put_float(buf, 108, nas_qy);
_mav_put_float(buf, 112, nas_qz);
_mav_put_float(buf, 116, nas_qw);
_mav_put_float(buf, 120, nas_bias_x);
_mav_put_float(buf, 124, nas_bias_y);
_mav_put_float(buf, 128, nas_bias_z);
_mav_put_float(buf, 132, wes_n);
_mav_put_float(buf, 136, wes_e);
_mav_put_float(buf, 140, battery_voltage);
_mav_put_float(buf, 144, cam_battery_voltage);
_mav_put_float(buf, 148, current_consumption);
_mav_put_float(buf, 152, temperature);
_mav_put_uint8_t(buf, 156, fmm_state);
_mav_put_uint8_t(buf, 157, nas_state);
_mav_put_uint8_t(buf, 158, wes_state);
_mav_put_uint8_t(buf, 159, gps_fix);
_mav_put_uint8_t(buf, 160, pin_nosecone);
_mav_put_int8_t(buf, 161, logger_error);
_mav_put_uint8_t(buf, 161, cutter_presence);
_mav_put_int8_t(buf, 162, logger_error);
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_PAYLOAD_FLIGHT_TM, buf, MAVLINK_MSG_ID_PAYLOAD_FLIGHT_TM_MIN_LEN, MAVLINK_MSG_ID_PAYLOAD_FLIGHT_TM_LEN, MAVLINK_MSG_ID_PAYLOAD_FLIGHT_TM_CRC);
#else
......@@ -612,7 +623,6 @@ static inline void mavlink_msg_payload_flight_tm_send(mavlink_channel_t chan, ui
packet.timestamp = timestamp;
packet.pressure_digi = pressure_digi;
packet.pressure_static = pressure_static;
packet.pressure_dpl = pressure_dpl;
packet.airspeed_pitot = airspeed_pitot;
packet.altitude_agl = altitude_agl;
packet.acc_x = acc_x;
......@@ -644,14 +654,16 @@ static inline void mavlink_msg_payload_flight_tm_send(mavlink_channel_t chan, ui
packet.nas_bias_z = nas_bias_z;
packet.wes_n = wes_n;
packet.wes_e = wes_e;
packet.vbat = vbat;
packet.vsupply_5v = vsupply_5v;
packet.battery_voltage = battery_voltage;
packet.cam_battery_voltage = cam_battery_voltage;
packet.current_consumption = current_consumption;
packet.temperature = temperature;
packet.fmm_state = fmm_state;
packet.nas_state = nas_state;
packet.wes_state = wes_state;
packet.gps_fix = gps_fix;
packet.pin_nosecone = pin_nosecone;
packet.cutter_presence = cutter_presence;
packet.logger_error = logger_error;
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_PAYLOAD_FLIGHT_TM, (const char *)&packet, MAVLINK_MSG_ID_PAYLOAD_FLIGHT_TM_MIN_LEN, MAVLINK_MSG_ID_PAYLOAD_FLIGHT_TM_LEN, MAVLINK_MSG_ID_PAYLOAD_FLIGHT_TM_CRC);
......@@ -666,7 +678,7 @@ static inline void mavlink_msg_payload_flight_tm_send(mavlink_channel_t chan, ui
static inline void mavlink_msg_payload_flight_tm_send_struct(mavlink_channel_t chan, const mavlink_payload_flight_tm_t* payload_flight_tm)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
mavlink_msg_payload_flight_tm_send(chan, payload_flight_tm->timestamp, payload_flight_tm->fmm_state, payload_flight_tm->nas_state, payload_flight_tm->wes_state, payload_flight_tm->pressure_digi, payload_flight_tm->pressure_static, payload_flight_tm->pressure_dpl, payload_flight_tm->airspeed_pitot, payload_flight_tm->altitude_agl, payload_flight_tm->acc_x, payload_flight_tm->acc_y, payload_flight_tm->acc_z, payload_flight_tm->gyro_x, payload_flight_tm->gyro_y, payload_flight_tm->gyro_z, payload_flight_tm->mag_x, payload_flight_tm->mag_y, payload_flight_tm->mag_z, payload_flight_tm->gps_fix, payload_flight_tm->gps_lat, payload_flight_tm->gps_lon, payload_flight_tm->gps_alt, payload_flight_tm->left_servo_angle, payload_flight_tm->right_servo_angle, payload_flight_tm->nas_n, payload_flight_tm->nas_e, payload_flight_tm->nas_d, payload_flight_tm->nas_vn, payload_flight_tm->nas_ve, payload_flight_tm->nas_vd, payload_flight_tm->nas_qx, payload_flight_tm->nas_qy, payload_flight_tm->nas_qz, payload_flight_tm->nas_qw, payload_flight_tm->nas_bias_x, payload_flight_tm->nas_bias_y, payload_flight_tm->nas_bias_z, payload_flight_tm->wes_n, payload_flight_tm->wes_e, payload_flight_tm->pin_nosecone, payload_flight_tm->vbat, payload_flight_tm->vsupply_5v, payload_flight_tm->temperature, payload_flight_tm->logger_error);
mavlink_msg_payload_flight_tm_send(chan, payload_flight_tm->timestamp, payload_flight_tm->fmm_state, payload_flight_tm->nas_state, payload_flight_tm->wes_state, payload_flight_tm->pressure_digi, payload_flight_tm->pressure_static, payload_flight_tm->airspeed_pitot, payload_flight_tm->altitude_agl, payload_flight_tm->acc_x, payload_flight_tm->acc_y, payload_flight_tm->acc_z, payload_flight_tm->gyro_x, payload_flight_tm->gyro_y, payload_flight_tm->gyro_z, payload_flight_tm->mag_x, payload_flight_tm->mag_y, payload_flight_tm->mag_z, payload_flight_tm->gps_fix, payload_flight_tm->gps_lat, payload_flight_tm->gps_lon, payload_flight_tm->gps_alt, payload_flight_tm->left_servo_angle, payload_flight_tm->right_servo_angle, payload_flight_tm->nas_n, payload_flight_tm->nas_e, payload_flight_tm->nas_d, payload_flight_tm->nas_vn, payload_flight_tm->nas_ve, payload_flight_tm->nas_vd, payload_flight_tm->nas_qx, payload_flight_tm->nas_qy, payload_flight_tm->nas_qz, payload_flight_tm->nas_qw, payload_flight_tm->nas_bias_x, payload_flight_tm->nas_bias_y, payload_flight_tm->nas_bias_z, payload_flight_tm->wes_n, payload_flight_tm->wes_e, payload_flight_tm->pin_nosecone, payload_flight_tm->battery_voltage, payload_flight_tm->cam_battery_voltage, payload_flight_tm->current_consumption, payload_flight_tm->cutter_presence, payload_flight_tm->temperature, payload_flight_tm->logger_error);
#else
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_PAYLOAD_FLIGHT_TM, (const char *)payload_flight_tm, MAVLINK_MSG_ID_PAYLOAD_FLIGHT_TM_MIN_LEN, MAVLINK_MSG_ID_PAYLOAD_FLIGHT_TM_LEN, MAVLINK_MSG_ID_PAYLOAD_FLIGHT_TM_CRC);
#endif
......@@ -680,54 +692,55 @@ static inline void mavlink_msg_payload_flight_tm_send_struct(mavlink_channel_t c
is usually the receive buffer for the channel, and allows a reply to an
incoming message with minimum stack space usage.
*/
static inline void mavlink_msg_payload_flight_tm_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint64_t timestamp, uint8_t fmm_state, uint8_t nas_state, uint8_t wes_state, float pressure_digi, float pressure_static, float pressure_dpl, float airspeed_pitot, float altitude_agl, float acc_x, float acc_y, float acc_z, float gyro_x, float gyro_y, float gyro_z, float mag_x, float mag_y, float mag_z, uint8_t gps_fix, float gps_lat, float gps_lon, float gps_alt, float left_servo_angle, float right_servo_angle, float nas_n, float nas_e, float nas_d, float nas_vn, float nas_ve, float nas_vd, float nas_qx, float nas_qy, float nas_qz, float nas_qw, float nas_bias_x, float nas_bias_y, float nas_bias_z, float wes_n, float wes_e, uint8_t pin_nosecone, float vbat, float vsupply_5v, float temperature, int8_t logger_error)
static inline void mavlink_msg_payload_flight_tm_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint64_t timestamp, uint8_t fmm_state, uint8_t nas_state, uint8_t wes_state, float pressure_digi, float pressure_static, float airspeed_pitot, float altitude_agl, float acc_x, float acc_y, float acc_z, float gyro_x, float gyro_y, float gyro_z, float mag_x, float mag_y, float mag_z, uint8_t gps_fix, float gps_lat, float gps_lon, float gps_alt, float left_servo_angle, float right_servo_angle, float nas_n, float nas_e, float nas_d, float nas_vn, float nas_ve, float nas_vd, float nas_qx, float nas_qy, float nas_qz, float nas_qw, float nas_bias_x, float nas_bias_y, float nas_bias_z, float wes_n, float wes_e, uint8_t pin_nosecone, float battery_voltage, float cam_battery_voltage, float current_consumption, uint8_t cutter_presence, float temperature, int8_t logger_error)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char *buf = (char *)msgbuf;
_mav_put_uint64_t(buf, 0, timestamp);
_mav_put_float(buf, 8, pressure_digi);
_mav_put_float(buf, 12, pressure_static);
_mav_put_float(buf, 16, pressure_dpl);
_mav_put_float(buf, 20, airspeed_pitot);
_mav_put_float(buf, 24, altitude_agl);
_mav_put_float(buf, 28, acc_x);
_mav_put_float(buf, 32, acc_y);
_mav_put_float(buf, 36, acc_z);
_mav_put_float(buf, 40, gyro_x);
_mav_put_float(buf, 44, gyro_y);
_mav_put_float(buf, 48, gyro_z);
_mav_put_float(buf, 52, mag_x);
_mav_put_float(buf, 56, mag_y);
_mav_put_float(buf, 60, mag_z);
_mav_put_float(buf, 64, gps_lat);
_mav_put_float(buf, 68, gps_lon);
_mav_put_float(buf, 72, gps_alt);
_mav_put_float(buf, 76, left_servo_angle);
_mav_put_float(buf, 80, right_servo_angle);
_mav_put_float(buf, 84, nas_n);
_mav_put_float(buf, 88, nas_e);
_mav_put_float(buf, 92, nas_d);
_mav_put_float(buf, 96, nas_vn);
_mav_put_float(buf, 100, nas_ve);
_mav_put_float(buf, 104, nas_vd);
_mav_put_float(buf, 108, nas_qx);
_mav_put_float(buf, 112, nas_qy);
_mav_put_float(buf, 116, nas_qz);
_mav_put_float(buf, 120, nas_qw);
_mav_put_float(buf, 124, nas_bias_x);
_mav_put_float(buf, 128, nas_bias_y);
_mav_put_float(buf, 132, nas_bias_z);
_mav_put_float(buf, 136, wes_n);
_mav_put_float(buf, 140, wes_e);
_mav_put_float(buf, 144, vbat);
_mav_put_float(buf, 148, vsupply_5v);
_mav_put_float(buf, 16, airspeed_pitot);
_mav_put_float(buf, 20, altitude_agl);
_mav_put_float(buf, 24, acc_x);
_mav_put_float(buf, 28, acc_y);
_mav_put_float(buf, 32, acc_z);
_mav_put_float(buf, 36, gyro_x);
_mav_put_float(buf, 40, gyro_y);
_mav_put_float(buf, 44, gyro_z);
_mav_put_float(buf, 48, mag_x);
_mav_put_float(buf, 52, mag_y);
_mav_put_float(buf, 56, mag_z);
_mav_put_float(buf, 60, gps_lat);
_mav_put_float(buf, 64, gps_lon);
_mav_put_float(buf, 68, gps_alt);
_mav_put_float(buf, 72, left_servo_angle);
_mav_put_float(buf, 76, right_servo_angle);
_mav_put_float(buf, 80, nas_n);
_mav_put_float(buf, 84, nas_e);
_mav_put_float(buf, 88, nas_d);
_mav_put_float(buf, 92, nas_vn);
_mav_put_float(buf, 96, nas_ve);
_mav_put_float(buf, 100, nas_vd);
_mav_put_float(buf, 104, nas_qx);
_mav_put_float(buf, 108, nas_qy);
_mav_put_float(buf, 112, nas_qz);
_mav_put_float(buf, 116, nas_qw);
_mav_put_float(buf, 120, nas_bias_x);
_mav_put_float(buf, 124, nas_bias_y);
_mav_put_float(buf, 128, nas_bias_z);
_mav_put_float(buf, 132, wes_n);
_mav_put_float(buf, 136, wes_e);
_mav_put_float(buf, 140, battery_voltage);
_mav_put_float(buf, 144, cam_battery_voltage);
_mav_put_float(buf, 148, current_consumption);
_mav_put_float(buf, 152, temperature);
_mav_put_uint8_t(buf, 156, fmm_state);
_mav_put_uint8_t(buf, 157, nas_state);
_mav_put_uint8_t(buf, 158, wes_state);
_mav_put_uint8_t(buf, 159, gps_fix);
_mav_put_uint8_t(buf, 160, pin_nosecone);
_mav_put_int8_t(buf, 161, logger_error);
_mav_put_uint8_t(buf, 161, cutter_presence);
_mav_put_int8_t(buf, 162, logger_error);
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_PAYLOAD_FLIGHT_TM, buf, MAVLINK_MSG_ID_PAYLOAD_FLIGHT_TM_MIN_LEN, MAVLINK_MSG_ID_PAYLOAD_FLIGHT_TM_LEN, MAVLINK_MSG_ID_PAYLOAD_FLIGHT_TM_CRC);
#else
......@@ -735,7 +748,6 @@ static inline void mavlink_msg_payload_flight_tm_send_buf(mavlink_message_t *msg
packet->timestamp = timestamp;
packet->pressure_digi = pressure_digi;
packet->pressure_static = pressure_static;
packet->pressure_dpl = pressure_dpl;
packet->airspeed_pitot = airspeed_pitot;
packet->altitude_agl = altitude_agl;
packet->acc_x = acc_x;
......@@ -767,14 +779,16 @@ static inline void mavlink_msg_payload_flight_tm_send_buf(mavlink_message_t *msg
packet->nas_bias_z = nas_bias_z;
packet->wes_n = wes_n;
packet->wes_e = wes_e;
packet->vbat = vbat;
packet->vsupply_5v = vsupply_5v;
packet->battery_voltage = battery_voltage;
packet->cam_battery_voltage = cam_battery_voltage;
packet->current_consumption = current_consumption;
packet->temperature = temperature;
packet->fmm_state = fmm_state;
packet->nas_state = nas_state;
packet->wes_state = wes_state;
packet->gps_fix = gps_fix;
packet->pin_nosecone = pin_nosecone;
packet->cutter_presence = cutter_presence;
packet->logger_error = logger_error;
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_PAYLOAD_FLIGHT_TM, (const char *)packet, MAVLINK_MSG_ID_PAYLOAD_FLIGHT_TM_MIN_LEN, MAVLINK_MSG_ID_PAYLOAD_FLIGHT_TM_LEN, MAVLINK_MSG_ID_PAYLOAD_FLIGHT_TM_CRC);
......@@ -847,16 +861,6 @@ static inline float mavlink_msg_payload_flight_tm_get_pressure_static(const mavl
return _MAV_RETURN_float(msg, 12);
}
/**
* @brief Get field pressure_dpl from payload_flight_tm message
*
* @return [Pa] Pressure from deployment vane sensor
*/
static inline float mavlink_msg_payload_flight_tm_get_pressure_dpl(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 16);
}
/**
* @brief Get field airspeed_pitot from payload_flight_tm message
*
......@@ -864,7 +868,7 @@ static inline float mavlink_msg_payload_flight_tm_get_pressure_dpl(const mavlink
*/
static inline float mavlink_msg_payload_flight_tm_get_airspeed_pitot(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 20);
return _MAV_RETURN_float(msg, 16);
}
/**
......@@ -874,7 +878,7 @@ static inline float mavlink_msg_payload_flight_tm_get_airspeed_pitot(const mavli
*/
static inline float mavlink_msg_payload_flight_tm_get_altitude_agl(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 24);
return _MAV_RETURN_float(msg, 20);
}
/**
......@@ -884,7 +888,7 @@ static inline float mavlink_msg_payload_flight_tm_get_altitude_agl(const mavlink
*/
static inline float mavlink_msg_payload_flight_tm_get_acc_x(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 28);
return _MAV_RETURN_float(msg, 24);
}
/**
......@@ -894,7 +898,7 @@ static inline float mavlink_msg_payload_flight_tm_get_acc_x(const mavlink_messag
*/
static inline float mavlink_msg_payload_flight_tm_get_acc_y(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 32);
return _MAV_RETURN_float(msg, 28);
}
/**
......@@ -904,7 +908,7 @@ static inline float mavlink_msg_payload_flight_tm_get_acc_y(const mavlink_messag
*/
static inline float mavlink_msg_payload_flight_tm_get_acc_z(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 36);
return _MAV_RETURN_float(msg, 32);
}
/**
......@@ -914,7 +918,7 @@ static inline float mavlink_msg_payload_flight_tm_get_acc_z(const mavlink_messag
*/
static inline float mavlink_msg_payload_flight_tm_get_gyro_x(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 40);
return _MAV_RETURN_float(msg, 36);
}
/**
......@@ -924,7 +928,7 @@ static inline float mavlink_msg_payload_flight_tm_get_gyro_x(const mavlink_messa
*/
static inline float mavlink_msg_payload_flight_tm_get_gyro_y(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 44);
return _MAV_RETURN_float(msg, 40);
}
/**
......@@ -934,7 +938,7 @@ static inline float mavlink_msg_payload_flight_tm_get_gyro_y(const mavlink_messa
*/
static inline float mavlink_msg_payload_flight_tm_get_gyro_z(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 48);
return _MAV_RETURN_float(msg, 44);
}
/**
......@@ -944,7 +948,7 @@ static inline float mavlink_msg_payload_flight_tm_get_gyro_z(const mavlink_messa
*/
static inline float mavlink_msg_payload_flight_tm_get_mag_x(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 52);
return _MAV_RETURN_float(msg, 48);
}
/**
......@@ -954,7 +958,7 @@ static inline float mavlink_msg_payload_flight_tm_get_mag_x(const mavlink_messag
*/
static inline float mavlink_msg_payload_flight_tm_get_mag_y(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 56);
return _MAV_RETURN_float(msg, 52);
}
/**
......@@ -964,7 +968,7 @@ static inline float mavlink_msg_payload_flight_tm_get_mag_y(const mavlink_messag
*/
static inline float mavlink_msg_payload_flight_tm_get_mag_z(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 60);
return _MAV_RETURN_float(msg, 56);
}
/**
......@@ -984,7 +988,7 @@ static inline uint8_t mavlink_msg_payload_flight_tm_get_gps_fix(const mavlink_me
*/
static inline float mavlink_msg_payload_flight_tm_get_gps_lat(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 64);
return _MAV_RETURN_float(msg, 60);
}
/**
......@@ -994,7 +998,7 @@ static inline float mavlink_msg_payload_flight_tm_get_gps_lat(const mavlink_mess
*/
static inline float mavlink_msg_payload_flight_tm_get_gps_lon(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 68);
return _MAV_RETURN_float(msg, 64);
}
/**
......@@ -1004,7 +1008,7 @@ static inline float mavlink_msg_payload_flight_tm_get_gps_lon(const mavlink_mess
*/
static inline float mavlink_msg_payload_flight_tm_get_gps_alt(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 72);
return _MAV_RETURN_float(msg, 68);
}
/**
......@@ -1014,7 +1018,7 @@ static inline float mavlink_msg_payload_flight_tm_get_gps_alt(const mavlink_mess
*/
static inline float mavlink_msg_payload_flight_tm_get_left_servo_angle(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 76);
return _MAV_RETURN_float(msg, 72);
}
/**
......@@ -1024,7 +1028,7 @@ static inline float mavlink_msg_payload_flight_tm_get_left_servo_angle(const mav
*/
static inline float mavlink_msg_payload_flight_tm_get_right_servo_angle(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 80);
return _MAV_RETURN_float(msg, 76);
}
/**
......@@ -1034,7 +1038,7 @@ static inline float mavlink_msg_payload_flight_tm_get_right_servo_angle(const ma
*/
static inline float mavlink_msg_payload_flight_tm_get_nas_n(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 84);
return _MAV_RETURN_float(msg, 80);
}
/**
......@@ -1044,7 +1048,7 @@ static inline float mavlink_msg_payload_flight_tm_get_nas_n(const mavlink_messag
*/
static inline float mavlink_msg_payload_flight_tm_get_nas_e(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 88);
return _MAV_RETURN_float(msg, 84);
}
/**
......@@ -1054,7 +1058,7 @@ static inline float mavlink_msg_payload_flight_tm_get_nas_e(const mavlink_messag
*/
static inline float mavlink_msg_payload_flight_tm_get_nas_d(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 92);
return _MAV_RETURN_float(msg, 88);
}
/**
......@@ -1064,7 +1068,7 @@ static inline float mavlink_msg_payload_flight_tm_get_nas_d(const mavlink_messag
*/
static inline float mavlink_msg_payload_flight_tm_get_nas_vn(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 96);
return _MAV_RETURN_float(msg, 92);
}
/**
......@@ -1074,7 +1078,7 @@ static inline float mavlink_msg_payload_flight_tm_get_nas_vn(const mavlink_messa
*/
static inline float mavlink_msg_payload_flight_tm_get_nas_ve(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 100);
return _MAV_RETURN_float(msg, 96);
}
/**
......@@ -1084,7 +1088,7 @@ static inline float mavlink_msg_payload_flight_tm_get_nas_ve(const mavlink_messa
*/
static inline float mavlink_msg_payload_flight_tm_get_nas_vd(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 104);
return _MAV_RETURN_float(msg, 100);
}
/**
......@@ -1094,7 +1098,7 @@ static inline float mavlink_msg_payload_flight_tm_get_nas_vd(const mavlink_messa
*/
static inline float mavlink_msg_payload_flight_tm_get_nas_qx(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 108);
return _MAV_RETURN_float(msg, 104);
}
/**
......@@ -1104,7 +1108,7 @@ static inline float mavlink_msg_payload_flight_tm_get_nas_qx(const mavlink_messa
*/
static inline float mavlink_msg_payload_flight_tm_get_nas_qy(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 112);
return _MAV_RETURN_float(msg, 108);
}
/**
......@@ -1114,7 +1118,7 @@ static inline float mavlink_msg_payload_flight_tm_get_nas_qy(const mavlink_messa
*/
static inline float mavlink_msg_payload_flight_tm_get_nas_qz(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 116);
return _MAV_RETURN_float(msg, 112);
}
/**
......@@ -1124,7 +1128,7 @@ static inline float mavlink_msg_payload_flight_tm_get_nas_qz(const mavlink_messa
*/
static inline float mavlink_msg_payload_flight_tm_get_nas_qw(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 120);
return _MAV_RETURN_float(msg, 116);
}
/**
......@@ -1134,7 +1138,7 @@ static inline float mavlink_msg_payload_flight_tm_get_nas_qw(const mavlink_messa
*/
static inline float mavlink_msg_payload_flight_tm_get_nas_bias_x(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 124);
return _MAV_RETURN_float(msg, 120);
}
/**
......@@ -1144,7 +1148,7 @@ static inline float mavlink_msg_payload_flight_tm_get_nas_bias_x(const mavlink_m
*/
static inline float mavlink_msg_payload_flight_tm_get_nas_bias_y(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 128);
return _MAV_RETURN_float(msg, 124);
}
/**
......@@ -1154,7 +1158,7 @@ static inline float mavlink_msg_payload_flight_tm_get_nas_bias_y(const mavlink_m
*/
static inline float mavlink_msg_payload_flight_tm_get_nas_bias_z(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 132);
return _MAV_RETURN_float(msg, 128);
}
/**
......@@ -1164,7 +1168,7 @@ static inline float mavlink_msg_payload_flight_tm_get_nas_bias_z(const mavlink_m
*/
static inline float mavlink_msg_payload_flight_tm_get_wes_n(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 136);
return _MAV_RETURN_float(msg, 132);
}
/**
......@@ -1174,7 +1178,7 @@ static inline float mavlink_msg_payload_flight_tm_get_wes_n(const mavlink_messag
*/
static inline float mavlink_msg_payload_flight_tm_get_wes_e(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 140);
return _MAV_RETURN_float(msg, 136);
}
/**
......@@ -1188,25 +1192,45 @@ static inline uint8_t mavlink_msg_payload_flight_tm_get_pin_nosecone(const mavli
}
/**
* @brief Get field vbat from payload_flight_tm message
* @brief Get field battery_voltage from payload_flight_tm message
*
* @return [V] Battery voltage
*/
static inline float mavlink_msg_payload_flight_tm_get_vbat(const mavlink_message_t* msg)
static inline float mavlink_msg_payload_flight_tm_get_battery_voltage(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 140);
}
/**
* @brief Get field cam_battery_voltage from payload_flight_tm message
*
* @return [V] Camera battery voltage
*/
static inline float mavlink_msg_payload_flight_tm_get_cam_battery_voltage(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 144);
}
/**
* @brief Get field vsupply_5v from payload_flight_tm message
* @brief Get field current_consumption from payload_flight_tm message
*
* @return [V] Power supply 5V
* @return [A] Battery current
*/
static inline float mavlink_msg_payload_flight_tm_get_vsupply_5v(const mavlink_message_t* msg)
static inline float mavlink_msg_payload_flight_tm_get_current_consumption(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 148);
}
/**
* @brief Get field cutter_presence from payload_flight_tm message
*
* @return Cutter presence status (1 = present, 0 = missing)
*/
static inline uint8_t mavlink_msg_payload_flight_tm_get_cutter_presence(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint8_t(msg, 161);
}
/**
* @brief Get field temperature from payload_flight_tm message
*
......@@ -1224,7 +1248,7 @@ static inline float mavlink_msg_payload_flight_tm_get_temperature(const mavlink_
*/
static inline int8_t mavlink_msg_payload_flight_tm_get_logger_error(const mavlink_message_t* msg)
{
return _MAV_RETURN_int8_t(msg, 161);
return _MAV_RETURN_int8_t(msg, 162);
}
/**
......@@ -1239,7 +1263,6 @@ static inline void mavlink_msg_payload_flight_tm_decode(const mavlink_message_t*
payload_flight_tm->timestamp = mavlink_msg_payload_flight_tm_get_timestamp(msg);
payload_flight_tm->pressure_digi = mavlink_msg_payload_flight_tm_get_pressure_digi(msg);
payload_flight_tm->pressure_static = mavlink_msg_payload_flight_tm_get_pressure_static(msg);
payload_flight_tm->pressure_dpl = mavlink_msg_payload_flight_tm_get_pressure_dpl(msg);
payload_flight_tm->airspeed_pitot = mavlink_msg_payload_flight_tm_get_airspeed_pitot(msg);
payload_flight_tm->altitude_agl = mavlink_msg_payload_flight_tm_get_altitude_agl(msg);
payload_flight_tm->acc_x = mavlink_msg_payload_flight_tm_get_acc_x(msg);
......@@ -1271,14 +1294,16 @@ static inline void mavlink_msg_payload_flight_tm_decode(const mavlink_message_t*
payload_flight_tm->nas_bias_z = mavlink_msg_payload_flight_tm_get_nas_bias_z(msg);
payload_flight_tm->wes_n = mavlink_msg_payload_flight_tm_get_wes_n(msg);
payload_flight_tm->wes_e = mavlink_msg_payload_flight_tm_get_wes_e(msg);
payload_flight_tm->vbat = mavlink_msg_payload_flight_tm_get_vbat(msg);
payload_flight_tm->vsupply_5v = mavlink_msg_payload_flight_tm_get_vsupply_5v(msg);
payload_flight_tm->battery_voltage = mavlink_msg_payload_flight_tm_get_battery_voltage(msg);
payload_flight_tm->cam_battery_voltage = mavlink_msg_payload_flight_tm_get_cam_battery_voltage(msg);
payload_flight_tm->current_consumption = mavlink_msg_payload_flight_tm_get_current_consumption(msg);
payload_flight_tm->temperature = mavlink_msg_payload_flight_tm_get_temperature(msg);
payload_flight_tm->fmm_state = mavlink_msg_payload_flight_tm_get_fmm_state(msg);
payload_flight_tm->nas_state = mavlink_msg_payload_flight_tm_get_nas_state(msg);
payload_flight_tm->wes_state = mavlink_msg_payload_flight_tm_get_wes_state(msg);
payload_flight_tm->gps_fix = mavlink_msg_payload_flight_tm_get_gps_fix(msg);
payload_flight_tm->pin_nosecone = mavlink_msg_payload_flight_tm_get_pin_nosecone(msg);
payload_flight_tm->cutter_presence = mavlink_msg_payload_flight_tm_get_cutter_presence(msg);
payload_flight_tm->logger_error = mavlink_msg_payload_flight_tm_get_logger_error(msg);
#else
uint8_t len = msg->len < MAVLINK_MSG_ID_PAYLOAD_FLIGHT_TM_LEN? msg->len : MAVLINK_MSG_ID_PAYLOAD_FLIGHT_TM_LEN;
......
mavlink_lib/gemini/mavlink_msg_receiver_tm.h
View file @ 7abedf97
......@@ -6,19 +6,34 @@
typedef struct __mavlink_receiver_tm_t {
uint64_t timestamp; /*< [us] Timestamp*/
uint64_t rx_bitrate; /*< [kb/s] Rx bitrate*/
uint64_t tx_bitrate; /*< [kb/s] Tx bitrate*/
float rssi; /*< [dBm] Rssi*/
float fei; /*< [Hz] Fei*/
float main_rx_rssi; /*< [dBm] Receive RSSI*/
float main_rx_fei; /*< [Hz] Receive frequency error index*/
float payload_rx_rssi; /*< [dBm] Receive RSSI*/
float payload_rx_fei; /*< [Hz] Receive frequency error index*/
float battery_voltage; /*< [V] Battery voltage*/
uint16_t main_packet_tx_error_count; /*< Number of errors during send*/
uint16_t main_tx_bitrate; /*< [b/s] Send bitrate*/
uint16_t main_packet_rx_success_count; /*< Number of succesfull received mavlink packets*/
uint16_t main_packet_rx_drop_count; /*< Number of dropped mavlink packets*/
uint16_t main_rx_bitrate; /*< [b/s] Receive bitrate*/
uint16_t payload_packet_tx_error_count; /*< Number of errors during send*/
uint16_t payload_tx_bitrate; /*< [b/s] Send bitrate*/
uint16_t payload_packet_rx_success_count; /*< Number of succesfull received mavlink packets*/
uint16_t payload_packet_rx_drop_count; /*< Number of dropped mavlink packets*/
uint16_t payload_rx_bitrate; /*< [b/s] Receive bitrate*/
uint8_t main_radio_present; /*< Boolean indicating the presence of the main radio*/
uint8_t payload_radio_present; /*< Boolean indicating the presence of the payload radio*/
uint8_t ethernet_present; /*< Boolean indicating the presence of the ethernet module*/
uint8_t ethernet_status; /*< Status flag indicating the status of the ethernet PHY*/
} mavlink_receiver_tm_t;
#define MAVLINK_MSG_ID_RECEIVER_TM_LEN 32
#define MAVLINK_MSG_ID_RECEIVER_TM_MIN_LEN 32
#define MAVLINK_MSG_ID_150_LEN 32
#define MAVLINK_MSG_ID_150_MIN_LEN 32
#define MAVLINK_MSG_ID_RECEIVER_TM_LEN 52
#define MAVLINK_MSG_ID_RECEIVER_TM_MIN_LEN 52
#define MAVLINK_MSG_ID_150_LEN 52
#define MAVLINK_MSG_ID_150_MIN_LEN 52
#define MAVLINK_MSG_ID_RECEIVER_TM_CRC 109
#define MAVLINK_MSG_ID_150_CRC 109
#define MAVLINK_MSG_ID_RECEIVER_TM_CRC 117
#define MAVLINK_MSG_ID_150_CRC 117
......@@ -26,23 +41,53 @@ typedef struct __mavlink_receiver_tm_t {
#define MAVLINK_MESSAGE_INFO_RECEIVER_TM { \
150, \
"RECEIVER_TM", \
5, \
20, \
{ { "timestamp", NULL, MAVLINK_TYPE_UINT64_T, 0, 0, offsetof(mavlink_receiver_tm_t, timestamp) }, \
{ "rssi", NULL, MAVLINK_TYPE_FLOAT, 0, 24, offsetof(mavlink_receiver_tm_t, rssi) }, \
{ "fei", NULL, MAVLINK_TYPE_FLOAT, 0, 28, offsetof(mavlink_receiver_tm_t, fei) }, \
{ "rx_bitrate", NULL, MAVLINK_TYPE_UINT64_T, 0, 8, offsetof(mavlink_receiver_tm_t, rx_bitrate) }, \
{ "tx_bitrate", NULL, MAVLINK_TYPE_UINT64_T, 0, 16, offsetof(mavlink_receiver_tm_t, tx_bitrate) }, \
{ "main_radio_present", NULL, MAVLINK_TYPE_UINT8_T, 0, 48, offsetof(mavlink_receiver_tm_t, main_radio_present) }, \
{ "main_packet_tx_error_count", NULL, MAVLINK_TYPE_UINT16_T, 0, 28, offsetof(mavlink_receiver_tm_t, main_packet_tx_error_count) }, \
{ "main_tx_bitrate", NULL, MAVLINK_TYPE_UINT16_T, 0, 30, offsetof(mavlink_receiver_tm_t, main_tx_bitrate) }, \
{ "main_packet_rx_success_count", NULL, MAVLINK_TYPE_UINT16_T, 0, 32, offsetof(mavlink_receiver_tm_t, main_packet_rx_success_count) }, \
{ "main_packet_rx_drop_count", NULL, MAVLINK_TYPE_UINT16_T, 0, 34, offsetof(mavlink_receiver_tm_t, main_packet_rx_drop_count) }, \
{ "main_rx_bitrate", NULL, MAVLINK_TYPE_UINT16_T, 0, 36, offsetof(mavlink_receiver_tm_t, main_rx_bitrate) }, \
{ "main_rx_rssi", NULL, MAVLINK_TYPE_FLOAT, 0, 8, offsetof(mavlink_receiver_tm_t, main_rx_rssi) }, \
{ "main_rx_fei", NULL, MAVLINK_TYPE_FLOAT, 0, 12, offsetof(mavlink_receiver_tm_t, main_rx_fei) }, \
{ "payload_radio_present", NULL, MAVLINK_TYPE_UINT8_T, 0, 49, offsetof(mavlink_receiver_tm_t, payload_radio_present) }, \
{ "payload_packet_tx_error_count", NULL, MAVLINK_TYPE_UINT16_T, 0, 38, offsetof(mavlink_receiver_tm_t, payload_packet_tx_error_count) }, \
{ "payload_tx_bitrate", NULL, MAVLINK_TYPE_UINT16_T, 0, 40, offsetof(mavlink_receiver_tm_t, payload_tx_bitrate) }, \
{ "payload_packet_rx_success_count", NULL, MAVLINK_TYPE_UINT16_T, 0, 42, offsetof(mavlink_receiver_tm_t, payload_packet_rx_success_count) }, \
{ "payload_packet_rx_drop_count", NULL, MAVLINK_TYPE_UINT16_T, 0, 44, offsetof(mavlink_receiver_tm_t, payload_packet_rx_drop_count) }, \
{ "payload_rx_bitrate", NULL, MAVLINK_TYPE_UINT16_T, 0, 46, offsetof(mavlink_receiver_tm_t, payload_rx_bitrate) }, \
{ "payload_rx_rssi", NULL, MAVLINK_TYPE_FLOAT, 0, 16, offsetof(mavlink_receiver_tm_t, payload_rx_rssi) }, \
{ "payload_rx_fei", NULL, MAVLINK_TYPE_FLOAT, 0, 20, offsetof(mavlink_receiver_tm_t, payload_rx_fei) }, \
{ "ethernet_present", NULL, MAVLINK_TYPE_UINT8_T, 0, 50, offsetof(mavlink_receiver_tm_t, ethernet_present) }, \
{ "ethernet_status", NULL, MAVLINK_TYPE_UINT8_T, 0, 51, offsetof(mavlink_receiver_tm_t, ethernet_status) }, \
{ "battery_voltage", NULL, MAVLINK_TYPE_FLOAT, 0, 24, offsetof(mavlink_receiver_tm_t, battery_voltage) }, \
} \
}
#else
#define MAVLINK_MESSAGE_INFO_RECEIVER_TM { \
"RECEIVER_TM", \
5, \
20, \
{ { "timestamp", NULL, MAVLINK_TYPE_UINT64_T, 0, 0, offsetof(mavlink_receiver_tm_t, timestamp) }, \
{ "rssi", NULL, MAVLINK_TYPE_FLOAT, 0, 24, offsetof(mavlink_receiver_tm_t, rssi) }, \
{ "fei", NULL, MAVLINK_TYPE_FLOAT, 0, 28, offsetof(mavlink_receiver_tm_t, fei) }, \
{ "rx_bitrate", NULL, MAVLINK_TYPE_UINT64_T, 0, 8, offsetof(mavlink_receiver_tm_t, rx_bitrate) }, \
{ "tx_bitrate", NULL, MAVLINK_TYPE_UINT64_T, 0, 16, offsetof(mavlink_receiver_tm_t, tx_bitrate) }, \
{ "main_radio_present", NULL, MAVLINK_TYPE_UINT8_T, 0, 48, offsetof(mavlink_receiver_tm_t, main_radio_present) }, \
{ "main_packet_tx_error_count", NULL, MAVLINK_TYPE_UINT16_T, 0, 28, offsetof(mavlink_receiver_tm_t, main_packet_tx_error_count) }, \
{ "main_tx_bitrate", NULL, MAVLINK_TYPE_UINT16_T, 0, 30, offsetof(mavlink_receiver_tm_t, main_tx_bitrate) }, \
{ "main_packet_rx_success_count", NULL, MAVLINK_TYPE_UINT16_T, 0, 32, offsetof(mavlink_receiver_tm_t, main_packet_rx_success_count) }, \
{ "main_packet_rx_drop_count", NULL, MAVLINK_TYPE_UINT16_T, 0, 34, offsetof(mavlink_receiver_tm_t, main_packet_rx_drop_count) }, \
{ "main_rx_bitrate", NULL, MAVLINK_TYPE_UINT16_T, 0, 36, offsetof(mavlink_receiver_tm_t, main_rx_bitrate) }, \
{ "main_rx_rssi", NULL, MAVLINK_TYPE_FLOAT, 0, 8, offsetof(mavlink_receiver_tm_t, main_rx_rssi) }, \
{ "main_rx_fei", NULL, MAVLINK_TYPE_FLOAT, 0, 12, offsetof(mavlink_receiver_tm_t, main_rx_fei) }, \
{ "payload_radio_present", NULL, MAVLINK_TYPE_UINT8_T, 0, 49, offsetof(mavlink_receiver_tm_t, payload_radio_present) }, \
{ "payload_packet_tx_error_count", NULL, MAVLINK_TYPE_UINT16_T, 0, 38, offsetof(mavlink_receiver_tm_t, payload_packet_tx_error_count) }, \
{ "payload_tx_bitrate", NULL, MAVLINK_TYPE_UINT16_T, 0, 40, offsetof(mavlink_receiver_tm_t, payload_tx_bitrate) }, \
{ "payload_packet_rx_success_count", NULL, MAVLINK_TYPE_UINT16_T, 0, 42, offsetof(mavlink_receiver_tm_t, payload_packet_rx_success_count) }, \
{ "payload_packet_rx_drop_count", NULL, MAVLINK_TYPE_UINT16_T, 0, 44, offsetof(mavlink_receiver_tm_t, payload_packet_rx_drop_count) }, \
{ "payload_rx_bitrate", NULL, MAVLINK_TYPE_UINT16_T, 0, 46, offsetof(mavlink_receiver_tm_t, payload_rx_bitrate) }, \
{ "payload_rx_rssi", NULL, MAVLINK_TYPE_FLOAT, 0, 16, offsetof(mavlink_receiver_tm_t, payload_rx_rssi) }, \
{ "payload_rx_fei", NULL, MAVLINK_TYPE_FLOAT, 0, 20, offsetof(mavlink_receiver_tm_t, payload_rx_fei) }, \
{ "ethernet_present", NULL, MAVLINK_TYPE_UINT8_T, 0, 50, offsetof(mavlink_receiver_tm_t, ethernet_present) }, \
{ "ethernet_status", NULL, MAVLINK_TYPE_UINT8_T, 0, 51, offsetof(mavlink_receiver_tm_t, ethernet_status) }, \
{ "battery_voltage", NULL, MAVLINK_TYPE_FLOAT, 0, 24, offsetof(mavlink_receiver_tm_t, battery_voltage) }, \
} \
}
#endif
......@@ -54,31 +99,76 @@ typedef struct __mavlink_receiver_tm_t {
* @param msg The MAVLink message to compress the data into
*
* @param timestamp [us] Timestamp
* @param rssi [dBm] Rssi
* @param fei [Hz] Fei
* @param rx_bitrate [kb/s] Rx bitrate
* @param tx_bitrate [kb/s] Tx bitrate
* @param main_radio_present Boolean indicating the presence of the main radio
* @param main_packet_tx_error_count Number of errors during send
* @param main_tx_bitrate [b/s] Send bitrate
* @param main_packet_rx_success_count Number of succesfull received mavlink packets
* @param main_packet_rx_drop_count Number of dropped mavlink packets
* @param main_rx_bitrate [b/s] Receive bitrate
* @param main_rx_rssi [dBm] Receive RSSI
* @param main_rx_fei [Hz] Receive frequency error index
* @param payload_radio_present Boolean indicating the presence of the payload radio
* @param payload_packet_tx_error_count Number of errors during send
* @param payload_tx_bitrate [b/s] Send bitrate
* @param payload_packet_rx_success_count Number of succesfull received mavlink packets
* @param payload_packet_rx_drop_count Number of dropped mavlink packets
* @param payload_rx_bitrate [b/s] Receive bitrate
* @param payload_rx_rssi [dBm] Receive RSSI
* @param payload_rx_fei [Hz] Receive frequency error index
* @param ethernet_present Boolean indicating the presence of the ethernet module
* @param ethernet_status Status flag indicating the status of the ethernet PHY
* @param battery_voltage [V] Battery voltage
* @return length of the message in bytes (excluding serial stream start sign)
*/
static inline uint16_t mavlink_msg_receiver_tm_pack(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg,
uint64_t timestamp, float rssi, float fei, uint64_t rx_bitrate, uint64_t tx_bitrate)
uint64_t timestamp, uint8_t main_radio_present, uint16_t main_packet_tx_error_count, uint16_t main_tx_bitrate, uint16_t main_packet_rx_success_count, uint16_t main_packet_rx_drop_count, uint16_t main_rx_bitrate, float main_rx_rssi, float main_rx_fei, uint8_t payload_radio_present, uint16_t payload_packet_tx_error_count, uint16_t payload_tx_bitrate, uint16_t payload_packet_rx_success_count, uint16_t payload_packet_rx_drop_count, uint16_t payload_rx_bitrate, float payload_rx_rssi, float payload_rx_fei, uint8_t ethernet_present, uint8_t ethernet_status, float battery_voltage)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char buf[MAVLINK_MSG_ID_RECEIVER_TM_LEN];
_mav_put_uint64_t(buf, 0, timestamp);
_mav_put_uint64_t(buf, 8, rx_bitrate);
_mav_put_uint64_t(buf, 16, tx_bitrate);
_mav_put_float(buf, 24, rssi);
_mav_put_float(buf, 28, fei);
_mav_put_float(buf, 8, main_rx_rssi);
_mav_put_float(buf, 12, main_rx_fei);
_mav_put_float(buf, 16, payload_rx_rssi);
_mav_put_float(buf, 20, payload_rx_fei);
_mav_put_float(buf, 24, battery_voltage);
_mav_put_uint16_t(buf, 28, main_packet_tx_error_count);
_mav_put_uint16_t(buf, 30, main_tx_bitrate);
_mav_put_uint16_t(buf, 32, main_packet_rx_success_count);
_mav_put_uint16_t(buf, 34, main_packet_rx_drop_count);
_mav_put_uint16_t(buf, 36, main_rx_bitrate);
_mav_put_uint16_t(buf, 38, payload_packet_tx_error_count);
_mav_put_uint16_t(buf, 40, payload_tx_bitrate);
_mav_put_uint16_t(buf, 42, payload_packet_rx_success_count);
_mav_put_uint16_t(buf, 44, payload_packet_rx_drop_count);
_mav_put_uint16_t(buf, 46, payload_rx_bitrate);
_mav_put_uint8_t(buf, 48, main_radio_present);
_mav_put_uint8_t(buf, 49, payload_radio_present);
_mav_put_uint8_t(buf, 50, ethernet_present);
_mav_put_uint8_t(buf, 51, ethernet_status);
memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_RECEIVER_TM_LEN);
#else
mavlink_receiver_tm_t packet;
packet.timestamp = timestamp;
packet.rx_bitrate = rx_bitrate;
packet.tx_bitrate = tx_bitrate;
packet.rssi = rssi;
packet.fei = fei;
packet.main_rx_rssi = main_rx_rssi;
packet.main_rx_fei = main_rx_fei;
packet.payload_rx_rssi = payload_rx_rssi;
packet.payload_rx_fei = payload_rx_fei;
packet.battery_voltage = battery_voltage;
packet.main_packet_tx_error_count = main_packet_tx_error_count;
packet.main_tx_bitrate = main_tx_bitrate;
packet.main_packet_rx_success_count = main_packet_rx_success_count;
packet.main_packet_rx_drop_count = main_packet_rx_drop_count;
packet.main_rx_bitrate = main_rx_bitrate;
packet.payload_packet_tx_error_count = payload_packet_tx_error_count;
packet.payload_tx_bitrate = payload_tx_bitrate;
packet.payload_packet_rx_success_count = payload_packet_rx_success_count;
packet.payload_packet_rx_drop_count = payload_packet_rx_drop_count;
packet.payload_rx_bitrate = payload_rx_bitrate;
packet.main_radio_present = main_radio_present;
packet.payload_radio_present = payload_radio_present;
packet.ethernet_present = ethernet_present;
packet.ethernet_status = ethernet_status;
memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_RECEIVER_TM_LEN);
#endif
......@@ -94,32 +184,77 @@ static inline uint16_t mavlink_msg_receiver_tm_pack(uint8_t system_id, uint8_t c
* @param chan The MAVLink channel this message will be sent over
* @param msg The MAVLink message to compress the data into
* @param timestamp [us] Timestamp
* @param rssi [dBm] Rssi
* @param fei [Hz] Fei
* @param rx_bitrate [kb/s] Rx bitrate
* @param tx_bitrate [kb/s] Tx bitrate
* @param main_radio_present Boolean indicating the presence of the main radio
* @param main_packet_tx_error_count Number of errors during send
* @param main_tx_bitrate [b/s] Send bitrate
* @param main_packet_rx_success_count Number of succesfull received mavlink packets
* @param main_packet_rx_drop_count Number of dropped mavlink packets
* @param main_rx_bitrate [b/s] Receive bitrate
* @param main_rx_rssi [dBm] Receive RSSI
* @param main_rx_fei [Hz] Receive frequency error index
* @param payload_radio_present Boolean indicating the presence of the payload radio
* @param payload_packet_tx_error_count Number of errors during send
* @param payload_tx_bitrate [b/s] Send bitrate
* @param payload_packet_rx_success_count Number of succesfull received mavlink packets
* @param payload_packet_rx_drop_count Number of dropped mavlink packets
* @param payload_rx_bitrate [b/s] Receive bitrate
* @param payload_rx_rssi [dBm] Receive RSSI
* @param payload_rx_fei [Hz] Receive frequency error index
* @param ethernet_present Boolean indicating the presence of the ethernet module
* @param ethernet_status Status flag indicating the status of the ethernet PHY
* @param battery_voltage [V] Battery voltage
* @return length of the message in bytes (excluding serial stream start sign)
*/
static inline uint16_t mavlink_msg_receiver_tm_pack_chan(uint8_t system_id, uint8_t component_id, uint8_t chan,
mavlink_message_t* msg,
uint64_t timestamp,float rssi,float fei,uint64_t rx_bitrate,uint64_t tx_bitrate)
uint64_t timestamp,uint8_t main_radio_present,uint16_t main_packet_tx_error_count,uint16_t main_tx_bitrate,uint16_t main_packet_rx_success_count,uint16_t main_packet_rx_drop_count,uint16_t main_rx_bitrate,float main_rx_rssi,float main_rx_fei,uint8_t payload_radio_present,uint16_t payload_packet_tx_error_count,uint16_t payload_tx_bitrate,uint16_t payload_packet_rx_success_count,uint16_t payload_packet_rx_drop_count,uint16_t payload_rx_bitrate,float payload_rx_rssi,float payload_rx_fei,uint8_t ethernet_present,uint8_t ethernet_status,float battery_voltage)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char buf[MAVLINK_MSG_ID_RECEIVER_TM_LEN];
_mav_put_uint64_t(buf, 0, timestamp);
_mav_put_uint64_t(buf, 8, rx_bitrate);
_mav_put_uint64_t(buf, 16, tx_bitrate);
_mav_put_float(buf, 24, rssi);
_mav_put_float(buf, 28, fei);
_mav_put_float(buf, 8, main_rx_rssi);
_mav_put_float(buf, 12, main_rx_fei);
_mav_put_float(buf, 16, payload_rx_rssi);
_mav_put_float(buf, 20, payload_rx_fei);
_mav_put_float(buf, 24, battery_voltage);
_mav_put_uint16_t(buf, 28, main_packet_tx_error_count);
_mav_put_uint16_t(buf, 30, main_tx_bitrate);
_mav_put_uint16_t(buf, 32, main_packet_rx_success_count);
_mav_put_uint16_t(buf, 34, main_packet_rx_drop_count);
_mav_put_uint16_t(buf, 36, main_rx_bitrate);
_mav_put_uint16_t(buf, 38, payload_packet_tx_error_count);
_mav_put_uint16_t(buf, 40, payload_tx_bitrate);
_mav_put_uint16_t(buf, 42, payload_packet_rx_success_count);
_mav_put_uint16_t(buf, 44, payload_packet_rx_drop_count);
_mav_put_uint16_t(buf, 46, payload_rx_bitrate);
_mav_put_uint8_t(buf, 48, main_radio_present);
_mav_put_uint8_t(buf, 49, payload_radio_present);
_mav_put_uint8_t(buf, 50, ethernet_present);
_mav_put_uint8_t(buf, 51, ethernet_status);
memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_RECEIVER_TM_LEN);
#else
mavlink_receiver_tm_t packet;
packet.timestamp = timestamp;
packet.rx_bitrate = rx_bitrate;
packet.tx_bitrate = tx_bitrate;
packet.rssi = rssi;
packet.fei = fei;
packet.main_rx_rssi = main_rx_rssi;
packet.main_rx_fei = main_rx_fei;
packet.payload_rx_rssi = payload_rx_rssi;
packet.payload_rx_fei = payload_rx_fei;
packet.battery_voltage = battery_voltage;
packet.main_packet_tx_error_count = main_packet_tx_error_count;
packet.main_tx_bitrate = main_tx_bitrate;
packet.main_packet_rx_success_count = main_packet_rx_success_count;
packet.main_packet_rx_drop_count = main_packet_rx_drop_count;
packet.main_rx_bitrate = main_rx_bitrate;
packet.payload_packet_tx_error_count = payload_packet_tx_error_count;
packet.payload_tx_bitrate = payload_tx_bitrate;
packet.payload_packet_rx_success_count = payload_packet_rx_success_count;
packet.payload_packet_rx_drop_count = payload_packet_rx_drop_count;
packet.payload_rx_bitrate = payload_rx_bitrate;
packet.main_radio_present = main_radio_present;
packet.payload_radio_present = payload_radio_present;
packet.ethernet_present = ethernet_present;
packet.ethernet_status = ethernet_status;
memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_RECEIVER_TM_LEN);
#endif
......@@ -138,7 +273,7 @@ static inline uint16_t mavlink_msg_receiver_tm_pack_chan(uint8_t system_id, uint
*/
static inline uint16_t mavlink_msg_receiver_tm_encode(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg, const mavlink_receiver_tm_t* receiver_tm)
{
return mavlink_msg_receiver_tm_pack(system_id, component_id, msg, receiver_tm->timestamp, receiver_tm->rssi, receiver_tm->fei, receiver_tm->rx_bitrate, receiver_tm->tx_bitrate);
return mavlink_msg_receiver_tm_pack(system_id, component_id, msg, receiver_tm->timestamp, receiver_tm->main_radio_present, receiver_tm->main_packet_tx_error_count, receiver_tm->main_tx_bitrate, receiver_tm->main_packet_rx_success_count, receiver_tm->main_packet_rx_drop_count, receiver_tm->main_rx_bitrate, receiver_tm->main_rx_rssi, receiver_tm->main_rx_fei, receiver_tm->payload_radio_present, receiver_tm->payload_packet_tx_error_count, receiver_tm->payload_tx_bitrate, receiver_tm->payload_packet_rx_success_count, receiver_tm->payload_packet_rx_drop_count, receiver_tm->payload_rx_bitrate, receiver_tm->payload_rx_rssi, receiver_tm->payload_rx_fei, receiver_tm->ethernet_present, receiver_tm->ethernet_status, receiver_tm->battery_voltage);
}
/**
......@@ -152,7 +287,7 @@ static inline uint16_t mavlink_msg_receiver_tm_encode(uint8_t system_id, uint8_t
*/
static inline uint16_t mavlink_msg_receiver_tm_encode_chan(uint8_t system_id, uint8_t component_id, uint8_t chan, mavlink_message_t* msg, const mavlink_receiver_tm_t* receiver_tm)
{
return mavlink_msg_receiver_tm_pack_chan(system_id, component_id, chan, msg, receiver_tm->timestamp, receiver_tm->rssi, receiver_tm->fei, receiver_tm->rx_bitrate, receiver_tm->tx_bitrate);
return mavlink_msg_receiver_tm_pack_chan(system_id, component_id, chan, msg, receiver_tm->timestamp, receiver_tm->main_radio_present, receiver_tm->main_packet_tx_error_count, receiver_tm->main_tx_bitrate, receiver_tm->main_packet_rx_success_count, receiver_tm->main_packet_rx_drop_count, receiver_tm->main_rx_bitrate, receiver_tm->main_rx_rssi, receiver_tm->main_rx_fei, receiver_tm->payload_radio_present, receiver_tm->payload_packet_tx_error_count, receiver_tm->payload_tx_bitrate, receiver_tm->payload_packet_rx_success_count, receiver_tm->payload_packet_rx_drop_count, receiver_tm->payload_rx_bitrate, receiver_tm->payload_rx_rssi, receiver_tm->payload_rx_fei, receiver_tm->ethernet_present, receiver_tm->ethernet_status, receiver_tm->battery_voltage);
}
/**
......@@ -160,31 +295,76 @@ static inline uint16_t mavlink_msg_receiver_tm_encode_chan(uint8_t system_id, ui
* @param chan MAVLink channel to send the message
*
* @param timestamp [us] Timestamp
* @param rssi [dBm] Rssi
* @param fei [Hz] Fei
* @param rx_bitrate [kb/s] Rx bitrate
* @param tx_bitrate [kb/s] Tx bitrate
* @param main_radio_present Boolean indicating the presence of the main radio
* @param main_packet_tx_error_count Number of errors during send
* @param main_tx_bitrate [b/s] Send bitrate
* @param main_packet_rx_success_count Number of succesfull received mavlink packets
* @param main_packet_rx_drop_count Number of dropped mavlink packets
* @param main_rx_bitrate [b/s] Receive bitrate
* @param main_rx_rssi [dBm] Receive RSSI
* @param main_rx_fei [Hz] Receive frequency error index
* @param payload_radio_present Boolean indicating the presence of the payload radio
* @param payload_packet_tx_error_count Number of errors during send
* @param payload_tx_bitrate [b/s] Send bitrate
* @param payload_packet_rx_success_count Number of succesfull received mavlink packets
* @param payload_packet_rx_drop_count Number of dropped mavlink packets
* @param payload_rx_bitrate [b/s] Receive bitrate
* @param payload_rx_rssi [dBm] Receive RSSI
* @param payload_rx_fei [Hz] Receive frequency error index
* @param ethernet_present Boolean indicating the presence of the ethernet module
* @param ethernet_status Status flag indicating the status of the ethernet PHY
* @param battery_voltage [V] Battery voltage
*/
#ifdef MAVLINK_USE_CONVENIENCE_FUNCTIONS
static inline void mavlink_msg_receiver_tm_send(mavlink_channel_t chan, uint64_t timestamp, float rssi, float fei, uint64_t rx_bitrate, uint64_t tx_bitrate)
static inline void mavlink_msg_receiver_tm_send(mavlink_channel_t chan, uint64_t timestamp, uint8_t main_radio_present, uint16_t main_packet_tx_error_count, uint16_t main_tx_bitrate, uint16_t main_packet_rx_success_count, uint16_t main_packet_rx_drop_count, uint16_t main_rx_bitrate, float main_rx_rssi, float main_rx_fei, uint8_t payload_radio_present, uint16_t payload_packet_tx_error_count, uint16_t payload_tx_bitrate, uint16_t payload_packet_rx_success_count, uint16_t payload_packet_rx_drop_count, uint16_t payload_rx_bitrate, float payload_rx_rssi, float payload_rx_fei, uint8_t ethernet_present, uint8_t ethernet_status, float battery_voltage)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char buf[MAVLINK_MSG_ID_RECEIVER_TM_LEN];
_mav_put_uint64_t(buf, 0, timestamp);
_mav_put_uint64_t(buf, 8, rx_bitrate);
_mav_put_uint64_t(buf, 16, tx_bitrate);
_mav_put_float(buf, 24, rssi);
_mav_put_float(buf, 28, fei);
_mav_put_float(buf, 8, main_rx_rssi);
_mav_put_float(buf, 12, main_rx_fei);
_mav_put_float(buf, 16, payload_rx_rssi);
_mav_put_float(buf, 20, payload_rx_fei);
_mav_put_float(buf, 24, battery_voltage);
_mav_put_uint16_t(buf, 28, main_packet_tx_error_count);
_mav_put_uint16_t(buf, 30, main_tx_bitrate);
_mav_put_uint16_t(buf, 32, main_packet_rx_success_count);
_mav_put_uint16_t(buf, 34, main_packet_rx_drop_count);
_mav_put_uint16_t(buf, 36, main_rx_bitrate);
_mav_put_uint16_t(buf, 38, payload_packet_tx_error_count);
_mav_put_uint16_t(buf, 40, payload_tx_bitrate);
_mav_put_uint16_t(buf, 42, payload_packet_rx_success_count);
_mav_put_uint16_t(buf, 44, payload_packet_rx_drop_count);
_mav_put_uint16_t(buf, 46, payload_rx_bitrate);
_mav_put_uint8_t(buf, 48, main_radio_present);
_mav_put_uint8_t(buf, 49, payload_radio_present);
_mav_put_uint8_t(buf, 50, ethernet_present);
_mav_put_uint8_t(buf, 51, ethernet_status);
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RECEIVER_TM, buf, MAVLINK_MSG_ID_RECEIVER_TM_MIN_LEN, MAVLINK_MSG_ID_RECEIVER_TM_LEN, MAVLINK_MSG_ID_RECEIVER_TM_CRC);
#else
mavlink_receiver_tm_t packet;
packet.timestamp = timestamp;
packet.rx_bitrate = rx_bitrate;
packet.tx_bitrate = tx_bitrate;
packet.rssi = rssi;
packet.fei = fei;
packet.main_rx_rssi = main_rx_rssi;
packet.main_rx_fei = main_rx_fei;
packet.payload_rx_rssi = payload_rx_rssi;
packet.payload_rx_fei = payload_rx_fei;
packet.battery_voltage = battery_voltage;
packet.main_packet_tx_error_count = main_packet_tx_error_count;
packet.main_tx_bitrate = main_tx_bitrate;
packet.main_packet_rx_success_count = main_packet_rx_success_count;
packet.main_packet_rx_drop_count = main_packet_rx_drop_count;
packet.main_rx_bitrate = main_rx_bitrate;
packet.payload_packet_tx_error_count = payload_packet_tx_error_count;
packet.payload_tx_bitrate = payload_tx_bitrate;
packet.payload_packet_rx_success_count = payload_packet_rx_success_count;
packet.payload_packet_rx_drop_count = payload_packet_rx_drop_count;
packet.payload_rx_bitrate = payload_rx_bitrate;
packet.main_radio_present = main_radio_present;
packet.payload_radio_present = payload_radio_present;
packet.ethernet_present = ethernet_present;
packet.ethernet_status = ethernet_status;
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RECEIVER_TM, (const char *)&packet, MAVLINK_MSG_ID_RECEIVER_TM_MIN_LEN, MAVLINK_MSG_ID_RECEIVER_TM_LEN, MAVLINK_MSG_ID_RECEIVER_TM_CRC);
#endif
......@@ -198,7 +378,7 @@ static inline void mavlink_msg_receiver_tm_send(mavlink_channel_t chan, uint64_t
static inline void mavlink_msg_receiver_tm_send_struct(mavlink_channel_t chan, const mavlink_receiver_tm_t* receiver_tm)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
mavlink_msg_receiver_tm_send(chan, receiver_tm->timestamp, receiver_tm->rssi, receiver_tm->fei, receiver_tm->rx_bitrate, receiver_tm->tx_bitrate);
mavlink_msg_receiver_tm_send(chan, receiver_tm->timestamp, receiver_tm->main_radio_present, receiver_tm->main_packet_tx_error_count, receiver_tm->main_tx_bitrate, receiver_tm->main_packet_rx_success_count, receiver_tm->main_packet_rx_drop_count, receiver_tm->main_rx_bitrate, receiver_tm->main_rx_rssi, receiver_tm->main_rx_fei, receiver_tm->payload_radio_present, receiver_tm->payload_packet_tx_error_count, receiver_tm->payload_tx_bitrate, receiver_tm->payload_packet_rx_success_count, receiver_tm->payload_packet_rx_drop_count, receiver_tm->payload_rx_bitrate, receiver_tm->payload_rx_rssi, receiver_tm->payload_rx_fei, receiver_tm->ethernet_present, receiver_tm->ethernet_status, receiver_tm->battery_voltage);
#else
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RECEIVER_TM, (const char *)receiver_tm, MAVLINK_MSG_ID_RECEIVER_TM_MIN_LEN, MAVLINK_MSG_ID_RECEIVER_TM_LEN, MAVLINK_MSG_ID_RECEIVER_TM_CRC);
#endif
......@@ -212,24 +392,54 @@ static inline void mavlink_msg_receiver_tm_send_struct(mavlink_channel_t chan, c
is usually the receive buffer for the channel, and allows a reply to an
incoming message with minimum stack space usage.
*/
static inline void mavlink_msg_receiver_tm_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint64_t timestamp, float rssi, float fei, uint64_t rx_bitrate, uint64_t tx_bitrate)
static inline void mavlink_msg_receiver_tm_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint64_t timestamp, uint8_t main_radio_present, uint16_t main_packet_tx_error_count, uint16_t main_tx_bitrate, uint16_t main_packet_rx_success_count, uint16_t main_packet_rx_drop_count, uint16_t main_rx_bitrate, float main_rx_rssi, float main_rx_fei, uint8_t payload_radio_present, uint16_t payload_packet_tx_error_count, uint16_t payload_tx_bitrate, uint16_t payload_packet_rx_success_count, uint16_t payload_packet_rx_drop_count, uint16_t payload_rx_bitrate, float payload_rx_rssi, float payload_rx_fei, uint8_t ethernet_present, uint8_t ethernet_status, float battery_voltage)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char *buf = (char *)msgbuf;
_mav_put_uint64_t(buf, 0, timestamp);
_mav_put_uint64_t(buf, 8, rx_bitrate);
_mav_put_uint64_t(buf, 16, tx_bitrate);
_mav_put_float(buf, 24, rssi);
_mav_put_float(buf, 28, fei);
_mav_put_float(buf, 8, main_rx_rssi);
_mav_put_float(buf, 12, main_rx_fei);
_mav_put_float(buf, 16, payload_rx_rssi);
_mav_put_float(buf, 20, payload_rx_fei);
_mav_put_float(buf, 24, battery_voltage);
_mav_put_uint16_t(buf, 28, main_packet_tx_error_count);
_mav_put_uint16_t(buf, 30, main_tx_bitrate);
_mav_put_uint16_t(buf, 32, main_packet_rx_success_count);
_mav_put_uint16_t(buf, 34, main_packet_rx_drop_count);
_mav_put_uint16_t(buf, 36, main_rx_bitrate);
_mav_put_uint16_t(buf, 38, payload_packet_tx_error_count);
_mav_put_uint16_t(buf, 40, payload_tx_bitrate);
_mav_put_uint16_t(buf, 42, payload_packet_rx_success_count);
_mav_put_uint16_t(buf, 44, payload_packet_rx_drop_count);
_mav_put_uint16_t(buf, 46, payload_rx_bitrate);
_mav_put_uint8_t(buf, 48, main_radio_present);
_mav_put_uint8_t(buf, 49, payload_radio_present);
_mav_put_uint8_t(buf, 50, ethernet_present);
_mav_put_uint8_t(buf, 51, ethernet_status);
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RECEIVER_TM, buf, MAVLINK_MSG_ID_RECEIVER_TM_MIN_LEN, MAVLINK_MSG_ID_RECEIVER_TM_LEN, MAVLINK_MSG_ID_RECEIVER_TM_CRC);
#else
mavlink_receiver_tm_t *packet = (mavlink_receiver_tm_t *)msgbuf;
packet->timestamp = timestamp;
packet->rx_bitrate = rx_bitrate;
packet->tx_bitrate = tx_bitrate;
packet->rssi = rssi;
packet->fei = fei;
packet->main_rx_rssi = main_rx_rssi;
packet->main_rx_fei = main_rx_fei;
packet->payload_rx_rssi = payload_rx_rssi;
packet->payload_rx_fei = payload_rx_fei;
packet->battery_voltage = battery_voltage;
packet->main_packet_tx_error_count = main_packet_tx_error_count;
packet->main_tx_bitrate = main_tx_bitrate;
packet->main_packet_rx_success_count = main_packet_rx_success_count;
packet->main_packet_rx_drop_count = main_packet_rx_drop_count;
packet->main_rx_bitrate = main_rx_bitrate;
packet->payload_packet_tx_error_count = payload_packet_tx_error_count;
packet->payload_tx_bitrate = payload_tx_bitrate;
packet->payload_packet_rx_success_count = payload_packet_rx_success_count;
packet->payload_packet_rx_drop_count = payload_packet_rx_drop_count;
packet->payload_rx_bitrate = payload_rx_bitrate;
packet->main_radio_present = main_radio_present;
packet->payload_radio_present = payload_radio_present;
packet->ethernet_present = ethernet_present;
packet->ethernet_status = ethernet_status;
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_RECEIVER_TM, (const char *)packet, MAVLINK_MSG_ID_RECEIVER_TM_MIN_LEN, MAVLINK_MSG_ID_RECEIVER_TM_LEN, MAVLINK_MSG_ID_RECEIVER_TM_CRC);
#endif
......@@ -252,43 +462,193 @@ static inline uint64_t mavlink_msg_receiver_tm_get_timestamp(const mavlink_messa
}
/**
* @brief Get field rssi from receiver_tm message
* @brief Get field main_radio_present from receiver_tm message
*
* @return [dBm] Rssi
* @return Boolean indicating the presence of the main radio
*/
static inline float mavlink_msg_receiver_tm_get_rssi(const mavlink_message_t* msg)
static inline uint8_t mavlink_msg_receiver_tm_get_main_radio_present(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 24);
return _MAV_RETURN_uint8_t(msg, 48);
}
/**
* @brief Get field main_packet_tx_error_count from receiver_tm message
*
* @return Number of errors during send
*/
static inline uint16_t mavlink_msg_receiver_tm_get_main_packet_tx_error_count(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint16_t(msg, 28);
}
/**
* @brief Get field main_tx_bitrate from receiver_tm message
*
* @return [b/s] Send bitrate
*/
static inline uint16_t mavlink_msg_receiver_tm_get_main_tx_bitrate(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint16_t(msg, 30);
}
/**
* @brief Get field main_packet_rx_success_count from receiver_tm message
*
* @return Number of succesfull received mavlink packets
*/
static inline uint16_t mavlink_msg_receiver_tm_get_main_packet_rx_success_count(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint16_t(msg, 32);
}
/**
* @brief Get field main_packet_rx_drop_count from receiver_tm message
*
* @return Number of dropped mavlink packets
*/
static inline uint16_t mavlink_msg_receiver_tm_get_main_packet_rx_drop_count(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint16_t(msg, 34);
}
/**
* @brief Get field main_rx_bitrate from receiver_tm message
*
* @return [b/s] Receive bitrate
*/
static inline uint16_t mavlink_msg_receiver_tm_get_main_rx_bitrate(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint16_t(msg, 36);
}
/**
* @brief Get field main_rx_rssi from receiver_tm message
*
* @return [dBm] Receive RSSI
*/
static inline float mavlink_msg_receiver_tm_get_main_rx_rssi(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 8);
}
/**
* @brief Get field main_rx_fei from receiver_tm message
*
* @return [Hz] Receive frequency error index
*/
static inline float mavlink_msg_receiver_tm_get_main_rx_fei(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 12);
}
/**
* @brief Get field payload_radio_present from receiver_tm message
*
* @return Boolean indicating the presence of the payload radio
*/
static inline uint8_t mavlink_msg_receiver_tm_get_payload_radio_present(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint8_t(msg, 49);
}
/**
* @brief Get field payload_packet_tx_error_count from receiver_tm message
*
* @return Number of errors during send
*/
static inline uint16_t mavlink_msg_receiver_tm_get_payload_packet_tx_error_count(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint16_t(msg, 38);
}
/**
* @brief Get field payload_tx_bitrate from receiver_tm message
*
* @return [b/s] Send bitrate
*/
static inline uint16_t mavlink_msg_receiver_tm_get_payload_tx_bitrate(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint16_t(msg, 40);
}
/**
* @brief Get field payload_packet_rx_success_count from receiver_tm message
*
* @return Number of succesfull received mavlink packets
*/
static inline uint16_t mavlink_msg_receiver_tm_get_payload_packet_rx_success_count(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint16_t(msg, 42);
}
/**
* @brief Get field payload_packet_rx_drop_count from receiver_tm message
*
* @return Number of dropped mavlink packets
*/
static inline uint16_t mavlink_msg_receiver_tm_get_payload_packet_rx_drop_count(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint16_t(msg, 44);
}
/**
* @brief Get field payload_rx_bitrate from receiver_tm message
*
* @return [b/s] Receive bitrate
*/
static inline uint16_t mavlink_msg_receiver_tm_get_payload_rx_bitrate(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint16_t(msg, 46);
}
/**
* @brief Get field fei from receiver_tm message
* @brief Get field payload_rx_rssi from receiver_tm message
*
* @return [Hz] Fei
* @return [dBm] Receive RSSI
*/
static inline float mavlink_msg_receiver_tm_get_fei(const mavlink_message_t* msg)
static inline float mavlink_msg_receiver_tm_get_payload_rx_rssi(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 28);
return _MAV_RETURN_float(msg, 16);
}
/**
* @brief Get field rx_bitrate from receiver_tm message
* @brief Get field payload_rx_fei from receiver_tm message
*
* @return [kb/s] Rx bitrate
* @return [Hz] Receive frequency error index
*/
static inline uint64_t mavlink_msg_receiver_tm_get_rx_bitrate(const mavlink_message_t* msg)
static inline float mavlink_msg_receiver_tm_get_payload_rx_fei(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint64_t(msg, 8);
return _MAV_RETURN_float(msg, 20);
}
/**
* @brief Get field tx_bitrate from receiver_tm message
* @brief Get field ethernet_present from receiver_tm message
*
* @return [kb/s] Tx bitrate
* @return Boolean indicating the presence of the ethernet module
*/
static inline uint64_t mavlink_msg_receiver_tm_get_tx_bitrate(const mavlink_message_t* msg)
static inline uint8_t mavlink_msg_receiver_tm_get_ethernet_present(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint64_t(msg, 16);
return _MAV_RETURN_uint8_t(msg, 50);
}
/**
* @brief Get field ethernet_status from receiver_tm message
*
* @return Status flag indicating the status of the ethernet PHY
*/
static inline uint8_t mavlink_msg_receiver_tm_get_ethernet_status(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint8_t(msg, 51);
}
/**
* @brief Get field battery_voltage from receiver_tm message
*
* @return [V] Battery voltage
*/
static inline float mavlink_msg_receiver_tm_get_battery_voltage(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 24);
}
/**
......@@ -301,10 +661,25 @@ static inline void mavlink_msg_receiver_tm_decode(const mavlink_message_t* msg,
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
receiver_tm->timestamp = mavlink_msg_receiver_tm_get_timestamp(msg);
receiver_tm->rx_bitrate = mavlink_msg_receiver_tm_get_rx_bitrate(msg);
receiver_tm->tx_bitrate = mavlink_msg_receiver_tm_get_tx_bitrate(msg);
receiver_tm->rssi = mavlink_msg_receiver_tm_get_rssi(msg);
receiver_tm->fei = mavlink_msg_receiver_tm_get_fei(msg);
receiver_tm->main_rx_rssi = mavlink_msg_receiver_tm_get_main_rx_rssi(msg);
receiver_tm->main_rx_fei = mavlink_msg_receiver_tm_get_main_rx_fei(msg);
receiver_tm->payload_rx_rssi = mavlink_msg_receiver_tm_get_payload_rx_rssi(msg);
receiver_tm->payload_rx_fei = mavlink_msg_receiver_tm_get_payload_rx_fei(msg);
receiver_tm->battery_voltage = mavlink_msg_receiver_tm_get_battery_voltage(msg);
receiver_tm->main_packet_tx_error_count = mavlink_msg_receiver_tm_get_main_packet_tx_error_count(msg);
receiver_tm->main_tx_bitrate = mavlink_msg_receiver_tm_get_main_tx_bitrate(msg);
receiver_tm->main_packet_rx_success_count = mavlink_msg_receiver_tm_get_main_packet_rx_success_count(msg);
receiver_tm->main_packet_rx_drop_count = mavlink_msg_receiver_tm_get_main_packet_rx_drop_count(msg);
receiver_tm->main_rx_bitrate = mavlink_msg_receiver_tm_get_main_rx_bitrate(msg);
receiver_tm->payload_packet_tx_error_count = mavlink_msg_receiver_tm_get_payload_packet_tx_error_count(msg);
receiver_tm->payload_tx_bitrate = mavlink_msg_receiver_tm_get_payload_tx_bitrate(msg);
receiver_tm->payload_packet_rx_success_count = mavlink_msg_receiver_tm_get_payload_packet_rx_success_count(msg);
receiver_tm->payload_packet_rx_drop_count = mavlink_msg_receiver_tm_get_payload_packet_rx_drop_count(msg);
receiver_tm->payload_rx_bitrate = mavlink_msg_receiver_tm_get_payload_rx_bitrate(msg);
receiver_tm->main_radio_present = mavlink_msg_receiver_tm_get_main_radio_present(msg);
receiver_tm->payload_radio_present = mavlink_msg_receiver_tm_get_payload_radio_present(msg);
receiver_tm->ethernet_present = mavlink_msg_receiver_tm_get_ethernet_present(msg);
receiver_tm->ethernet_status = mavlink_msg_receiver_tm_get_ethernet_status(msg);
#else
uint8_t len = msg->len < MAVLINK_MSG_ID_RECEIVER_TM_LEN? msg->len : MAVLINK_MSG_ID_RECEIVER_TM_LEN;
memset(receiver_tm, 0, MAVLINK_MSG_ID_RECEIVER_TM_LEN);
......
mavlink_lib/gemini/mavlink_msg_rocket_flight_tm.h
View file @ 7abedf97
......@@ -13,6 +13,7 @@ typedef struct __mavlink_rocket_flight_tm_t {
float airspeed_pitot; /*< [m/s] Pitot airspeed*/
float altitude_agl; /*< [m] Altitude above ground level*/
float ada_vert_speed; /*< [m/s] Vertical speed estimated by ADA*/
float mea_mass; /*< [kg] Mass estimated by MEA*/
float acc_x; /*< [m/s^2] Acceleration on X axis (body)*/
float acc_y; /*< [m/s^2] Acceleration on Y axis (body)*/
float acc_z; /*< [m/s^2] Acceleration on Z axis (body)*/
......@@ -26,8 +27,6 @@ typedef struct __mavlink_rocket_flight_tm_t {
float gps_lon; /*< [deg] Longitude*/
float gps_alt; /*< [m] GPS Altitude*/
float abk_angle; /*< [deg] Air Brakes angle*/
float abk_estimated_cd; /*< Estimated drag coefficient*/
float parachute_load; /*< Parachute load cell value*/
float nas_n; /*< [deg] Navigation system estimated noth position*/
float nas_e; /*< [deg] Navigation system estimated east position*/
float nas_d; /*< [m] Navigation system estimated down position*/
......@@ -41,14 +40,17 @@ typedef struct __mavlink_rocket_flight_tm_t {
float nas_bias_x; /*< Navigation system gyroscope bias on x axis*/
float nas_bias_y; /*< Navigation system gyroscope bias on y axis*/
float nas_bias_z; /*< Navigation system gyroscope bias on z axis*/
float estimated_thrust; /*< Estimated thrust from automatic shutdown algorithm*/
float vbat; /*< [V] Battery voltage*/
float pin_quick_connector; /*< Quick connector detach pin */
float battery_voltage; /*< [V] Battery voltage*/
float cam_battery_voltage; /*< [V] Camera battery voltage*/
float current_consumption; /*< [A] Battery current*/
float temperature; /*< [degC] Temperature*/
uint8_t ada_state; /*< ADA Controller State*/
uint8_t fmm_state; /*< Flight Mode Manager State*/
uint8_t dpl_state; /*< Deployment Controller State*/
uint8_t abk_state; /*< Airbrake FSM state*/
uint8_t nas_state; /*< Navigation System FSM State*/
uint8_t mea_state; /*< MEA Controller State*/
uint8_t gps_fix; /*< GPS fix (1 = fix, 0 = no fix)*/
uint8_t pin_launch; /*< Launch pin status (1 = connected, 0 = disconnected)*/
uint8_t pin_nosecone; /*< Nosecone pin status (1 = connected, 0 = disconnected)*/
......@@ -57,13 +59,13 @@ typedef struct __mavlink_rocket_flight_tm_t {
int8_t logger_error; /*< Logger error (0 = no error, -1 otherwise)*/
} mavlink_rocket_flight_tm_t;
#define MAVLINK_MSG_ID_ROCKET_FLIGHT_TM_LEN 171
#define MAVLINK_MSG_ID_ROCKET_FLIGHT_TM_MIN_LEN 171
#define MAVLINK_MSG_ID_208_LEN 171
#define MAVLINK_MSG_ID_208_MIN_LEN 171
#define MAVLINK_MSG_ID_ROCKET_FLIGHT_TM_LEN 176
#define MAVLINK_MSG_ID_ROCKET_FLIGHT_TM_MIN_LEN 176
#define MAVLINK_MSG_ID_208_LEN 176
#define MAVLINK_MSG_ID_208_MIN_LEN 176
#define MAVLINK_MSG_ID_ROCKET_FLIGHT_TM_CRC 141
#define MAVLINK_MSG_ID_208_CRC 141
#define MAVLINK_MSG_ID_ROCKET_FLIGHT_TM_CRC 214
#define MAVLINK_MSG_ID_208_CRC 214
......@@ -71,13 +73,14 @@ typedef struct __mavlink_rocket_flight_tm_t {
#define MAVLINK_MESSAGE_INFO_ROCKET_FLIGHT_TM { \
208, \
"ROCKET_FLIGHT_TM", \
50, \
52, \
{ { "timestamp", NULL, MAVLINK_TYPE_UINT64_T, 0, 0, offsetof(mavlink_rocket_flight_tm_t, timestamp) }, \
{ "ada_state", NULL, MAVLINK_TYPE_UINT8_T, 0, 160, offsetof(mavlink_rocket_flight_tm_t, ada_state) }, \
{ "fmm_state", NULL, MAVLINK_TYPE_UINT8_T, 0, 161, offsetof(mavlink_rocket_flight_tm_t, fmm_state) }, \
{ "dpl_state", NULL, MAVLINK_TYPE_UINT8_T, 0, 162, offsetof(mavlink_rocket_flight_tm_t, dpl_state) }, \
{ "abk_state", NULL, MAVLINK_TYPE_UINT8_T, 0, 163, offsetof(mavlink_rocket_flight_tm_t, abk_state) }, \
{ "nas_state", NULL, MAVLINK_TYPE_UINT8_T, 0, 164, offsetof(mavlink_rocket_flight_tm_t, nas_state) }, \
{ "ada_state", NULL, MAVLINK_TYPE_UINT8_T, 0, 164, offsetof(mavlink_rocket_flight_tm_t, ada_state) }, \
{ "fmm_state", NULL, MAVLINK_TYPE_UINT8_T, 0, 165, offsetof(mavlink_rocket_flight_tm_t, fmm_state) }, \
{ "dpl_state", NULL, MAVLINK_TYPE_UINT8_T, 0, 166, offsetof(mavlink_rocket_flight_tm_t, dpl_state) }, \
{ "abk_state", NULL, MAVLINK_TYPE_UINT8_T, 0, 167, offsetof(mavlink_rocket_flight_tm_t, abk_state) }, \
{ "nas_state", NULL, MAVLINK_TYPE_UINT8_T, 0, 168, offsetof(mavlink_rocket_flight_tm_t, nas_state) }, \
{ "mea_state", NULL, MAVLINK_TYPE_UINT8_T, 0, 169, offsetof(mavlink_rocket_flight_tm_t, mea_state) }, \
{ "pressure_ada", NULL, MAVLINK_TYPE_FLOAT, 0, 8, offsetof(mavlink_rocket_flight_tm_t, pressure_ada) }, \
{ "pressure_digi", NULL, MAVLINK_TYPE_FLOAT, 0, 12, offsetof(mavlink_rocket_flight_tm_t, pressure_digi) }, \
{ "pressure_static", NULL, MAVLINK_TYPE_FLOAT, 0, 16, offsetof(mavlink_rocket_flight_tm_t, pressure_static) }, \
......@@ -85,55 +88,57 @@ typedef struct __mavlink_rocket_flight_tm_t {
{ "airspeed_pitot", NULL, MAVLINK_TYPE_FLOAT, 0, 24, offsetof(mavlink_rocket_flight_tm_t, airspeed_pitot) }, \
{ "altitude_agl", NULL, MAVLINK_TYPE_FLOAT, 0, 28, offsetof(mavlink_rocket_flight_tm_t, altitude_agl) }, \
{ "ada_vert_speed", NULL, MAVLINK_TYPE_FLOAT, 0, 32, offsetof(mavlink_rocket_flight_tm_t, ada_vert_speed) }, \
{ "acc_x", NULL, MAVLINK_TYPE_FLOAT, 0, 36, offsetof(mavlink_rocket_flight_tm_t, acc_x) }, \
{ "acc_y", NULL, MAVLINK_TYPE_FLOAT, 0, 40, offsetof(mavlink_rocket_flight_tm_t, acc_y) }, \
{ "acc_z", NULL, MAVLINK_TYPE_FLOAT, 0, 44, offsetof(mavlink_rocket_flight_tm_t, acc_z) }, \
{ "gyro_x", NULL, MAVLINK_TYPE_FLOAT, 0, 48, offsetof(mavlink_rocket_flight_tm_t, gyro_x) }, \
{ "gyro_y", NULL, MAVLINK_TYPE_FLOAT, 0, 52, offsetof(mavlink_rocket_flight_tm_t, gyro_y) }, \
{ "gyro_z", NULL, MAVLINK_TYPE_FLOAT, 0, 56, offsetof(mavlink_rocket_flight_tm_t, gyro_z) }, \
{ "mag_x", NULL, MAVLINK_TYPE_FLOAT, 0, 60, offsetof(mavlink_rocket_flight_tm_t, mag_x) }, \
{ "mag_y", NULL, MAVLINK_TYPE_FLOAT, 0, 64, offsetof(mavlink_rocket_flight_tm_t, mag_y) }, \
{ "mag_z", NULL, MAVLINK_TYPE_FLOAT, 0, 68, offsetof(mavlink_rocket_flight_tm_t, mag_z) }, \
{ "gps_fix", NULL, MAVLINK_TYPE_UINT8_T, 0, 165, offsetof(mavlink_rocket_flight_tm_t, gps_fix) }, \
{ "gps_lat", NULL, MAVLINK_TYPE_FLOAT, 0, 72, offsetof(mavlink_rocket_flight_tm_t, gps_lat) }, \
{ "gps_lon", NULL, MAVLINK_TYPE_FLOAT, 0, 76, offsetof(mavlink_rocket_flight_tm_t, gps_lon) }, \
{ "gps_alt", NULL, MAVLINK_TYPE_FLOAT, 0, 80, offsetof(mavlink_rocket_flight_tm_t, gps_alt) }, \
{ "abk_angle", NULL, MAVLINK_TYPE_FLOAT, 0, 84, offsetof(mavlink_rocket_flight_tm_t, abk_angle) }, \
{ "abk_estimated_cd", NULL, MAVLINK_TYPE_FLOAT, 0, 88, offsetof(mavlink_rocket_flight_tm_t, abk_estimated_cd) }, \
{ "parachute_load", NULL, MAVLINK_TYPE_FLOAT, 0, 92, offsetof(mavlink_rocket_flight_tm_t, parachute_load) }, \
{ "nas_n", NULL, MAVLINK_TYPE_FLOAT, 0, 96, offsetof(mavlink_rocket_flight_tm_t, nas_n) }, \
{ "nas_e", NULL, MAVLINK_TYPE_FLOAT, 0, 100, offsetof(mavlink_rocket_flight_tm_t, nas_e) }, \
{ "nas_d", NULL, MAVLINK_TYPE_FLOAT, 0, 104, offsetof(mavlink_rocket_flight_tm_t, nas_d) }, \
{ "nas_vn", NULL, MAVLINK_TYPE_FLOAT, 0, 108, offsetof(mavlink_rocket_flight_tm_t, nas_vn) }, \
{ "nas_ve", NULL, MAVLINK_TYPE_FLOAT, 0, 112, offsetof(mavlink_rocket_flight_tm_t, nas_ve) }, \
{ "nas_vd", NULL, MAVLINK_TYPE_FLOAT, 0, 116, offsetof(mavlink_rocket_flight_tm_t, nas_vd) }, \
{ "nas_qx", NULL, MAVLINK_TYPE_FLOAT, 0, 120, offsetof(mavlink_rocket_flight_tm_t, nas_qx) }, \
{ "nas_qy", NULL, MAVLINK_TYPE_FLOAT, 0, 124, offsetof(mavlink_rocket_flight_tm_t, nas_qy) }, \
{ "nas_qz", NULL, MAVLINK_TYPE_FLOAT, 0, 128, offsetof(mavlink_rocket_flight_tm_t, nas_qz) }, \
{ "nas_qw", NULL, MAVLINK_TYPE_FLOAT, 0, 132, offsetof(mavlink_rocket_flight_tm_t, nas_qw) }, \
{ "nas_bias_x", NULL, MAVLINK_TYPE_FLOAT, 0, 136, offsetof(mavlink_rocket_flight_tm_t, nas_bias_x) }, \
{ "nas_bias_y", NULL, MAVLINK_TYPE_FLOAT, 0, 140, offsetof(mavlink_rocket_flight_tm_t, nas_bias_y) }, \
{ "nas_bias_z", NULL, MAVLINK_TYPE_FLOAT, 0, 144, offsetof(mavlink_rocket_flight_tm_t, nas_bias_z) }, \
{ "pin_launch", NULL, MAVLINK_TYPE_UINT8_T, 0, 166, offsetof(mavlink_rocket_flight_tm_t, pin_launch) }, \
{ "pin_nosecone", NULL, MAVLINK_TYPE_UINT8_T, 0, 167, offsetof(mavlink_rocket_flight_tm_t, pin_nosecone) }, \
{ "pin_expulsion", NULL, MAVLINK_TYPE_UINT8_T, 0, 168, offsetof(mavlink_rocket_flight_tm_t, pin_expulsion) }, \
{ "cutter_presence", NULL, MAVLINK_TYPE_UINT8_T, 0, 169, offsetof(mavlink_rocket_flight_tm_t, cutter_presence) }, \
{ "estimated_thrust", NULL, MAVLINK_TYPE_FLOAT, 0, 148, offsetof(mavlink_rocket_flight_tm_t, estimated_thrust) }, \
{ "vbat", NULL, MAVLINK_TYPE_FLOAT, 0, 152, offsetof(mavlink_rocket_flight_tm_t, vbat) }, \
{ "temperature", NULL, MAVLINK_TYPE_FLOAT, 0, 156, offsetof(mavlink_rocket_flight_tm_t, temperature) }, \
{ "logger_error", NULL, MAVLINK_TYPE_INT8_T, 0, 170, offsetof(mavlink_rocket_flight_tm_t, logger_error) }, \
{ "mea_mass", NULL, MAVLINK_TYPE_FLOAT, 0, 36, offsetof(mavlink_rocket_flight_tm_t, mea_mass) }, \
{ "acc_x", NULL, MAVLINK_TYPE_FLOAT, 0, 40, offsetof(mavlink_rocket_flight_tm_t, acc_x) }, \
{ "acc_y", NULL, MAVLINK_TYPE_FLOAT, 0, 44, offsetof(mavlink_rocket_flight_tm_t, acc_y) }, \
{ "acc_z", NULL, MAVLINK_TYPE_FLOAT, 0, 48, offsetof(mavlink_rocket_flight_tm_t, acc_z) }, \
{ "gyro_x", NULL, MAVLINK_TYPE_FLOAT, 0, 52, offsetof(mavlink_rocket_flight_tm_t, gyro_x) }, \
{ "gyro_y", NULL, MAVLINK_TYPE_FLOAT, 0, 56, offsetof(mavlink_rocket_flight_tm_t, gyro_y) }, \
{ "gyro_z", NULL, MAVLINK_TYPE_FLOAT, 0, 60, offsetof(mavlink_rocket_flight_tm_t, gyro_z) }, \
{ "mag_x", NULL, MAVLINK_TYPE_FLOAT, 0, 64, offsetof(mavlink_rocket_flight_tm_t, mag_x) }, \
{ "mag_y", NULL, MAVLINK_TYPE_FLOAT, 0, 68, offsetof(mavlink_rocket_flight_tm_t, mag_y) }, \
{ "mag_z", NULL, MAVLINK_TYPE_FLOAT, 0, 72, offsetof(mavlink_rocket_flight_tm_t, mag_z) }, \
{ "gps_fix", NULL, MAVLINK_TYPE_UINT8_T, 0, 170, offsetof(mavlink_rocket_flight_tm_t, gps_fix) }, \
{ "gps_lat", NULL, MAVLINK_TYPE_FLOAT, 0, 76, offsetof(mavlink_rocket_flight_tm_t, gps_lat) }, \
{ "gps_lon", NULL, MAVLINK_TYPE_FLOAT, 0, 80, offsetof(mavlink_rocket_flight_tm_t, gps_lon) }, \
{ "gps_alt", NULL, MAVLINK_TYPE_FLOAT, 0, 84, offsetof(mavlink_rocket_flight_tm_t, gps_alt) }, \
{ "abk_angle", NULL, MAVLINK_TYPE_FLOAT, 0, 88, offsetof(mavlink_rocket_flight_tm_t, abk_angle) }, \
{ "nas_n", NULL, MAVLINK_TYPE_FLOAT, 0, 92, offsetof(mavlink_rocket_flight_tm_t, nas_n) }, \
{ "nas_e", NULL, MAVLINK_TYPE_FLOAT, 0, 96, offsetof(mavlink_rocket_flight_tm_t, nas_e) }, \
{ "nas_d", NULL, MAVLINK_TYPE_FLOAT, 0, 100, offsetof(mavlink_rocket_flight_tm_t, nas_d) }, \
{ "nas_vn", NULL, MAVLINK_TYPE_FLOAT, 0, 104, offsetof(mavlink_rocket_flight_tm_t, nas_vn) }, \
{ "nas_ve", NULL, MAVLINK_TYPE_FLOAT, 0, 108, offsetof(mavlink_rocket_flight_tm_t, nas_ve) }, \
{ "nas_vd", NULL, MAVLINK_TYPE_FLOAT, 0, 112, offsetof(mavlink_rocket_flight_tm_t, nas_vd) }, \
{ "nas_qx", NULL, MAVLINK_TYPE_FLOAT, 0, 116, offsetof(mavlink_rocket_flight_tm_t, nas_qx) }, \
{ "nas_qy", NULL, MAVLINK_TYPE_FLOAT, 0, 120, offsetof(mavlink_rocket_flight_tm_t, nas_qy) }, \
{ "nas_qz", NULL, MAVLINK_TYPE_FLOAT, 0, 124, offsetof(mavlink_rocket_flight_tm_t, nas_qz) }, \
{ "nas_qw", NULL, MAVLINK_TYPE_FLOAT, 0, 128, offsetof(mavlink_rocket_flight_tm_t, nas_qw) }, \
{ "nas_bias_x", NULL, MAVLINK_TYPE_FLOAT, 0, 132, offsetof(mavlink_rocket_flight_tm_t, nas_bias_x) }, \
{ "nas_bias_y", NULL, MAVLINK_TYPE_FLOAT, 0, 136, offsetof(mavlink_rocket_flight_tm_t, nas_bias_y) }, \
{ "nas_bias_z", NULL, MAVLINK_TYPE_FLOAT, 0, 140, offsetof(mavlink_rocket_flight_tm_t, nas_bias_z) }, \
{ "pin_quick_connector", NULL, MAVLINK_TYPE_FLOAT, 0, 144, offsetof(mavlink_rocket_flight_tm_t, pin_quick_connector) }, \
{ "pin_launch", NULL, MAVLINK_TYPE_UINT8_T, 0, 171, offsetof(mavlink_rocket_flight_tm_t, pin_launch) }, \
{ "pin_nosecone", NULL, MAVLINK_TYPE_UINT8_T, 0, 172, offsetof(mavlink_rocket_flight_tm_t, pin_nosecone) }, \
{ "pin_expulsion", NULL, MAVLINK_TYPE_UINT8_T, 0, 173, offsetof(mavlink_rocket_flight_tm_t, pin_expulsion) }, \
{ "cutter_presence", NULL, MAVLINK_TYPE_UINT8_T, 0, 174, offsetof(mavlink_rocket_flight_tm_t, cutter_presence) }, \
{ "battery_voltage", NULL, MAVLINK_TYPE_FLOAT, 0, 148, offsetof(mavlink_rocket_flight_tm_t, battery_voltage) }, \
{ "cam_battery_voltage", NULL, MAVLINK_TYPE_FLOAT, 0, 152, offsetof(mavlink_rocket_flight_tm_t, cam_battery_voltage) }, \
{ "current_consumption", NULL, MAVLINK_TYPE_FLOAT, 0, 156, offsetof(mavlink_rocket_flight_tm_t, current_consumption) }, \
{ "temperature", NULL, MAVLINK_TYPE_FLOAT, 0, 160, offsetof(mavlink_rocket_flight_tm_t, temperature) }, \
{ "logger_error", NULL, MAVLINK_TYPE_INT8_T, 0, 175, offsetof(mavlink_rocket_flight_tm_t, logger_error) }, \
} \
}
#else
#define MAVLINK_MESSAGE_INFO_ROCKET_FLIGHT_TM { \
"ROCKET_FLIGHT_TM", \
50, \
52, \
{ { "timestamp", NULL, MAVLINK_TYPE_UINT64_T, 0, 0, offsetof(mavlink_rocket_flight_tm_t, timestamp) }, \
{ "ada_state", NULL, MAVLINK_TYPE_UINT8_T, 0, 160, offsetof(mavlink_rocket_flight_tm_t, ada_state) }, \
{ "fmm_state", NULL, MAVLINK_TYPE_UINT8_T, 0, 161, offsetof(mavlink_rocket_flight_tm_t, fmm_state) }, \
{ "dpl_state", NULL, MAVLINK_TYPE_UINT8_T, 0, 162, offsetof(mavlink_rocket_flight_tm_t, dpl_state) }, \
{ "abk_state", NULL, MAVLINK_TYPE_UINT8_T, 0, 163, offsetof(mavlink_rocket_flight_tm_t, abk_state) }, \
{ "nas_state", NULL, MAVLINK_TYPE_UINT8_T, 0, 164, offsetof(mavlink_rocket_flight_tm_t, nas_state) }, \
{ "ada_state", NULL, MAVLINK_TYPE_UINT8_T, 0, 164, offsetof(mavlink_rocket_flight_tm_t, ada_state) }, \
{ "fmm_state", NULL, MAVLINK_TYPE_UINT8_T, 0, 165, offsetof(mavlink_rocket_flight_tm_t, fmm_state) }, \
{ "dpl_state", NULL, MAVLINK_TYPE_UINT8_T, 0, 166, offsetof(mavlink_rocket_flight_tm_t, dpl_state) }, \
{ "abk_state", NULL, MAVLINK_TYPE_UINT8_T, 0, 167, offsetof(mavlink_rocket_flight_tm_t, abk_state) }, \
{ "nas_state", NULL, MAVLINK_TYPE_UINT8_T, 0, 168, offsetof(mavlink_rocket_flight_tm_t, nas_state) }, \
{ "mea_state", NULL, MAVLINK_TYPE_UINT8_T, 0, 169, offsetof(mavlink_rocket_flight_tm_t, mea_state) }, \
{ "pressure_ada", NULL, MAVLINK_TYPE_FLOAT, 0, 8, offsetof(mavlink_rocket_flight_tm_t, pressure_ada) }, \
{ "pressure_digi", NULL, MAVLINK_TYPE_FLOAT, 0, 12, offsetof(mavlink_rocket_flight_tm_t, pressure_digi) }, \
{ "pressure_static", NULL, MAVLINK_TYPE_FLOAT, 0, 16, offsetof(mavlink_rocket_flight_tm_t, pressure_static) }, \
......@@ -141,43 +146,44 @@ typedef struct __mavlink_rocket_flight_tm_t {
{ "airspeed_pitot", NULL, MAVLINK_TYPE_FLOAT, 0, 24, offsetof(mavlink_rocket_flight_tm_t, airspeed_pitot) }, \
{ "altitude_agl", NULL, MAVLINK_TYPE_FLOAT, 0, 28, offsetof(mavlink_rocket_flight_tm_t, altitude_agl) }, \
{ "ada_vert_speed", NULL, MAVLINK_TYPE_FLOAT, 0, 32, offsetof(mavlink_rocket_flight_tm_t, ada_vert_speed) }, \
{ "acc_x", NULL, MAVLINK_TYPE_FLOAT, 0, 36, offsetof(mavlink_rocket_flight_tm_t, acc_x) }, \
{ "acc_y", NULL, MAVLINK_TYPE_FLOAT, 0, 40, offsetof(mavlink_rocket_flight_tm_t, acc_y) }, \
{ "acc_z", NULL, MAVLINK_TYPE_FLOAT, 0, 44, offsetof(mavlink_rocket_flight_tm_t, acc_z) }, \
{ "gyro_x", NULL, MAVLINK_TYPE_FLOAT, 0, 48, offsetof(mavlink_rocket_flight_tm_t, gyro_x) }, \
{ "gyro_y", NULL, MAVLINK_TYPE_FLOAT, 0, 52, offsetof(mavlink_rocket_flight_tm_t, gyro_y) }, \
{ "gyro_z", NULL, MAVLINK_TYPE_FLOAT, 0, 56, offsetof(mavlink_rocket_flight_tm_t, gyro_z) }, \
{ "mag_x", NULL, MAVLINK_TYPE_FLOAT, 0, 60, offsetof(mavlink_rocket_flight_tm_t, mag_x) }, \
{ "mag_y", NULL, MAVLINK_TYPE_FLOAT, 0, 64, offsetof(mavlink_rocket_flight_tm_t, mag_y) }, \
{ "mag_z", NULL, MAVLINK_TYPE_FLOAT, 0, 68, offsetof(mavlink_rocket_flight_tm_t, mag_z) }, \
{ "gps_fix", NULL, MAVLINK_TYPE_UINT8_T, 0, 165, offsetof(mavlink_rocket_flight_tm_t, gps_fix) }, \
{ "gps_lat", NULL, MAVLINK_TYPE_FLOAT, 0, 72, offsetof(mavlink_rocket_flight_tm_t, gps_lat) }, \
{ "gps_lon", NULL, MAVLINK_TYPE_FLOAT, 0, 76, offsetof(mavlink_rocket_flight_tm_t, gps_lon) }, \
{ "gps_alt", NULL, MAVLINK_TYPE_FLOAT, 0, 80, offsetof(mavlink_rocket_flight_tm_t, gps_alt) }, \
{ "abk_angle", NULL, MAVLINK_TYPE_FLOAT, 0, 84, offsetof(mavlink_rocket_flight_tm_t, abk_angle) }, \
{ "abk_estimated_cd", NULL, MAVLINK_TYPE_FLOAT, 0, 88, offsetof(mavlink_rocket_flight_tm_t, abk_estimated_cd) }, \
{ "parachute_load", NULL, MAVLINK_TYPE_FLOAT, 0, 92, offsetof(mavlink_rocket_flight_tm_t, parachute_load) }, \
{ "nas_n", NULL, MAVLINK_TYPE_FLOAT, 0, 96, offsetof(mavlink_rocket_flight_tm_t, nas_n) }, \
{ "nas_e", NULL, MAVLINK_TYPE_FLOAT, 0, 100, offsetof(mavlink_rocket_flight_tm_t, nas_e) }, \
{ "nas_d", NULL, MAVLINK_TYPE_FLOAT, 0, 104, offsetof(mavlink_rocket_flight_tm_t, nas_d) }, \
{ "nas_vn", NULL, MAVLINK_TYPE_FLOAT, 0, 108, offsetof(mavlink_rocket_flight_tm_t, nas_vn) }, \
{ "nas_ve", NULL, MAVLINK_TYPE_FLOAT, 0, 112, offsetof(mavlink_rocket_flight_tm_t, nas_ve) }, \
{ "nas_vd", NULL, MAVLINK_TYPE_FLOAT, 0, 116, offsetof(mavlink_rocket_flight_tm_t, nas_vd) }, \
{ "nas_qx", NULL, MAVLINK_TYPE_FLOAT, 0, 120, offsetof(mavlink_rocket_flight_tm_t, nas_qx) }, \
{ "nas_qy", NULL, MAVLINK_TYPE_FLOAT, 0, 124, offsetof(mavlink_rocket_flight_tm_t, nas_qy) }, \
{ "nas_qz", NULL, MAVLINK_TYPE_FLOAT, 0, 128, offsetof(mavlink_rocket_flight_tm_t, nas_qz) }, \
{ "nas_qw", NULL, MAVLINK_TYPE_FLOAT, 0, 132, offsetof(mavlink_rocket_flight_tm_t, nas_qw) }, \
{ "nas_bias_x", NULL, MAVLINK_TYPE_FLOAT, 0, 136, offsetof(mavlink_rocket_flight_tm_t, nas_bias_x) }, \
{ "nas_bias_y", NULL, MAVLINK_TYPE_FLOAT, 0, 140, offsetof(mavlink_rocket_flight_tm_t, nas_bias_y) }, \
{ "nas_bias_z", NULL, MAVLINK_TYPE_FLOAT, 0, 144, offsetof(mavlink_rocket_flight_tm_t, nas_bias_z) }, \
{ "pin_launch", NULL, MAVLINK_TYPE_UINT8_T, 0, 166, offsetof(mavlink_rocket_flight_tm_t, pin_launch) }, \
{ "pin_nosecone", NULL, MAVLINK_TYPE_UINT8_T, 0, 167, offsetof(mavlink_rocket_flight_tm_t, pin_nosecone) }, \
{ "pin_expulsion", NULL, MAVLINK_TYPE_UINT8_T, 0, 168, offsetof(mavlink_rocket_flight_tm_t, pin_expulsion) }, \
{ "cutter_presence", NULL, MAVLINK_TYPE_UINT8_T, 0, 169, offsetof(mavlink_rocket_flight_tm_t, cutter_presence) }, \
{ "estimated_thrust", NULL, MAVLINK_TYPE_FLOAT, 0, 148, offsetof(mavlink_rocket_flight_tm_t, estimated_thrust) }, \
{ "vbat", NULL, MAVLINK_TYPE_FLOAT, 0, 152, offsetof(mavlink_rocket_flight_tm_t, vbat) }, \
{ "temperature", NULL, MAVLINK_TYPE_FLOAT, 0, 156, offsetof(mavlink_rocket_flight_tm_t, temperature) }, \
{ "logger_error", NULL, MAVLINK_TYPE_INT8_T, 0, 170, offsetof(mavlink_rocket_flight_tm_t, logger_error) }, \
{ "mea_mass", NULL, MAVLINK_TYPE_FLOAT, 0, 36, offsetof(mavlink_rocket_flight_tm_t, mea_mass) }, \
{ "acc_x", NULL, MAVLINK_TYPE_FLOAT, 0, 40, offsetof(mavlink_rocket_flight_tm_t, acc_x) }, \
{ "acc_y", NULL, MAVLINK_TYPE_FLOAT, 0, 44, offsetof(mavlink_rocket_flight_tm_t, acc_y) }, \
{ "acc_z", NULL, MAVLINK_TYPE_FLOAT, 0, 48, offsetof(mavlink_rocket_flight_tm_t, acc_z) }, \
{ "gyro_x", NULL, MAVLINK_TYPE_FLOAT, 0, 52, offsetof(mavlink_rocket_flight_tm_t, gyro_x) }, \
{ "gyro_y", NULL, MAVLINK_TYPE_FLOAT, 0, 56, offsetof(mavlink_rocket_flight_tm_t, gyro_y) }, \
{ "gyro_z", NULL, MAVLINK_TYPE_FLOAT, 0, 60, offsetof(mavlink_rocket_flight_tm_t, gyro_z) }, \
{ "mag_x", NULL, MAVLINK_TYPE_FLOAT, 0, 64, offsetof(mavlink_rocket_flight_tm_t, mag_x) }, \
{ "mag_y", NULL, MAVLINK_TYPE_FLOAT, 0, 68, offsetof(mavlink_rocket_flight_tm_t, mag_y) }, \
{ "mag_z", NULL, MAVLINK_TYPE_FLOAT, 0, 72, offsetof(mavlink_rocket_flight_tm_t, mag_z) }, \
{ "gps_fix", NULL, MAVLINK_TYPE_UINT8_T, 0, 170, offsetof(mavlink_rocket_flight_tm_t, gps_fix) }, \
{ "gps_lat", NULL, MAVLINK_TYPE_FLOAT, 0, 76, offsetof(mavlink_rocket_flight_tm_t, gps_lat) }, \
{ "gps_lon", NULL, MAVLINK_TYPE_FLOAT, 0, 80, offsetof(mavlink_rocket_flight_tm_t, gps_lon) }, \
{ "gps_alt", NULL, MAVLINK_TYPE_FLOAT, 0, 84, offsetof(mavlink_rocket_flight_tm_t, gps_alt) }, \
{ "abk_angle", NULL, MAVLINK_TYPE_FLOAT, 0, 88, offsetof(mavlink_rocket_flight_tm_t, abk_angle) }, \
{ "nas_n", NULL, MAVLINK_TYPE_FLOAT, 0, 92, offsetof(mavlink_rocket_flight_tm_t, nas_n) }, \
{ "nas_e", NULL, MAVLINK_TYPE_FLOAT, 0, 96, offsetof(mavlink_rocket_flight_tm_t, nas_e) }, \
{ "nas_d", NULL, MAVLINK_TYPE_FLOAT, 0, 100, offsetof(mavlink_rocket_flight_tm_t, nas_d) }, \
{ "nas_vn", NULL, MAVLINK_TYPE_FLOAT, 0, 104, offsetof(mavlink_rocket_flight_tm_t, nas_vn) }, \
{ "nas_ve", NULL, MAVLINK_TYPE_FLOAT, 0, 108, offsetof(mavlink_rocket_flight_tm_t, nas_ve) }, \
{ "nas_vd", NULL, MAVLINK_TYPE_FLOAT, 0, 112, offsetof(mavlink_rocket_flight_tm_t, nas_vd) }, \
{ "nas_qx", NULL, MAVLINK_TYPE_FLOAT, 0, 116, offsetof(mavlink_rocket_flight_tm_t, nas_qx) }, \
{ "nas_qy", NULL, MAVLINK_TYPE_FLOAT, 0, 120, offsetof(mavlink_rocket_flight_tm_t, nas_qy) }, \
{ "nas_qz", NULL, MAVLINK_TYPE_FLOAT, 0, 124, offsetof(mavlink_rocket_flight_tm_t, nas_qz) }, \
{ "nas_qw", NULL, MAVLINK_TYPE_FLOAT, 0, 128, offsetof(mavlink_rocket_flight_tm_t, nas_qw) }, \
{ "nas_bias_x", NULL, MAVLINK_TYPE_FLOAT, 0, 132, offsetof(mavlink_rocket_flight_tm_t, nas_bias_x) }, \
{ "nas_bias_y", NULL, MAVLINK_TYPE_FLOAT, 0, 136, offsetof(mavlink_rocket_flight_tm_t, nas_bias_y) }, \
{ "nas_bias_z", NULL, MAVLINK_TYPE_FLOAT, 0, 140, offsetof(mavlink_rocket_flight_tm_t, nas_bias_z) }, \
{ "pin_quick_connector", NULL, MAVLINK_TYPE_FLOAT, 0, 144, offsetof(mavlink_rocket_flight_tm_t, pin_quick_connector) }, \
{ "pin_launch", NULL, MAVLINK_TYPE_UINT8_T, 0, 171, offsetof(mavlink_rocket_flight_tm_t, pin_launch) }, \
{ "pin_nosecone", NULL, MAVLINK_TYPE_UINT8_T, 0, 172, offsetof(mavlink_rocket_flight_tm_t, pin_nosecone) }, \
{ "pin_expulsion", NULL, MAVLINK_TYPE_UINT8_T, 0, 173, offsetof(mavlink_rocket_flight_tm_t, pin_expulsion) }, \
{ "cutter_presence", NULL, MAVLINK_TYPE_UINT8_T, 0, 174, offsetof(mavlink_rocket_flight_tm_t, cutter_presence) }, \
{ "battery_voltage", NULL, MAVLINK_TYPE_FLOAT, 0, 148, offsetof(mavlink_rocket_flight_tm_t, battery_voltage) }, \
{ "cam_battery_voltage", NULL, MAVLINK_TYPE_FLOAT, 0, 152, offsetof(mavlink_rocket_flight_tm_t, cam_battery_voltage) }, \
{ "current_consumption", NULL, MAVLINK_TYPE_FLOAT, 0, 156, offsetof(mavlink_rocket_flight_tm_t, current_consumption) }, \
{ "temperature", NULL, MAVLINK_TYPE_FLOAT, 0, 160, offsetof(mavlink_rocket_flight_tm_t, temperature) }, \
{ "logger_error", NULL, MAVLINK_TYPE_INT8_T, 0, 175, offsetof(mavlink_rocket_flight_tm_t, logger_error) }, \
} \
}
#endif
......@@ -194,6 +200,7 @@ typedef struct __mavlink_rocket_flight_tm_t {
* @param dpl_state Deployment Controller State
* @param abk_state Airbrake FSM state
* @param nas_state Navigation System FSM State
* @param mea_state MEA Controller State
* @param pressure_ada [Pa] Atmospheric pressure estimated by ADA
* @param pressure_digi [Pa] Pressure from digital sensor
* @param pressure_static [Pa] Pressure from static port
......@@ -201,6 +208,7 @@ typedef struct __mavlink_rocket_flight_tm_t {
* @param airspeed_pitot [m/s] Pitot airspeed
* @param altitude_agl [m] Altitude above ground level
* @param ada_vert_speed [m/s] Vertical speed estimated by ADA
* @param mea_mass [kg] Mass estimated by MEA
* @param acc_x [m/s^2] Acceleration on X axis (body)
* @param acc_y [m/s^2] Acceleration on Y axis (body)
* @param acc_z [m/s^2] Acceleration on Z axis (body)
......@@ -215,8 +223,6 @@ typedef struct __mavlink_rocket_flight_tm_t {
* @param gps_lon [deg] Longitude
* @param gps_alt [m] GPS Altitude
* @param abk_angle [deg] Air Brakes angle
* @param abk_estimated_cd Estimated drag coefficient
* @param parachute_load Parachute load cell value
* @param nas_n [deg] Navigation system estimated noth position
* @param nas_e [deg] Navigation system estimated east position
* @param nas_d [m] Navigation system estimated down position
......@@ -230,18 +236,20 @@ typedef struct __mavlink_rocket_flight_tm_t {
* @param nas_bias_x Navigation system gyroscope bias on x axis
* @param nas_bias_y Navigation system gyroscope bias on y axis
* @param nas_bias_z Navigation system gyroscope bias on z axis
* @param pin_quick_connector Quick connector detach pin
* @param pin_launch Launch pin status (1 = connected, 0 = disconnected)
* @param pin_nosecone Nosecone pin status (1 = connected, 0 = disconnected)
* @param pin_expulsion Servo sensor status (1 = actuated, 0 = idle)
* @param cutter_presence Cutter presence status (1 = present, 0 = missing)
* @param estimated_thrust Estimated thrust from automatic shutdown algorithm
* @param vbat [V] Battery voltage
* @param battery_voltage [V] Battery voltage
* @param cam_battery_voltage [V] Camera battery voltage
* @param current_consumption [A] Battery current
* @param temperature [degC] Temperature
* @param logger_error Logger error (0 = no error, -1 otherwise)
* @return length of the message in bytes (excluding serial stream start sign)
*/
static inline uint16_t mavlink_msg_rocket_flight_tm_pack(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg,
uint64_t timestamp, uint8_t ada_state, uint8_t fmm_state, uint8_t dpl_state, uint8_t abk_state, uint8_t nas_state, float pressure_ada, float pressure_digi, float pressure_static, float pressure_dpl, float airspeed_pitot, float altitude_agl, float ada_vert_speed, float acc_x, float acc_y, float acc_z, float gyro_x, float gyro_y, float gyro_z, float mag_x, float mag_y, float mag_z, uint8_t gps_fix, float gps_lat, float gps_lon, float gps_alt, float abk_angle, float abk_estimated_cd, float parachute_load, float nas_n, float nas_e, float nas_d, float nas_vn, float nas_ve, float nas_vd, float nas_qx, float nas_qy, float nas_qz, float nas_qw, float nas_bias_x, float nas_bias_y, float nas_bias_z, uint8_t pin_launch, uint8_t pin_nosecone, uint8_t pin_expulsion, uint8_t cutter_presence, float estimated_thrust, float vbat, float temperature, int8_t logger_error)
uint64_t timestamp, uint8_t ada_state, uint8_t fmm_state, uint8_t dpl_state, uint8_t abk_state, uint8_t nas_state, uint8_t mea_state, float pressure_ada, float pressure_digi, float pressure_static, float pressure_dpl, float airspeed_pitot, float altitude_agl, float ada_vert_speed, float mea_mass, float acc_x, float acc_y, float acc_z, float gyro_x, float gyro_y, float gyro_z, float mag_x, float mag_y, float mag_z, uint8_t gps_fix, float gps_lat, float gps_lon, float gps_alt, float abk_angle, float nas_n, float nas_e, float nas_d, float nas_vn, float nas_ve, float nas_vd, float nas_qx, float nas_qy, float nas_qz, float nas_qw, float nas_bias_x, float nas_bias_y, float nas_bias_z, float pin_quick_connector, uint8_t pin_launch, uint8_t pin_nosecone, uint8_t pin_expulsion, uint8_t cutter_presence, float battery_voltage, float cam_battery_voltage, float current_consumption, float temperature, int8_t logger_error)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char buf[MAVLINK_MSG_ID_ROCKET_FLIGHT_TM_LEN];
......@@ -253,48 +261,50 @@ static inline uint16_t mavlink_msg_rocket_flight_tm_pack(uint8_t system_id, uint
_mav_put_float(buf, 24, airspeed_pitot);
_mav_put_float(buf, 28, altitude_agl);
_mav_put_float(buf, 32, ada_vert_speed);
_mav_put_float(buf, 36, acc_x);
_mav_put_float(buf, 40, acc_y);
_mav_put_float(buf, 44, acc_z);
_mav_put_float(buf, 48, gyro_x);
_mav_put_float(buf, 52, gyro_y);
_mav_put_float(buf, 56, gyro_z);
_mav_put_float(buf, 60, mag_x);
_mav_put_float(buf, 64, mag_y);
_mav_put_float(buf, 68, mag_z);
_mav_put_float(buf, 72, gps_lat);
_mav_put_float(buf, 76, gps_lon);
_mav_put_float(buf, 80, gps_alt);
_mav_put_float(buf, 84, abk_angle);
_mav_put_float(buf, 88, abk_estimated_cd);
_mav_put_float(buf, 92, parachute_load);
_mav_put_float(buf, 96, nas_n);
_mav_put_float(buf, 100, nas_e);
_mav_put_float(buf, 104, nas_d);
_mav_put_float(buf, 108, nas_vn);
_mav_put_float(buf, 112, nas_ve);
_mav_put_float(buf, 116, nas_vd);
_mav_put_float(buf, 120, nas_qx);
_mav_put_float(buf, 124, nas_qy);
_mav_put_float(buf, 128, nas_qz);
_mav_put_float(buf, 132, nas_qw);
_mav_put_float(buf, 136, nas_bias_x);
_mav_put_float(buf, 140, nas_bias_y);
_mav_put_float(buf, 144, nas_bias_z);
_mav_put_float(buf, 148, estimated_thrust);
_mav_put_float(buf, 152, vbat);
_mav_put_float(buf, 156, temperature);
_mav_put_uint8_t(buf, 160, ada_state);
_mav_put_uint8_t(buf, 161, fmm_state);
_mav_put_uint8_t(buf, 162, dpl_state);
_mav_put_uint8_t(buf, 163, abk_state);
_mav_put_uint8_t(buf, 164, nas_state);
_mav_put_uint8_t(buf, 165, gps_fix);
_mav_put_uint8_t(buf, 166, pin_launch);
_mav_put_uint8_t(buf, 167, pin_nosecone);
_mav_put_uint8_t(buf, 168, pin_expulsion);
_mav_put_uint8_t(buf, 169, cutter_presence);
_mav_put_int8_t(buf, 170, logger_error);
_mav_put_float(buf, 36, mea_mass);
_mav_put_float(buf, 40, acc_x);
_mav_put_float(buf, 44, acc_y);
_mav_put_float(buf, 48, acc_z);
_mav_put_float(buf, 52, gyro_x);
_mav_put_float(buf, 56, gyro_y);
_mav_put_float(buf, 60, gyro_z);
_mav_put_float(buf, 64, mag_x);
_mav_put_float(buf, 68, mag_y);
_mav_put_float(buf, 72, mag_z);
_mav_put_float(buf, 76, gps_lat);
_mav_put_float(buf, 80, gps_lon);
_mav_put_float(buf, 84, gps_alt);
_mav_put_float(buf, 88, abk_angle);
_mav_put_float(buf, 92, nas_n);
_mav_put_float(buf, 96, nas_e);
_mav_put_float(buf, 100, nas_d);
_mav_put_float(buf, 104, nas_vn);
_mav_put_float(buf, 108, nas_ve);
_mav_put_float(buf, 112, nas_vd);
_mav_put_float(buf, 116, nas_qx);
_mav_put_float(buf, 120, nas_qy);
_mav_put_float(buf, 124, nas_qz);
_mav_put_float(buf, 128, nas_qw);
_mav_put_float(buf, 132, nas_bias_x);
_mav_put_float(buf, 136, nas_bias_y);
_mav_put_float(buf, 140, nas_bias_z);
_mav_put_float(buf, 144, pin_quick_connector);
_mav_put_float(buf, 148, battery_voltage);
_mav_put_float(buf, 152, cam_battery_voltage);
_mav_put_float(buf, 156, current_consumption);
_mav_put_float(buf, 160, temperature);
_mav_put_uint8_t(buf, 164, ada_state);
_mav_put_uint8_t(buf, 165, fmm_state);
_mav_put_uint8_t(buf, 166, dpl_state);
_mav_put_uint8_t(buf, 167, abk_state);
_mav_put_uint8_t(buf, 168, nas_state);
_mav_put_uint8_t(buf, 169, mea_state);
_mav_put_uint8_t(buf, 170, gps_fix);
_mav_put_uint8_t(buf, 171, pin_launch);
_mav_put_uint8_t(buf, 172, pin_nosecone);
_mav_put_uint8_t(buf, 173, pin_expulsion);
_mav_put_uint8_t(buf, 174, cutter_presence);
_mav_put_int8_t(buf, 175, logger_error);
memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_ROCKET_FLIGHT_TM_LEN);
#else
......@@ -307,6 +317,7 @@ static inline uint16_t mavlink_msg_rocket_flight_tm_pack(uint8_t system_id, uint
packet.airspeed_pitot = airspeed_pitot;
packet.altitude_agl = altitude_agl;
packet.ada_vert_speed = ada_vert_speed;
packet.mea_mass = mea_mass;
packet.acc_x = acc_x;
packet.acc_y = acc_y;
packet.acc_z = acc_z;
......@@ -320,8 +331,6 @@ static inline uint16_t mavlink_msg_rocket_flight_tm_pack(uint8_t system_id, uint
packet.gps_lon = gps_lon;
packet.gps_alt = gps_alt;
packet.abk_angle = abk_angle;
packet.abk_estimated_cd = abk_estimated_cd;
packet.parachute_load = parachute_load;
packet.nas_n = nas_n;
packet.nas_e = nas_e;
packet.nas_d = nas_d;
......@@ -335,14 +344,17 @@ static inline uint16_t mavlink_msg_rocket_flight_tm_pack(uint8_t system_id, uint
packet.nas_bias_x = nas_bias_x;
packet.nas_bias_y = nas_bias_y;
packet.nas_bias_z = nas_bias_z;
packet.estimated_thrust = estimated_thrust;
packet.vbat = vbat;
packet.pin_quick_connector = pin_quick_connector;
packet.battery_voltage = battery_voltage;
packet.cam_battery_voltage = cam_battery_voltage;
packet.current_consumption = current_consumption;
packet.temperature = temperature;
packet.ada_state = ada_state;
packet.fmm_state = fmm_state;
packet.dpl_state = dpl_state;
packet.abk_state = abk_state;
packet.nas_state = nas_state;
packet.mea_state = mea_state;
packet.gps_fix = gps_fix;
packet.pin_launch = pin_launch;
packet.pin_nosecone = pin_nosecone;
......@@ -369,6 +381,7 @@ static inline uint16_t mavlink_msg_rocket_flight_tm_pack(uint8_t system_id, uint
* @param dpl_state Deployment Controller State
* @param abk_state Airbrake FSM state
* @param nas_state Navigation System FSM State
* @param mea_state MEA Controller State
* @param pressure_ada [Pa] Atmospheric pressure estimated by ADA
* @param pressure_digi [Pa] Pressure from digital sensor
* @param pressure_static [Pa] Pressure from static port
......@@ -376,6 +389,7 @@ static inline uint16_t mavlink_msg_rocket_flight_tm_pack(uint8_t system_id, uint
* @param airspeed_pitot [m/s] Pitot airspeed
* @param altitude_agl [m] Altitude above ground level
* @param ada_vert_speed [m/s] Vertical speed estimated by ADA
* @param mea_mass [kg] Mass estimated by MEA
* @param acc_x [m/s^2] Acceleration on X axis (body)
* @param acc_y [m/s^2] Acceleration on Y axis (body)
* @param acc_z [m/s^2] Acceleration on Z axis (body)
......@@ -390,8 +404,6 @@ static inline uint16_t mavlink_msg_rocket_flight_tm_pack(uint8_t system_id, uint
* @param gps_lon [deg] Longitude
* @param gps_alt [m] GPS Altitude
* @param abk_angle [deg] Air Brakes angle
* @param abk_estimated_cd Estimated drag coefficient
* @param parachute_load Parachute load cell value
* @param nas_n [deg] Navigation system estimated noth position
* @param nas_e [deg] Navigation system estimated east position
* @param nas_d [m] Navigation system estimated down position
......@@ -405,19 +417,21 @@ static inline uint16_t mavlink_msg_rocket_flight_tm_pack(uint8_t system_id, uint
* @param nas_bias_x Navigation system gyroscope bias on x axis
* @param nas_bias_y Navigation system gyroscope bias on y axis
* @param nas_bias_z Navigation system gyroscope bias on z axis
* @param pin_quick_connector Quick connector detach pin
* @param pin_launch Launch pin status (1 = connected, 0 = disconnected)
* @param pin_nosecone Nosecone pin status (1 = connected, 0 = disconnected)
* @param pin_expulsion Servo sensor status (1 = actuated, 0 = idle)
* @param cutter_presence Cutter presence status (1 = present, 0 = missing)
* @param estimated_thrust Estimated thrust from automatic shutdown algorithm
* @param vbat [V] Battery voltage
* @param battery_voltage [V] Battery voltage
* @param cam_battery_voltage [V] Camera battery voltage
* @param current_consumption [A] Battery current
* @param temperature [degC] Temperature
* @param logger_error Logger error (0 = no error, -1 otherwise)
* @return length of the message in bytes (excluding serial stream start sign)
*/
static inline uint16_t mavlink_msg_rocket_flight_tm_pack_chan(uint8_t system_id, uint8_t component_id, uint8_t chan,
mavlink_message_t* msg,
uint64_t timestamp,uint8_t ada_state,uint8_t fmm_state,uint8_t dpl_state,uint8_t abk_state,uint8_t nas_state,float pressure_ada,float pressure_digi,float pressure_static,float pressure_dpl,float airspeed_pitot,float altitude_agl,float ada_vert_speed,float acc_x,float acc_y,float acc_z,float gyro_x,float gyro_y,float gyro_z,float mag_x,float mag_y,float mag_z,uint8_t gps_fix,float gps_lat,float gps_lon,float gps_alt,float abk_angle,float abk_estimated_cd,float parachute_load,float nas_n,float nas_e,float nas_d,float nas_vn,float nas_ve,float nas_vd,float nas_qx,float nas_qy,float nas_qz,float nas_qw,float nas_bias_x,float nas_bias_y,float nas_bias_z,uint8_t pin_launch,uint8_t pin_nosecone,uint8_t pin_expulsion,uint8_t cutter_presence,float estimated_thrust,float vbat,float temperature,int8_t logger_error)
uint64_t timestamp,uint8_t ada_state,uint8_t fmm_state,uint8_t dpl_state,uint8_t abk_state,uint8_t nas_state,uint8_t mea_state,float pressure_ada,float pressure_digi,float pressure_static,float pressure_dpl,float airspeed_pitot,float altitude_agl,float ada_vert_speed,float mea_mass,float acc_x,float acc_y,float acc_z,float gyro_x,float gyro_y,float gyro_z,float mag_x,float mag_y,float mag_z,uint8_t gps_fix,float gps_lat,float gps_lon,float gps_alt,float abk_angle,float nas_n,float nas_e,float nas_d,float nas_vn,float nas_ve,float nas_vd,float nas_qx,float nas_qy,float nas_qz,float nas_qw,float nas_bias_x,float nas_bias_y,float nas_bias_z,float pin_quick_connector,uint8_t pin_launch,uint8_t pin_nosecone,uint8_t pin_expulsion,uint8_t cutter_presence,float battery_voltage,float cam_battery_voltage,float current_consumption,float temperature,int8_t logger_error)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char buf[MAVLINK_MSG_ID_ROCKET_FLIGHT_TM_LEN];
......@@ -429,48 +443,50 @@ static inline uint16_t mavlink_msg_rocket_flight_tm_pack_chan(uint8_t system_id,
_mav_put_float(buf, 24, airspeed_pitot);
_mav_put_float(buf, 28, altitude_agl);
_mav_put_float(buf, 32, ada_vert_speed);
_mav_put_float(buf, 36, acc_x);
_mav_put_float(buf, 40, acc_y);
_mav_put_float(buf, 44, acc_z);
_mav_put_float(buf, 48, gyro_x);
_mav_put_float(buf, 52, gyro_y);
_mav_put_float(buf, 56, gyro_z);
_mav_put_float(buf, 60, mag_x);
_mav_put_float(buf, 64, mag_y);
_mav_put_float(buf, 68, mag_z);
_mav_put_float(buf, 72, gps_lat);
_mav_put_float(buf, 76, gps_lon);
_mav_put_float(buf, 80, gps_alt);
_mav_put_float(buf, 84, abk_angle);
_mav_put_float(buf, 88, abk_estimated_cd);
_mav_put_float(buf, 92, parachute_load);
_mav_put_float(buf, 96, nas_n);
_mav_put_float(buf, 100, nas_e);
_mav_put_float(buf, 104, nas_d);
_mav_put_float(buf, 108, nas_vn);
_mav_put_float(buf, 112, nas_ve);
_mav_put_float(buf, 116, nas_vd);
_mav_put_float(buf, 120, nas_qx);
_mav_put_float(buf, 124, nas_qy);
_mav_put_float(buf, 128, nas_qz);
_mav_put_float(buf, 132, nas_qw);
_mav_put_float(buf, 136, nas_bias_x);
_mav_put_float(buf, 140, nas_bias_y);
_mav_put_float(buf, 144, nas_bias_z);
_mav_put_float(buf, 148, estimated_thrust);
_mav_put_float(buf, 152, vbat);
_mav_put_float(buf, 156, temperature);
_mav_put_uint8_t(buf, 160, ada_state);
_mav_put_uint8_t(buf, 161, fmm_state);
_mav_put_uint8_t(buf, 162, dpl_state);
_mav_put_uint8_t(buf, 163, abk_state);
_mav_put_uint8_t(buf, 164, nas_state);
_mav_put_uint8_t(buf, 165, gps_fix);
_mav_put_uint8_t(buf, 166, pin_launch);
_mav_put_uint8_t(buf, 167, pin_nosecone);
_mav_put_uint8_t(buf, 168, pin_expulsion);
_mav_put_uint8_t(buf, 169, cutter_presence);
_mav_put_int8_t(buf, 170, logger_error);
_mav_put_float(buf, 36, mea_mass);
_mav_put_float(buf, 40, acc_x);
_mav_put_float(buf, 44, acc_y);
_mav_put_float(buf, 48, acc_z);
_mav_put_float(buf, 52, gyro_x);
_mav_put_float(buf, 56, gyro_y);
_mav_put_float(buf, 60, gyro_z);
_mav_put_float(buf, 64, mag_x);
_mav_put_float(buf, 68, mag_y);
_mav_put_float(buf, 72, mag_z);
_mav_put_float(buf, 76, gps_lat);
_mav_put_float(buf, 80, gps_lon);
_mav_put_float(buf, 84, gps_alt);
_mav_put_float(buf, 88, abk_angle);
_mav_put_float(buf, 92, nas_n);
_mav_put_float(buf, 96, nas_e);
_mav_put_float(buf, 100, nas_d);
_mav_put_float(buf, 104, nas_vn);
_mav_put_float(buf, 108, nas_ve);
_mav_put_float(buf, 112, nas_vd);
_mav_put_float(buf, 116, nas_qx);
_mav_put_float(buf, 120, nas_qy);
_mav_put_float(buf, 124, nas_qz);
_mav_put_float(buf, 128, nas_qw);
_mav_put_float(buf, 132, nas_bias_x);
_mav_put_float(buf, 136, nas_bias_y);
_mav_put_float(buf, 140, nas_bias_z);
_mav_put_float(buf, 144, pin_quick_connector);
_mav_put_float(buf, 148, battery_voltage);
_mav_put_float(buf, 152, cam_battery_voltage);
_mav_put_float(buf, 156, current_consumption);
_mav_put_float(buf, 160, temperature);
_mav_put_uint8_t(buf, 164, ada_state);
_mav_put_uint8_t(buf, 165, fmm_state);
_mav_put_uint8_t(buf, 166, dpl_state);
_mav_put_uint8_t(buf, 167, abk_state);
_mav_put_uint8_t(buf, 168, nas_state);
_mav_put_uint8_t(buf, 169, mea_state);
_mav_put_uint8_t(buf, 170, gps_fix);
_mav_put_uint8_t(buf, 171, pin_launch);
_mav_put_uint8_t(buf, 172, pin_nosecone);
_mav_put_uint8_t(buf, 173, pin_expulsion);
_mav_put_uint8_t(buf, 174, cutter_presence);
_mav_put_int8_t(buf, 175, logger_error);
memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_ROCKET_FLIGHT_TM_LEN);
#else
......@@ -483,6 +499,7 @@ static inline uint16_t mavlink_msg_rocket_flight_tm_pack_chan(uint8_t system_id,
packet.airspeed_pitot = airspeed_pitot;
packet.altitude_agl = altitude_agl;
packet.ada_vert_speed = ada_vert_speed;
packet.mea_mass = mea_mass;
packet.acc_x = acc_x;
packet.acc_y = acc_y;
packet.acc_z = acc_z;
......@@ -496,8 +513,6 @@ static inline uint16_t mavlink_msg_rocket_flight_tm_pack_chan(uint8_t system_id,
packet.gps_lon = gps_lon;
packet.gps_alt = gps_alt;
packet.abk_angle = abk_angle;
packet.abk_estimated_cd = abk_estimated_cd;
packet.parachute_load = parachute_load;
packet.nas_n = nas_n;
packet.nas_e = nas_e;
packet.nas_d = nas_d;
......@@ -511,14 +526,17 @@ static inline uint16_t mavlink_msg_rocket_flight_tm_pack_chan(uint8_t system_id,
packet.nas_bias_x = nas_bias_x;
packet.nas_bias_y = nas_bias_y;
packet.nas_bias_z = nas_bias_z;
packet.estimated_thrust = estimated_thrust;
packet.vbat = vbat;
packet.pin_quick_connector = pin_quick_connector;
packet.battery_voltage = battery_voltage;
packet.cam_battery_voltage = cam_battery_voltage;
packet.current_consumption = current_consumption;
packet.temperature = temperature;
packet.ada_state = ada_state;
packet.fmm_state = fmm_state;
packet.dpl_state = dpl_state;
packet.abk_state = abk_state;
packet.nas_state = nas_state;
packet.mea_state = mea_state;
packet.gps_fix = gps_fix;
packet.pin_launch = pin_launch;
packet.pin_nosecone = pin_nosecone;
......@@ -543,7 +561,7 @@ static inline uint16_t mavlink_msg_rocket_flight_tm_pack_chan(uint8_t system_id,
*/
static inline uint16_t mavlink_msg_rocket_flight_tm_encode(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg, const mavlink_rocket_flight_tm_t* rocket_flight_tm)
{
return mavlink_msg_rocket_flight_tm_pack(system_id, component_id, msg, rocket_flight_tm->timestamp, rocket_flight_tm->ada_state, rocket_flight_tm->fmm_state, rocket_flight_tm->dpl_state, rocket_flight_tm->abk_state, rocket_flight_tm->nas_state, rocket_flight_tm->pressure_ada, rocket_flight_tm->pressure_digi, rocket_flight_tm->pressure_static, rocket_flight_tm->pressure_dpl, rocket_flight_tm->airspeed_pitot, rocket_flight_tm->altitude_agl, rocket_flight_tm->ada_vert_speed, rocket_flight_tm->acc_x, rocket_flight_tm->acc_y, rocket_flight_tm->acc_z, rocket_flight_tm->gyro_x, rocket_flight_tm->gyro_y, rocket_flight_tm->gyro_z, rocket_flight_tm->mag_x, rocket_flight_tm->mag_y, rocket_flight_tm->mag_z, rocket_flight_tm->gps_fix, rocket_flight_tm->gps_lat, rocket_flight_tm->gps_lon, rocket_flight_tm->gps_alt, rocket_flight_tm->abk_angle, rocket_flight_tm->abk_estimated_cd, rocket_flight_tm->parachute_load, rocket_flight_tm->nas_n, rocket_flight_tm->nas_e, rocket_flight_tm->nas_d, rocket_flight_tm->nas_vn, rocket_flight_tm->nas_ve, rocket_flight_tm->nas_vd, rocket_flight_tm->nas_qx, rocket_flight_tm->nas_qy, rocket_flight_tm->nas_qz, rocket_flight_tm->nas_qw, rocket_flight_tm->nas_bias_x, rocket_flight_tm->nas_bias_y, rocket_flight_tm->nas_bias_z, rocket_flight_tm->pin_launch, rocket_flight_tm->pin_nosecone, rocket_flight_tm->pin_expulsion, rocket_flight_tm->cutter_presence, rocket_flight_tm->estimated_thrust, rocket_flight_tm->vbat, rocket_flight_tm->temperature, rocket_flight_tm->logger_error);
return mavlink_msg_rocket_flight_tm_pack(system_id, component_id, msg, rocket_flight_tm->timestamp, rocket_flight_tm->ada_state, rocket_flight_tm->fmm_state, rocket_flight_tm->dpl_state, rocket_flight_tm->abk_state, rocket_flight_tm->nas_state, rocket_flight_tm->mea_state, rocket_flight_tm->pressure_ada, rocket_flight_tm->pressure_digi, rocket_flight_tm->pressure_static, rocket_flight_tm->pressure_dpl, rocket_flight_tm->airspeed_pitot, rocket_flight_tm->altitude_agl, rocket_flight_tm->ada_vert_speed, rocket_flight_tm->mea_mass, rocket_flight_tm->acc_x, rocket_flight_tm->acc_y, rocket_flight_tm->acc_z, rocket_flight_tm->gyro_x, rocket_flight_tm->gyro_y, rocket_flight_tm->gyro_z, rocket_flight_tm->mag_x, rocket_flight_tm->mag_y, rocket_flight_tm->mag_z, rocket_flight_tm->gps_fix, rocket_flight_tm->gps_lat, rocket_flight_tm->gps_lon, rocket_flight_tm->gps_alt, rocket_flight_tm->abk_angle, rocket_flight_tm->nas_n, rocket_flight_tm->nas_e, rocket_flight_tm->nas_d, rocket_flight_tm->nas_vn, rocket_flight_tm->nas_ve, rocket_flight_tm->nas_vd, rocket_flight_tm->nas_qx, rocket_flight_tm->nas_qy, rocket_flight_tm->nas_qz, rocket_flight_tm->nas_qw, rocket_flight_tm->nas_bias_x, rocket_flight_tm->nas_bias_y, rocket_flight_tm->nas_bias_z, rocket_flight_tm->pin_quick_connector, rocket_flight_tm->pin_launch, rocket_flight_tm->pin_nosecone, rocket_flight_tm->pin_expulsion, rocket_flight_tm->cutter_presence, rocket_flight_tm->battery_voltage, rocket_flight_tm->cam_battery_voltage, rocket_flight_tm->current_consumption, rocket_flight_tm->temperature, rocket_flight_tm->logger_error);
}
/**
......@@ -557,7 +575,7 @@ static inline uint16_t mavlink_msg_rocket_flight_tm_encode(uint8_t system_id, ui
*/
static inline uint16_t mavlink_msg_rocket_flight_tm_encode_chan(uint8_t system_id, uint8_t component_id, uint8_t chan, mavlink_message_t* msg, const mavlink_rocket_flight_tm_t* rocket_flight_tm)
{
return mavlink_msg_rocket_flight_tm_pack_chan(system_id, component_id, chan, msg, rocket_flight_tm->timestamp, rocket_flight_tm->ada_state, rocket_flight_tm->fmm_state, rocket_flight_tm->dpl_state, rocket_flight_tm->abk_state, rocket_flight_tm->nas_state, rocket_flight_tm->pressure_ada, rocket_flight_tm->pressure_digi, rocket_flight_tm->pressure_static, rocket_flight_tm->pressure_dpl, rocket_flight_tm->airspeed_pitot, rocket_flight_tm->altitude_agl, rocket_flight_tm->ada_vert_speed, rocket_flight_tm->acc_x, rocket_flight_tm->acc_y, rocket_flight_tm->acc_z, rocket_flight_tm->gyro_x, rocket_flight_tm->gyro_y, rocket_flight_tm->gyro_z, rocket_flight_tm->mag_x, rocket_flight_tm->mag_y, rocket_flight_tm->mag_z, rocket_flight_tm->gps_fix, rocket_flight_tm->gps_lat, rocket_flight_tm->gps_lon, rocket_flight_tm->gps_alt, rocket_flight_tm->abk_angle, rocket_flight_tm->abk_estimated_cd, rocket_flight_tm->parachute_load, rocket_flight_tm->nas_n, rocket_flight_tm->nas_e, rocket_flight_tm->nas_d, rocket_flight_tm->nas_vn, rocket_flight_tm->nas_ve, rocket_flight_tm->nas_vd, rocket_flight_tm->nas_qx, rocket_flight_tm->nas_qy, rocket_flight_tm->nas_qz, rocket_flight_tm->nas_qw, rocket_flight_tm->nas_bias_x, rocket_flight_tm->nas_bias_y, rocket_flight_tm->nas_bias_z, rocket_flight_tm->pin_launch, rocket_flight_tm->pin_nosecone, rocket_flight_tm->pin_expulsion, rocket_flight_tm->cutter_presence, rocket_flight_tm->estimated_thrust, rocket_flight_tm->vbat, rocket_flight_tm->temperature, rocket_flight_tm->logger_error);
return mavlink_msg_rocket_flight_tm_pack_chan(system_id, component_id, chan, msg, rocket_flight_tm->timestamp, rocket_flight_tm->ada_state, rocket_flight_tm->fmm_state, rocket_flight_tm->dpl_state, rocket_flight_tm->abk_state, rocket_flight_tm->nas_state, rocket_flight_tm->mea_state, rocket_flight_tm->pressure_ada, rocket_flight_tm->pressure_digi, rocket_flight_tm->pressure_static, rocket_flight_tm->pressure_dpl, rocket_flight_tm->airspeed_pitot, rocket_flight_tm->altitude_agl, rocket_flight_tm->ada_vert_speed, rocket_flight_tm->mea_mass, rocket_flight_tm->acc_x, rocket_flight_tm->acc_y, rocket_flight_tm->acc_z, rocket_flight_tm->gyro_x, rocket_flight_tm->gyro_y, rocket_flight_tm->gyro_z, rocket_flight_tm->mag_x, rocket_flight_tm->mag_y, rocket_flight_tm->mag_z, rocket_flight_tm->gps_fix, rocket_flight_tm->gps_lat, rocket_flight_tm->gps_lon, rocket_flight_tm->gps_alt, rocket_flight_tm->abk_angle, rocket_flight_tm->nas_n, rocket_flight_tm->nas_e, rocket_flight_tm->nas_d, rocket_flight_tm->nas_vn, rocket_flight_tm->nas_ve, rocket_flight_tm->nas_vd, rocket_flight_tm->nas_qx, rocket_flight_tm->nas_qy, rocket_flight_tm->nas_qz, rocket_flight_tm->nas_qw, rocket_flight_tm->nas_bias_x, rocket_flight_tm->nas_bias_y, rocket_flight_tm->nas_bias_z, rocket_flight_tm->pin_quick_connector, rocket_flight_tm->pin_launch, rocket_flight_tm->pin_nosecone, rocket_flight_tm->pin_expulsion, rocket_flight_tm->cutter_presence, rocket_flight_tm->battery_voltage, rocket_flight_tm->cam_battery_voltage, rocket_flight_tm->current_consumption, rocket_flight_tm->temperature, rocket_flight_tm->logger_error);
}
/**
......@@ -570,6 +588,7 @@ static inline uint16_t mavlink_msg_rocket_flight_tm_encode_chan(uint8_t system_i
* @param dpl_state Deployment Controller State
* @param abk_state Airbrake FSM state
* @param nas_state Navigation System FSM State
* @param mea_state MEA Controller State
* @param pressure_ada [Pa] Atmospheric pressure estimated by ADA
* @param pressure_digi [Pa] Pressure from digital sensor
* @param pressure_static [Pa] Pressure from static port
......@@ -577,6 +596,7 @@ static inline uint16_t mavlink_msg_rocket_flight_tm_encode_chan(uint8_t system_i
* @param airspeed_pitot [m/s] Pitot airspeed
* @param altitude_agl [m] Altitude above ground level
* @param ada_vert_speed [m/s] Vertical speed estimated by ADA
* @param mea_mass [kg] Mass estimated by MEA
* @param acc_x [m/s^2] Acceleration on X axis (body)
* @param acc_y [m/s^2] Acceleration on Y axis (body)
* @param acc_z [m/s^2] Acceleration on Z axis (body)
......@@ -591,8 +611,6 @@ static inline uint16_t mavlink_msg_rocket_flight_tm_encode_chan(uint8_t system_i
* @param gps_lon [deg] Longitude
* @param gps_alt [m] GPS Altitude
* @param abk_angle [deg] Air Brakes angle
* @param abk_estimated_cd Estimated drag coefficient
* @param parachute_load Parachute load cell value
* @param nas_n [deg] Navigation system estimated noth position
* @param nas_e [deg] Navigation system estimated east position
* @param nas_d [m] Navigation system estimated down position
......@@ -606,18 +624,20 @@ static inline uint16_t mavlink_msg_rocket_flight_tm_encode_chan(uint8_t system_i
* @param nas_bias_x Navigation system gyroscope bias on x axis
* @param nas_bias_y Navigation system gyroscope bias on y axis
* @param nas_bias_z Navigation system gyroscope bias on z axis
* @param pin_quick_connector Quick connector detach pin
* @param pin_launch Launch pin status (1 = connected, 0 = disconnected)
* @param pin_nosecone Nosecone pin status (1 = connected, 0 = disconnected)
* @param pin_expulsion Servo sensor status (1 = actuated, 0 = idle)
* @param cutter_presence Cutter presence status (1 = present, 0 = missing)
* @param estimated_thrust Estimated thrust from automatic shutdown algorithm
* @param vbat [V] Battery voltage
* @param battery_voltage [V] Battery voltage
* @param cam_battery_voltage [V] Camera battery voltage
* @param current_consumption [A] Battery current
* @param temperature [degC] Temperature
* @param logger_error Logger error (0 = no error, -1 otherwise)
*/
#ifdef MAVLINK_USE_CONVENIENCE_FUNCTIONS
static inline void mavlink_msg_rocket_flight_tm_send(mavlink_channel_t chan, uint64_t timestamp, uint8_t ada_state, uint8_t fmm_state, uint8_t dpl_state, uint8_t abk_state, uint8_t nas_state, float pressure_ada, float pressure_digi, float pressure_static, float pressure_dpl, float airspeed_pitot, float altitude_agl, float ada_vert_speed, float acc_x, float acc_y, float acc_z, float gyro_x, float gyro_y, float gyro_z, float mag_x, float mag_y, float mag_z, uint8_t gps_fix, float gps_lat, float gps_lon, float gps_alt, float abk_angle, float abk_estimated_cd, float parachute_load, float nas_n, float nas_e, float nas_d, float nas_vn, float nas_ve, float nas_vd, float nas_qx, float nas_qy, float nas_qz, float nas_qw, float nas_bias_x, float nas_bias_y, float nas_bias_z, uint8_t pin_launch, uint8_t pin_nosecone, uint8_t pin_expulsion, uint8_t cutter_presence, float estimated_thrust, float vbat, float temperature, int8_t logger_error)
static inline void mavlink_msg_rocket_flight_tm_send(mavlink_channel_t chan, uint64_t timestamp, uint8_t ada_state, uint8_t fmm_state, uint8_t dpl_state, uint8_t abk_state, uint8_t nas_state, uint8_t mea_state, float pressure_ada, float pressure_digi, float pressure_static, float pressure_dpl, float airspeed_pitot, float altitude_agl, float ada_vert_speed, float mea_mass, float acc_x, float acc_y, float acc_z, float gyro_x, float gyro_y, float gyro_z, float mag_x, float mag_y, float mag_z, uint8_t gps_fix, float gps_lat, float gps_lon, float gps_alt, float abk_angle, float nas_n, float nas_e, float nas_d, float nas_vn, float nas_ve, float nas_vd, float nas_qx, float nas_qy, float nas_qz, float nas_qw, float nas_bias_x, float nas_bias_y, float nas_bias_z, float pin_quick_connector, uint8_t pin_launch, uint8_t pin_nosecone, uint8_t pin_expulsion, uint8_t cutter_presence, float battery_voltage, float cam_battery_voltage, float current_consumption, float temperature, int8_t logger_error)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char buf[MAVLINK_MSG_ID_ROCKET_FLIGHT_TM_LEN];
......@@ -629,48 +649,50 @@ static inline void mavlink_msg_rocket_flight_tm_send(mavlink_channel_t chan, uin
_mav_put_float(buf, 24, airspeed_pitot);
_mav_put_float(buf, 28, altitude_agl);
_mav_put_float(buf, 32, ada_vert_speed);
_mav_put_float(buf, 36, acc_x);
_mav_put_float(buf, 40, acc_y);
_mav_put_float(buf, 44, acc_z);
_mav_put_float(buf, 48, gyro_x);
_mav_put_float(buf, 52, gyro_y);
_mav_put_float(buf, 56, gyro_z);
_mav_put_float(buf, 60, mag_x);
_mav_put_float(buf, 64, mag_y);
_mav_put_float(buf, 68, mag_z);
_mav_put_float(buf, 72, gps_lat);
_mav_put_float(buf, 76, gps_lon);
_mav_put_float(buf, 80, gps_alt);
_mav_put_float(buf, 84, abk_angle);
_mav_put_float(buf, 88, abk_estimated_cd);
_mav_put_float(buf, 92, parachute_load);
_mav_put_float(buf, 96, nas_n);
_mav_put_float(buf, 100, nas_e);
_mav_put_float(buf, 104, nas_d);
_mav_put_float(buf, 108, nas_vn);
_mav_put_float(buf, 112, nas_ve);
_mav_put_float(buf, 116, nas_vd);
_mav_put_float(buf, 120, nas_qx);
_mav_put_float(buf, 124, nas_qy);
_mav_put_float(buf, 128, nas_qz);
_mav_put_float(buf, 132, nas_qw);
_mav_put_float(buf, 136, nas_bias_x);
_mav_put_float(buf, 140, nas_bias_y);
_mav_put_float(buf, 144, nas_bias_z);
_mav_put_float(buf, 148, estimated_thrust);
_mav_put_float(buf, 152, vbat);
_mav_put_float(buf, 156, temperature);
_mav_put_uint8_t(buf, 160, ada_state);
_mav_put_uint8_t(buf, 161, fmm_state);
_mav_put_uint8_t(buf, 162, dpl_state);
_mav_put_uint8_t(buf, 163, abk_state);
_mav_put_uint8_t(buf, 164, nas_state);
_mav_put_uint8_t(buf, 165, gps_fix);
_mav_put_uint8_t(buf, 166, pin_launch);
_mav_put_uint8_t(buf, 167, pin_nosecone);
_mav_put_uint8_t(buf, 168, pin_expulsion);
_mav_put_uint8_t(buf, 169, cutter_presence);
_mav_put_int8_t(buf, 170, logger_error);
_mav_put_float(buf, 36, mea_mass);
_mav_put_float(buf, 40, acc_x);
_mav_put_float(buf, 44, acc_y);
_mav_put_float(buf, 48, acc_z);
_mav_put_float(buf, 52, gyro_x);
_mav_put_float(buf, 56, gyro_y);
_mav_put_float(buf, 60, gyro_z);
_mav_put_float(buf, 64, mag_x);
_mav_put_float(buf, 68, mag_y);
_mav_put_float(buf, 72, mag_z);
_mav_put_float(buf, 76, gps_lat);
_mav_put_float(buf, 80, gps_lon);
_mav_put_float(buf, 84, gps_alt);
_mav_put_float(buf, 88, abk_angle);
_mav_put_float(buf, 92, nas_n);
_mav_put_float(buf, 96, nas_e);
_mav_put_float(buf, 100, nas_d);
_mav_put_float(buf, 104, nas_vn);
_mav_put_float(buf, 108, nas_ve);
_mav_put_float(buf, 112, nas_vd);
_mav_put_float(buf, 116, nas_qx);
_mav_put_float(buf, 120, nas_qy);
_mav_put_float(buf, 124, nas_qz);
_mav_put_float(buf, 128, nas_qw);
_mav_put_float(buf, 132, nas_bias_x);
_mav_put_float(buf, 136, nas_bias_y);
_mav_put_float(buf, 140, nas_bias_z);
_mav_put_float(buf, 144, pin_quick_connector);
_mav_put_float(buf, 148, battery_voltage);
_mav_put_float(buf, 152, cam_battery_voltage);
_mav_put_float(buf, 156, current_consumption);
_mav_put_float(buf, 160, temperature);
_mav_put_uint8_t(buf, 164, ada_state);
_mav_put_uint8_t(buf, 165, fmm_state);
_mav_put_uint8_t(buf, 166, dpl_state);
_mav_put_uint8_t(buf, 167, abk_state);
_mav_put_uint8_t(buf, 168, nas_state);
_mav_put_uint8_t(buf, 169, mea_state);
_mav_put_uint8_t(buf, 170, gps_fix);
_mav_put_uint8_t(buf, 171, pin_launch);
_mav_put_uint8_t(buf, 172, pin_nosecone);
_mav_put_uint8_t(buf, 173, pin_expulsion);
_mav_put_uint8_t(buf, 174, cutter_presence);
_mav_put_int8_t(buf, 175, logger_error);
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_ROCKET_FLIGHT_TM, buf, MAVLINK_MSG_ID_ROCKET_FLIGHT_TM_MIN_LEN, MAVLINK_MSG_ID_ROCKET_FLIGHT_TM_LEN, MAVLINK_MSG_ID_ROCKET_FLIGHT_TM_CRC);
#else
......@@ -683,6 +705,7 @@ static inline void mavlink_msg_rocket_flight_tm_send(mavlink_channel_t chan, uin
packet.airspeed_pitot = airspeed_pitot;
packet.altitude_agl = altitude_agl;
packet.ada_vert_speed = ada_vert_speed;
packet.mea_mass = mea_mass;
packet.acc_x = acc_x;
packet.acc_y = acc_y;
packet.acc_z = acc_z;
......@@ -696,8 +719,6 @@ static inline void mavlink_msg_rocket_flight_tm_send(mavlink_channel_t chan, uin
packet.gps_lon = gps_lon;
packet.gps_alt = gps_alt;
packet.abk_angle = abk_angle;
packet.abk_estimated_cd = abk_estimated_cd;
packet.parachute_load = parachute_load;
packet.nas_n = nas_n;
packet.nas_e = nas_e;
packet.nas_d = nas_d;
......@@ -711,14 +732,17 @@ static inline void mavlink_msg_rocket_flight_tm_send(mavlink_channel_t chan, uin
packet.nas_bias_x = nas_bias_x;
packet.nas_bias_y = nas_bias_y;
packet.nas_bias_z = nas_bias_z;
packet.estimated_thrust = estimated_thrust;
packet.vbat = vbat;
packet.pin_quick_connector = pin_quick_connector;
packet.battery_voltage = battery_voltage;
packet.cam_battery_voltage = cam_battery_voltage;
packet.current_consumption = current_consumption;
packet.temperature = temperature;
packet.ada_state = ada_state;
packet.fmm_state = fmm_state;
packet.dpl_state = dpl_state;
packet.abk_state = abk_state;
packet.nas_state = nas_state;
packet.mea_state = mea_state;
packet.gps_fix = gps_fix;
packet.pin_launch = pin_launch;
packet.pin_nosecone = pin_nosecone;
......@@ -738,7 +762,7 @@ static inline void mavlink_msg_rocket_flight_tm_send(mavlink_channel_t chan, uin
static inline void mavlink_msg_rocket_flight_tm_send_struct(mavlink_channel_t chan, const mavlink_rocket_flight_tm_t* rocket_flight_tm)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
mavlink_msg_rocket_flight_tm_send(chan, rocket_flight_tm->timestamp, rocket_flight_tm->ada_state, rocket_flight_tm->fmm_state, rocket_flight_tm->dpl_state, rocket_flight_tm->abk_state, rocket_flight_tm->nas_state, rocket_flight_tm->pressure_ada, rocket_flight_tm->pressure_digi, rocket_flight_tm->pressure_static, rocket_flight_tm->pressure_dpl, rocket_flight_tm->airspeed_pitot, rocket_flight_tm->altitude_agl, rocket_flight_tm->ada_vert_speed, rocket_flight_tm->acc_x, rocket_flight_tm->acc_y, rocket_flight_tm->acc_z, rocket_flight_tm->gyro_x, rocket_flight_tm->gyro_y, rocket_flight_tm->gyro_z, rocket_flight_tm->mag_x, rocket_flight_tm->mag_y, rocket_flight_tm->mag_z, rocket_flight_tm->gps_fix, rocket_flight_tm->gps_lat, rocket_flight_tm->gps_lon, rocket_flight_tm->gps_alt, rocket_flight_tm->abk_angle, rocket_flight_tm->abk_estimated_cd, rocket_flight_tm->parachute_load, rocket_flight_tm->nas_n, rocket_flight_tm->nas_e, rocket_flight_tm->nas_d, rocket_flight_tm->nas_vn, rocket_flight_tm->nas_ve, rocket_flight_tm->nas_vd, rocket_flight_tm->nas_qx, rocket_flight_tm->nas_qy, rocket_flight_tm->nas_qz, rocket_flight_tm->nas_qw, rocket_flight_tm->nas_bias_x, rocket_flight_tm->nas_bias_y, rocket_flight_tm->nas_bias_z, rocket_flight_tm->pin_launch, rocket_flight_tm->pin_nosecone, rocket_flight_tm->pin_expulsion, rocket_flight_tm->cutter_presence, rocket_flight_tm->estimated_thrust, rocket_flight_tm->vbat, rocket_flight_tm->temperature, rocket_flight_tm->logger_error);
mavlink_msg_rocket_flight_tm_send(chan, rocket_flight_tm->timestamp, rocket_flight_tm->ada_state, rocket_flight_tm->fmm_state, rocket_flight_tm->dpl_state, rocket_flight_tm->abk_state, rocket_flight_tm->nas_state, rocket_flight_tm->mea_state, rocket_flight_tm->pressure_ada, rocket_flight_tm->pressure_digi, rocket_flight_tm->pressure_static, rocket_flight_tm->pressure_dpl, rocket_flight_tm->airspeed_pitot, rocket_flight_tm->altitude_agl, rocket_flight_tm->ada_vert_speed, rocket_flight_tm->mea_mass, rocket_flight_tm->acc_x, rocket_flight_tm->acc_y, rocket_flight_tm->acc_z, rocket_flight_tm->gyro_x, rocket_flight_tm->gyro_y, rocket_flight_tm->gyro_z, rocket_flight_tm->mag_x, rocket_flight_tm->mag_y, rocket_flight_tm->mag_z, rocket_flight_tm->gps_fix, rocket_flight_tm->gps_lat, rocket_flight_tm->gps_lon, rocket_flight_tm->gps_alt, rocket_flight_tm->abk_angle, rocket_flight_tm->nas_n, rocket_flight_tm->nas_e, rocket_flight_tm->nas_d, rocket_flight_tm->nas_vn, rocket_flight_tm->nas_ve, rocket_flight_tm->nas_vd, rocket_flight_tm->nas_qx, rocket_flight_tm->nas_qy, rocket_flight_tm->nas_qz, rocket_flight_tm->nas_qw, rocket_flight_tm->nas_bias_x, rocket_flight_tm->nas_bias_y, rocket_flight_tm->nas_bias_z, rocket_flight_tm->pin_quick_connector, rocket_flight_tm->pin_launch, rocket_flight_tm->pin_nosecone, rocket_flight_tm->pin_expulsion, rocket_flight_tm->cutter_presence, rocket_flight_tm->battery_voltage, rocket_flight_tm->cam_battery_voltage, rocket_flight_tm->current_consumption, rocket_flight_tm->temperature, rocket_flight_tm->logger_error);
#else
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_ROCKET_FLIGHT_TM, (const char *)rocket_flight_tm, MAVLINK_MSG_ID_ROCKET_FLIGHT_TM_MIN_LEN, MAVLINK_MSG_ID_ROCKET_FLIGHT_TM_LEN, MAVLINK_MSG_ID_ROCKET_FLIGHT_TM_CRC);
#endif
......@@ -752,7 +776,7 @@ static inline void mavlink_msg_rocket_flight_tm_send_struct(mavlink_channel_t ch
is usually the receive buffer for the channel, and allows a reply to an
incoming message with minimum stack space usage.
*/
static inline void mavlink_msg_rocket_flight_tm_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint64_t timestamp, uint8_t ada_state, uint8_t fmm_state, uint8_t dpl_state, uint8_t abk_state, uint8_t nas_state, float pressure_ada, float pressure_digi, float pressure_static, float pressure_dpl, float airspeed_pitot, float altitude_agl, float ada_vert_speed, float acc_x, float acc_y, float acc_z, float gyro_x, float gyro_y, float gyro_z, float mag_x, float mag_y, float mag_z, uint8_t gps_fix, float gps_lat, float gps_lon, float gps_alt, float abk_angle, float abk_estimated_cd, float parachute_load, float nas_n, float nas_e, float nas_d, float nas_vn, float nas_ve, float nas_vd, float nas_qx, float nas_qy, float nas_qz, float nas_qw, float nas_bias_x, float nas_bias_y, float nas_bias_z, uint8_t pin_launch, uint8_t pin_nosecone, uint8_t pin_expulsion, uint8_t cutter_presence, float estimated_thrust, float vbat, float temperature, int8_t logger_error)
static inline void mavlink_msg_rocket_flight_tm_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint64_t timestamp, uint8_t ada_state, uint8_t fmm_state, uint8_t dpl_state, uint8_t abk_state, uint8_t nas_state, uint8_t mea_state, float pressure_ada, float pressure_digi, float pressure_static, float pressure_dpl, float airspeed_pitot, float altitude_agl, float ada_vert_speed, float mea_mass, float acc_x, float acc_y, float acc_z, float gyro_x, float gyro_y, float gyro_z, float mag_x, float mag_y, float mag_z, uint8_t gps_fix, float gps_lat, float gps_lon, float gps_alt, float abk_angle, float nas_n, float nas_e, float nas_d, float nas_vn, float nas_ve, float nas_vd, float nas_qx, float nas_qy, float nas_qz, float nas_qw, float nas_bias_x, float nas_bias_y, float nas_bias_z, float pin_quick_connector, uint8_t pin_launch, uint8_t pin_nosecone, uint8_t pin_expulsion, uint8_t cutter_presence, float battery_voltage, float cam_battery_voltage, float current_consumption, float temperature, int8_t logger_error)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char *buf = (char *)msgbuf;
......@@ -764,48 +788,50 @@ static inline void mavlink_msg_rocket_flight_tm_send_buf(mavlink_message_t *msgb
_mav_put_float(buf, 24, airspeed_pitot);
_mav_put_float(buf, 28, altitude_agl);
_mav_put_float(buf, 32, ada_vert_speed);
_mav_put_float(buf, 36, acc_x);
_mav_put_float(buf, 40, acc_y);
_mav_put_float(buf, 44, acc_z);
_mav_put_float(buf, 48, gyro_x);
_mav_put_float(buf, 52, gyro_y);
_mav_put_float(buf, 56, gyro_z);
_mav_put_float(buf, 60, mag_x);
_mav_put_float(buf, 64, mag_y);
_mav_put_float(buf, 68, mag_z);
_mav_put_float(buf, 72, gps_lat);
_mav_put_float(buf, 76, gps_lon);
_mav_put_float(buf, 80, gps_alt);
_mav_put_float(buf, 84, abk_angle);
_mav_put_float(buf, 88, abk_estimated_cd);
_mav_put_float(buf, 92, parachute_load);
_mav_put_float(buf, 96, nas_n);
_mav_put_float(buf, 100, nas_e);
_mav_put_float(buf, 104, nas_d);
_mav_put_float(buf, 108, nas_vn);
_mav_put_float(buf, 112, nas_ve);
_mav_put_float(buf, 116, nas_vd);
_mav_put_float(buf, 120, nas_qx);
_mav_put_float(buf, 124, nas_qy);
_mav_put_float(buf, 128, nas_qz);
_mav_put_float(buf, 132, nas_qw);
_mav_put_float(buf, 136, nas_bias_x);
_mav_put_float(buf, 140, nas_bias_y);
_mav_put_float(buf, 144, nas_bias_z);
_mav_put_float(buf, 148, estimated_thrust);
_mav_put_float(buf, 152, vbat);
_mav_put_float(buf, 156, temperature);
_mav_put_uint8_t(buf, 160, ada_state);
_mav_put_uint8_t(buf, 161, fmm_state);
_mav_put_uint8_t(buf, 162, dpl_state);
_mav_put_uint8_t(buf, 163, abk_state);
_mav_put_uint8_t(buf, 164, nas_state);
_mav_put_uint8_t(buf, 165, gps_fix);
_mav_put_uint8_t(buf, 166, pin_launch);
_mav_put_uint8_t(buf, 167, pin_nosecone);
_mav_put_uint8_t(buf, 168, pin_expulsion);
_mav_put_uint8_t(buf, 169, cutter_presence);
_mav_put_int8_t(buf, 170, logger_error);
_mav_put_float(buf, 36, mea_mass);
_mav_put_float(buf, 40, acc_x);
_mav_put_float(buf, 44, acc_y);
_mav_put_float(buf, 48, acc_z);
_mav_put_float(buf, 52, gyro_x);
_mav_put_float(buf, 56, gyro_y);
_mav_put_float(buf, 60, gyro_z);
_mav_put_float(buf, 64, mag_x);
_mav_put_float(buf, 68, mag_y);
_mav_put_float(buf, 72, mag_z);
_mav_put_float(buf, 76, gps_lat);
_mav_put_float(buf, 80, gps_lon);
_mav_put_float(buf, 84, gps_alt);
_mav_put_float(buf, 88, abk_angle);
_mav_put_float(buf, 92, nas_n);
_mav_put_float(buf, 96, nas_e);
_mav_put_float(buf, 100, nas_d);
_mav_put_float(buf, 104, nas_vn);
_mav_put_float(buf, 108, nas_ve);
_mav_put_float(buf, 112, nas_vd);
_mav_put_float(buf, 116, nas_qx);
_mav_put_float(buf, 120, nas_qy);
_mav_put_float(buf, 124, nas_qz);
_mav_put_float(buf, 128, nas_qw);
_mav_put_float(buf, 132, nas_bias_x);
_mav_put_float(buf, 136, nas_bias_y);
_mav_put_float(buf, 140, nas_bias_z);
_mav_put_float(buf, 144, pin_quick_connector);
_mav_put_float(buf, 148, battery_voltage);
_mav_put_float(buf, 152, cam_battery_voltage);
_mav_put_float(buf, 156, current_consumption);
_mav_put_float(buf, 160, temperature);
_mav_put_uint8_t(buf, 164, ada_state);
_mav_put_uint8_t(buf, 165, fmm_state);
_mav_put_uint8_t(buf, 166, dpl_state);
_mav_put_uint8_t(buf, 167, abk_state);
_mav_put_uint8_t(buf, 168, nas_state);
_mav_put_uint8_t(buf, 169, mea_state);
_mav_put_uint8_t(buf, 170, gps_fix);
_mav_put_uint8_t(buf, 171, pin_launch);
_mav_put_uint8_t(buf, 172, pin_nosecone);
_mav_put_uint8_t(buf, 173, pin_expulsion);
_mav_put_uint8_t(buf, 174, cutter_presence);
_mav_put_int8_t(buf, 175, logger_error);
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_ROCKET_FLIGHT_TM, buf, MAVLINK_MSG_ID_ROCKET_FLIGHT_TM_MIN_LEN, MAVLINK_MSG_ID_ROCKET_FLIGHT_TM_LEN, MAVLINK_MSG_ID_ROCKET_FLIGHT_TM_CRC);
#else
......@@ -818,6 +844,7 @@ static inline void mavlink_msg_rocket_flight_tm_send_buf(mavlink_message_t *msgb
packet->airspeed_pitot = airspeed_pitot;
packet->altitude_agl = altitude_agl;
packet->ada_vert_speed = ada_vert_speed;
packet->mea_mass = mea_mass;
packet->acc_x = acc_x;
packet->acc_y = acc_y;
packet->acc_z = acc_z;
......@@ -831,8 +858,6 @@ static inline void mavlink_msg_rocket_flight_tm_send_buf(mavlink_message_t *msgb
packet->gps_lon = gps_lon;
packet->gps_alt = gps_alt;
packet->abk_angle = abk_angle;
packet->abk_estimated_cd = abk_estimated_cd;
packet->parachute_load = parachute_load;
packet->nas_n = nas_n;
packet->nas_e = nas_e;
packet->nas_d = nas_d;
......@@ -846,14 +871,17 @@ static inline void mavlink_msg_rocket_flight_tm_send_buf(mavlink_message_t *msgb
packet->nas_bias_x = nas_bias_x;
packet->nas_bias_y = nas_bias_y;
packet->nas_bias_z = nas_bias_z;
packet->estimated_thrust = estimated_thrust;
packet->vbat = vbat;
packet->pin_quick_connector = pin_quick_connector;
packet->battery_voltage = battery_voltage;
packet->cam_battery_voltage = cam_battery_voltage;
packet->current_consumption = current_consumption;
packet->temperature = temperature;
packet->ada_state = ada_state;
packet->fmm_state = fmm_state;
packet->dpl_state = dpl_state;
packet->abk_state = abk_state;
packet->nas_state = nas_state;
packet->mea_state = mea_state;
packet->gps_fix = gps_fix;
packet->pin_launch = pin_launch;
packet->pin_nosecone = pin_nosecone;
......@@ -888,7 +916,7 @@ static inline uint64_t mavlink_msg_rocket_flight_tm_get_timestamp(const mavlink_
*/
static inline uint8_t mavlink_msg_rocket_flight_tm_get_ada_state(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint8_t(msg, 160);
return _MAV_RETURN_uint8_t(msg, 164);
}
/**
......@@ -898,7 +926,7 @@ static inline uint8_t mavlink_msg_rocket_flight_tm_get_ada_state(const mavlink_m
*/
static inline uint8_t mavlink_msg_rocket_flight_tm_get_fmm_state(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint8_t(msg, 161);
return _MAV_RETURN_uint8_t(msg, 165);
}
/**
......@@ -908,7 +936,7 @@ static inline uint8_t mavlink_msg_rocket_flight_tm_get_fmm_state(const mavlink_m
*/
static inline uint8_t mavlink_msg_rocket_flight_tm_get_dpl_state(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint8_t(msg, 162);
return _MAV_RETURN_uint8_t(msg, 166);
}
/**
......@@ -918,7 +946,7 @@ static inline uint8_t mavlink_msg_rocket_flight_tm_get_dpl_state(const mavlink_m
*/
static inline uint8_t mavlink_msg_rocket_flight_tm_get_abk_state(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint8_t(msg, 163);
return _MAV_RETURN_uint8_t(msg, 167);
}
/**
......@@ -928,7 +956,17 @@ static inline uint8_t mavlink_msg_rocket_flight_tm_get_abk_state(const mavlink_m
*/
static inline uint8_t mavlink_msg_rocket_flight_tm_get_nas_state(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint8_t(msg, 164);
return _MAV_RETURN_uint8_t(msg, 168);
}
/**
* @brief Get field mea_state from rocket_flight_tm message
*
* @return MEA Controller State
*/
static inline uint8_t mavlink_msg_rocket_flight_tm_get_mea_state(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint8_t(msg, 169);
}
/**
......@@ -1001,6 +1039,16 @@ static inline float mavlink_msg_rocket_flight_tm_get_ada_vert_speed(const mavlin
return _MAV_RETURN_float(msg, 32);
}
/**
* @brief Get field mea_mass from rocket_flight_tm message
*
* @return [kg] Mass estimated by MEA
*/
static inline float mavlink_msg_rocket_flight_tm_get_mea_mass(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 36);
}
/**
* @brief Get field acc_x from rocket_flight_tm message
*
......@@ -1008,7 +1056,7 @@ static inline float mavlink_msg_rocket_flight_tm_get_ada_vert_speed(const mavlin
*/
static inline float mavlink_msg_rocket_flight_tm_get_acc_x(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 36);
return _MAV_RETURN_float(msg, 40);
}
/**
......@@ -1018,7 +1066,7 @@ static inline float mavlink_msg_rocket_flight_tm_get_acc_x(const mavlink_message
*/
static inline float mavlink_msg_rocket_flight_tm_get_acc_y(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 40);
return _MAV_RETURN_float(msg, 44);
}
/**
......@@ -1028,7 +1076,7 @@ static inline float mavlink_msg_rocket_flight_tm_get_acc_y(const mavlink_message
*/
static inline float mavlink_msg_rocket_flight_tm_get_acc_z(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 44);
return _MAV_RETURN_float(msg, 48);
}
/**
......@@ -1038,7 +1086,7 @@ static inline float mavlink_msg_rocket_flight_tm_get_acc_z(const mavlink_message
*/
static inline float mavlink_msg_rocket_flight_tm_get_gyro_x(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 48);
return _MAV_RETURN_float(msg, 52);
}
/**
......@@ -1048,7 +1096,7 @@ static inline float mavlink_msg_rocket_flight_tm_get_gyro_x(const mavlink_messag
*/
static inline float mavlink_msg_rocket_flight_tm_get_gyro_y(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 52);
return _MAV_RETURN_float(msg, 56);
}
/**
......@@ -1058,7 +1106,7 @@ static inline float mavlink_msg_rocket_flight_tm_get_gyro_y(const mavlink_messag
*/
static inline float mavlink_msg_rocket_flight_tm_get_gyro_z(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 56);
return _MAV_RETURN_float(msg, 60);
}
/**
......@@ -1068,7 +1116,7 @@ static inline float mavlink_msg_rocket_flight_tm_get_gyro_z(const mavlink_messag
*/
static inline float mavlink_msg_rocket_flight_tm_get_mag_x(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 60);
return _MAV_RETURN_float(msg, 64);
}
/**
......@@ -1078,7 +1126,7 @@ static inline float mavlink_msg_rocket_flight_tm_get_mag_x(const mavlink_message
*/
static inline float mavlink_msg_rocket_flight_tm_get_mag_y(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 64);
return _MAV_RETURN_float(msg, 68);
}
/**
......@@ -1088,7 +1136,7 @@ static inline float mavlink_msg_rocket_flight_tm_get_mag_y(const mavlink_message
*/
static inline float mavlink_msg_rocket_flight_tm_get_mag_z(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 68);
return _MAV_RETURN_float(msg, 72);
}
/**
......@@ -1098,7 +1146,7 @@ static inline float mavlink_msg_rocket_flight_tm_get_mag_z(const mavlink_message
*/
static inline uint8_t mavlink_msg_rocket_flight_tm_get_gps_fix(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint8_t(msg, 165);
return _MAV_RETURN_uint8_t(msg, 170);
}
/**
......@@ -1108,7 +1156,7 @@ static inline uint8_t mavlink_msg_rocket_flight_tm_get_gps_fix(const mavlink_mes
*/
static inline float mavlink_msg_rocket_flight_tm_get_gps_lat(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 72);
return _MAV_RETURN_float(msg, 76);
}
/**
......@@ -1118,7 +1166,7 @@ static inline float mavlink_msg_rocket_flight_tm_get_gps_lat(const mavlink_messa
*/
static inline float mavlink_msg_rocket_flight_tm_get_gps_lon(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 76);
return _MAV_RETURN_float(msg, 80);
}
/**
......@@ -1128,7 +1176,7 @@ static inline float mavlink_msg_rocket_flight_tm_get_gps_lon(const mavlink_messa
*/
static inline float mavlink_msg_rocket_flight_tm_get_gps_alt(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 80);
return _MAV_RETURN_float(msg, 84);
}
/**
......@@ -1137,30 +1185,10 @@ static inline float mavlink_msg_rocket_flight_tm_get_gps_alt(const mavlink_messa
* @return [deg] Air Brakes angle
*/
static inline float mavlink_msg_rocket_flight_tm_get_abk_angle(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 84);
}
/**
* @brief Get field abk_estimated_cd from rocket_flight_tm message
*
* @return Estimated drag coefficient
*/
static inline float mavlink_msg_rocket_flight_tm_get_abk_estimated_cd(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 88);
}
/**
* @brief Get field parachute_load from rocket_flight_tm message
*
* @return Parachute load cell value
*/
static inline float mavlink_msg_rocket_flight_tm_get_parachute_load(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 92);
}
/**
* @brief Get field nas_n from rocket_flight_tm message
*
......@@ -1168,7 +1196,7 @@ static inline float mavlink_msg_rocket_flight_tm_get_parachute_load(const mavlin
*/
static inline float mavlink_msg_rocket_flight_tm_get_nas_n(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 96);
return _MAV_RETURN_float(msg, 92);
}
/**
......@@ -1178,7 +1206,7 @@ static inline float mavlink_msg_rocket_flight_tm_get_nas_n(const mavlink_message
*/
static inline float mavlink_msg_rocket_flight_tm_get_nas_e(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 100);
return _MAV_RETURN_float(msg, 96);
}
/**
......@@ -1188,7 +1216,7 @@ static inline float mavlink_msg_rocket_flight_tm_get_nas_e(const mavlink_message
*/
static inline float mavlink_msg_rocket_flight_tm_get_nas_d(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 104);
return _MAV_RETURN_float(msg, 100);
}
/**
......@@ -1198,7 +1226,7 @@ static inline float mavlink_msg_rocket_flight_tm_get_nas_d(const mavlink_message
*/
static inline float mavlink_msg_rocket_flight_tm_get_nas_vn(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 108);
return _MAV_RETURN_float(msg, 104);
}
/**
......@@ -1208,7 +1236,7 @@ static inline float mavlink_msg_rocket_flight_tm_get_nas_vn(const mavlink_messag
*/
static inline float mavlink_msg_rocket_flight_tm_get_nas_ve(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 112);
return _MAV_RETURN_float(msg, 108);
}
/**
......@@ -1218,7 +1246,7 @@ static inline float mavlink_msg_rocket_flight_tm_get_nas_ve(const mavlink_messag
*/
static inline float mavlink_msg_rocket_flight_tm_get_nas_vd(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 116);
return _MAV_RETURN_float(msg, 112);
}
/**
......@@ -1228,7 +1256,7 @@ static inline float mavlink_msg_rocket_flight_tm_get_nas_vd(const mavlink_messag
*/
static inline float mavlink_msg_rocket_flight_tm_get_nas_qx(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 120);
return _MAV_RETURN_float(msg, 116);
}
/**
......@@ -1238,7 +1266,7 @@ static inline float mavlink_msg_rocket_flight_tm_get_nas_qx(const mavlink_messag
*/
static inline float mavlink_msg_rocket_flight_tm_get_nas_qy(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 124);
return _MAV_RETURN_float(msg, 120);
}
/**
......@@ -1248,7 +1276,7 @@ static inline float mavlink_msg_rocket_flight_tm_get_nas_qy(const mavlink_messag
*/
static inline float mavlink_msg_rocket_flight_tm_get_nas_qz(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 128);
return _MAV_RETURN_float(msg, 124);
}
/**
......@@ -1258,7 +1286,7 @@ static inline float mavlink_msg_rocket_flight_tm_get_nas_qz(const mavlink_messag
*/
static inline float mavlink_msg_rocket_flight_tm_get_nas_qw(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 132);
return _MAV_RETURN_float(msg, 128);
}
/**
......@@ -1268,7 +1296,7 @@ static inline float mavlink_msg_rocket_flight_tm_get_nas_qw(const mavlink_messag
*/
static inline float mavlink_msg_rocket_flight_tm_get_nas_bias_x(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 136);
return _MAV_RETURN_float(msg, 132);
}
/**
......@@ -1278,7 +1306,7 @@ static inline float mavlink_msg_rocket_flight_tm_get_nas_bias_x(const mavlink_me
*/
static inline float mavlink_msg_rocket_flight_tm_get_nas_bias_y(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 140);
return _MAV_RETURN_float(msg, 136);
}
/**
......@@ -1287,6 +1315,16 @@ static inline float mavlink_msg_rocket_flight_tm_get_nas_bias_y(const mavlink_me
* @return Navigation system gyroscope bias on z axis
*/
static inline float mavlink_msg_rocket_flight_tm_get_nas_bias_z(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 140);
}
/**
* @brief Get field pin_quick_connector from rocket_flight_tm message
*
* @return Quick connector detach pin
*/
static inline float mavlink_msg_rocket_flight_tm_get_pin_quick_connector(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 144);
}
......@@ -1298,7 +1336,7 @@ static inline float mavlink_msg_rocket_flight_tm_get_nas_bias_z(const mavlink_me
*/
static inline uint8_t mavlink_msg_rocket_flight_tm_get_pin_launch(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint8_t(msg, 166);
return _MAV_RETURN_uint8_t(msg, 171);
}
/**
......@@ -1308,7 +1346,7 @@ static inline uint8_t mavlink_msg_rocket_flight_tm_get_pin_launch(const mavlink_
*/
static inline uint8_t mavlink_msg_rocket_flight_tm_get_pin_nosecone(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint8_t(msg, 167);
return _MAV_RETURN_uint8_t(msg, 172);
}
/**
......@@ -1318,7 +1356,7 @@ static inline uint8_t mavlink_msg_rocket_flight_tm_get_pin_nosecone(const mavlin
*/
static inline uint8_t mavlink_msg_rocket_flight_tm_get_pin_expulsion(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint8_t(msg, 168);
return _MAV_RETURN_uint8_t(msg, 173);
}
/**
......@@ -1328,29 +1366,39 @@ static inline uint8_t mavlink_msg_rocket_flight_tm_get_pin_expulsion(const mavli
*/
static inline uint8_t mavlink_msg_rocket_flight_tm_get_cutter_presence(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint8_t(msg, 169);
return _MAV_RETURN_uint8_t(msg, 174);
}
/**
* @brief Get field estimated_thrust from rocket_flight_tm message
* @brief Get field battery_voltage from rocket_flight_tm message
*
* @return Estimated thrust from automatic shutdown algorithm
* @return [V] Battery voltage
*/
static inline float mavlink_msg_rocket_flight_tm_get_estimated_thrust(const mavlink_message_t* msg)
static inline float mavlink_msg_rocket_flight_tm_get_battery_voltage(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 148);
}
/**
* @brief Get field vbat from rocket_flight_tm message
* @brief Get field cam_battery_voltage from rocket_flight_tm message
*
* @return [V] Battery voltage
* @return [V] Camera battery voltage
*/
static inline float mavlink_msg_rocket_flight_tm_get_vbat(const mavlink_message_t* msg)
static inline float mavlink_msg_rocket_flight_tm_get_cam_battery_voltage(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 152);
}
/**
* @brief Get field current_consumption from rocket_flight_tm message
*
* @return [A] Battery current
*/
static inline float mavlink_msg_rocket_flight_tm_get_current_consumption(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 156);
}
/**
* @brief Get field temperature from rocket_flight_tm message
*
......@@ -1358,7 +1406,7 @@ static inline float mavlink_msg_rocket_flight_tm_get_vbat(const mavlink_message_
*/
static inline float mavlink_msg_rocket_flight_tm_get_temperature(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 156);
return _MAV_RETURN_float(msg, 160);
}
/**
......@@ -1368,7 +1416,7 @@ static inline float mavlink_msg_rocket_flight_tm_get_temperature(const mavlink_m
*/
static inline int8_t mavlink_msg_rocket_flight_tm_get_logger_error(const mavlink_message_t* msg)
{
return _MAV_RETURN_int8_t(msg, 170);
return _MAV_RETURN_int8_t(msg, 175);
}
/**
......@@ -1388,6 +1436,7 @@ static inline void mavlink_msg_rocket_flight_tm_decode(const mavlink_message_t*
rocket_flight_tm->airspeed_pitot = mavlink_msg_rocket_flight_tm_get_airspeed_pitot(msg);
rocket_flight_tm->altitude_agl = mavlink_msg_rocket_flight_tm_get_altitude_agl(msg);
rocket_flight_tm->ada_vert_speed = mavlink_msg_rocket_flight_tm_get_ada_vert_speed(msg);
rocket_flight_tm->mea_mass = mavlink_msg_rocket_flight_tm_get_mea_mass(msg);
rocket_flight_tm->acc_x = mavlink_msg_rocket_flight_tm_get_acc_x(msg);
rocket_flight_tm->acc_y = mavlink_msg_rocket_flight_tm_get_acc_y(msg);
rocket_flight_tm->acc_z = mavlink_msg_rocket_flight_tm_get_acc_z(msg);
......@@ -1401,8 +1450,6 @@ static inline void mavlink_msg_rocket_flight_tm_decode(const mavlink_message_t*
rocket_flight_tm->gps_lon = mavlink_msg_rocket_flight_tm_get_gps_lon(msg);
rocket_flight_tm->gps_alt = mavlink_msg_rocket_flight_tm_get_gps_alt(msg);
rocket_flight_tm->abk_angle = mavlink_msg_rocket_flight_tm_get_abk_angle(msg);
rocket_flight_tm->abk_estimated_cd = mavlink_msg_rocket_flight_tm_get_abk_estimated_cd(msg);
rocket_flight_tm->parachute_load = mavlink_msg_rocket_flight_tm_get_parachute_load(msg);
rocket_flight_tm->nas_n = mavlink_msg_rocket_flight_tm_get_nas_n(msg);
rocket_flight_tm->nas_e = mavlink_msg_rocket_flight_tm_get_nas_e(msg);
rocket_flight_tm->nas_d = mavlink_msg_rocket_flight_tm_get_nas_d(msg);
......@@ -1416,14 +1463,17 @@ static inline void mavlink_msg_rocket_flight_tm_decode(const mavlink_message_t*
rocket_flight_tm->nas_bias_x = mavlink_msg_rocket_flight_tm_get_nas_bias_x(msg);
rocket_flight_tm->nas_bias_y = mavlink_msg_rocket_flight_tm_get_nas_bias_y(msg);
rocket_flight_tm->nas_bias_z = mavlink_msg_rocket_flight_tm_get_nas_bias_z(msg);
rocket_flight_tm->estimated_thrust = mavlink_msg_rocket_flight_tm_get_estimated_thrust(msg);
rocket_flight_tm->vbat = mavlink_msg_rocket_flight_tm_get_vbat(msg);
rocket_flight_tm->pin_quick_connector = mavlink_msg_rocket_flight_tm_get_pin_quick_connector(msg);
rocket_flight_tm->battery_voltage = mavlink_msg_rocket_flight_tm_get_battery_voltage(msg);
rocket_flight_tm->cam_battery_voltage = mavlink_msg_rocket_flight_tm_get_cam_battery_voltage(msg);
rocket_flight_tm->current_consumption = mavlink_msg_rocket_flight_tm_get_current_consumption(msg);
rocket_flight_tm->temperature = mavlink_msg_rocket_flight_tm_get_temperature(msg);
rocket_flight_tm->ada_state = mavlink_msg_rocket_flight_tm_get_ada_state(msg);
rocket_flight_tm->fmm_state = mavlink_msg_rocket_flight_tm_get_fmm_state(msg);
rocket_flight_tm->dpl_state = mavlink_msg_rocket_flight_tm_get_dpl_state(msg);
rocket_flight_tm->abk_state = mavlink_msg_rocket_flight_tm_get_abk_state(msg);
rocket_flight_tm->nas_state = mavlink_msg_rocket_flight_tm_get_nas_state(msg);
rocket_flight_tm->mea_state = mavlink_msg_rocket_flight_tm_get_mea_state(msg);
rocket_flight_tm->gps_fix = mavlink_msg_rocket_flight_tm_get_gps_fix(msg);
rocket_flight_tm->pin_launch = mavlink_msg_rocket_flight_tm_get_pin_launch(msg);
rocket_flight_tm->pin_nosecone = mavlink_msg_rocket_flight_tm_get_pin_nosecone(msg);
......
mavlink_lib/gemini/mavlink_msg_set_servo_angle_tc.h
View file @ 7abedf97
......@@ -5,7 +5,7 @@
typedef struct __mavlink_set_servo_angle_tc_t {
float angle; /*< [deg] Servo angle*/
float angle; /*< Servo angle in normalized value [0-1]*/
uint8_t servo_id; /*< A member of the ServosList enum*/
} mavlink_set_servo_angle_tc_t;
......@@ -45,7 +45,7 @@ typedef struct __mavlink_set_servo_angle_tc_t {
* @param msg The MAVLink message to compress the data into
*
* @param servo_id A member of the ServosList enum
* @param angle [deg] Servo angle
* @param angle Servo angle in normalized value [0-1]
* @return length of the message in bytes (excluding serial stream start sign)
*/
static inline uint16_t mavlink_msg_set_servo_angle_tc_pack(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg,
......@@ -76,7 +76,7 @@ static inline uint16_t mavlink_msg_set_servo_angle_tc_pack(uint8_t system_id, ui
* @param chan The MAVLink channel this message will be sent over
* @param msg The MAVLink message to compress the data into
* @param servo_id A member of the ServosList enum
* @param angle [deg] Servo angle
* @param angle Servo angle in normalized value [0-1]
* @return length of the message in bytes (excluding serial stream start sign)
*/
static inline uint16_t mavlink_msg_set_servo_angle_tc_pack_chan(uint8_t system_id, uint8_t component_id, uint8_t chan,
......@@ -133,7 +133,7 @@ static inline uint16_t mavlink_msg_set_servo_angle_tc_encode_chan(uint8_t system
* @param chan MAVLink channel to send the message
*
* @param servo_id A member of the ServosList enum
* @param angle [deg] Servo angle
* @param angle Servo angle in normalized value [0-1]
*/
#ifdef MAVLINK_USE_CONVENIENCE_FUNCTIONS
......@@ -212,7 +212,7 @@ static inline uint8_t mavlink_msg_set_servo_angle_tc_get_servo_id(const mavlink_
/**
* @brief Get field angle from set_servo_angle_tc message
*
* @return [deg] Servo angle
* @return Servo angle in normalized value [0-1]
*/
static inline float mavlink_msg_set_servo_angle_tc_get_angle(const mavlink_message_t* msg)
{
......
mavlink_lib/gemini/testsuite.h
View file @ 7abedf97
......@@ -1551,7 +1551,7 @@ static void mavlink_test_adc_tm(uint8_t system_id, uint8_t component_id, mavlink
uint8_t buffer[MAVLINK_MAX_PACKET_LEN];
uint16_t i;
mavlink_adc_tm_t packet_in = {
93372036854775807ULL,73.0,101.0,129.0,157.0,"YZABCDEFGHIJKLMNOPQ"
93372036854775807ULL,73.0,101.0,129.0,157.0,185.0,213.0,241.0,269.0,"OPQRSTUVWXYZABCDEFG"
};
mavlink_adc_tm_t packet1, packet2;
memset(&packet1, 0, sizeof(packet1));
......@@ -1560,6 +1560,10 @@ static void mavlink_test_adc_tm(uint8_t system_id, uint8_t component_id, mavlink
packet1.channel_1 = packet_in.channel_1;
packet1.channel_2 = packet_in.channel_2;
packet1.channel_3 = packet_in.channel_3;
packet1.channel_4 = packet_in.channel_4;
packet1.channel_5 = packet_in.channel_5;
packet1.channel_6 = packet_in.channel_6;
packet1.channel_7 = packet_in.channel_7;
mav_array_memcpy(packet1.sensor_name, packet_in.sensor_name, sizeof(char)*20);
......@@ -1575,12 +1579,12 @@ static void mavlink_test_adc_tm(uint8_t system_id, uint8_t component_id, mavlink
MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0);
memset(&packet2, 0, sizeof(packet2));
mavlink_msg_adc_tm_pack(system_id, component_id, &msg , packet1.timestamp , packet1.sensor_name , packet1.channel_0 , packet1.channel_1 , packet1.channel_2 , packet1.channel_3 );
mavlink_msg_adc_tm_pack(system_id, component_id, &msg , packet1.timestamp , packet1.sensor_name , packet1.channel_0 , packet1.channel_1 , packet1.channel_2 , packet1.channel_3 , packet1.channel_4 , packet1.channel_5 , packet1.channel_6 , packet1.channel_7 );
mavlink_msg_adc_tm_decode(&msg, &packet2);
MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0);
memset(&packet2, 0, sizeof(packet2));
mavlink_msg_adc_tm_pack_chan(system_id, component_id, MAVLINK_COMM_0, &msg , packet1.timestamp , packet1.sensor_name , packet1.channel_0 , packet1.channel_1 , packet1.channel_2 , packet1.channel_3 );
mavlink_msg_adc_tm_pack_chan(system_id, component_id, MAVLINK_COMM_0, &msg , packet1.timestamp , packet1.sensor_name , packet1.channel_0 , packet1.channel_1 , packet1.channel_2 , packet1.channel_3 , packet1.channel_4 , packet1.channel_5 , packet1.channel_6 , packet1.channel_7 );
mavlink_msg_adc_tm_decode(&msg, &packet2);
MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0);
......@@ -1593,7 +1597,7 @@ static void mavlink_test_adc_tm(uint8_t system_id, uint8_t component_id, mavlink
MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0);
memset(&packet2, 0, sizeof(packet2));
mavlink_msg_adc_tm_send(MAVLINK_COMM_1 , packet1.timestamp , packet1.sensor_name , packet1.channel_0 , packet1.channel_1 , packet1.channel_2 , packet1.channel_3 );
mavlink_msg_adc_tm_send(MAVLINK_COMM_1 , packet1.timestamp , packet1.sensor_name , packet1.channel_0 , packet1.channel_1 , packet1.channel_2 , packet1.channel_3 , packet1.channel_4 , packet1.channel_5 , packet1.channel_6 , packet1.channel_7 );
mavlink_msg_adc_tm_decode(last_msg, &packet2);
MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0);
......@@ -2109,15 +2113,30 @@ static void mavlink_test_receiver_tm(uint8_t system_id, uint8_t component_id, ma
uint8_t buffer[MAVLINK_MAX_PACKET_LEN];
uint16_t i;
mavlink_receiver_tm_t packet_in = {
93372036854775807ULL,93372036854776311ULL,93372036854776815ULL,185.0,213.0
93372036854775807ULL,73.0,101.0,129.0,157.0,185.0,18691,18795,18899,19003,19107,19211,19315,19419,19523,19627,149,216,27,94
};
mavlink_receiver_tm_t packet1, packet2;
memset(&packet1, 0, sizeof(packet1));
packet1.timestamp = packet_in.timestamp;
packet1.rx_bitrate = packet_in.rx_bitrate;
packet1.tx_bitrate = packet_in.tx_bitrate;
packet1.rssi = packet_in.rssi;
packet1.fei = packet_in.fei;
packet1.main_rx_rssi = packet_in.main_rx_rssi;
packet1.main_rx_fei = packet_in.main_rx_fei;
packet1.payload_rx_rssi = packet_in.payload_rx_rssi;
packet1.payload_rx_fei = packet_in.payload_rx_fei;
packet1.battery_voltage = packet_in.battery_voltage;
packet1.main_packet_tx_error_count = packet_in.main_packet_tx_error_count;
packet1.main_tx_bitrate = packet_in.main_tx_bitrate;
packet1.main_packet_rx_success_count = packet_in.main_packet_rx_success_count;
packet1.main_packet_rx_drop_count = packet_in.main_packet_rx_drop_count;
packet1.main_rx_bitrate = packet_in.main_rx_bitrate;
packet1.payload_packet_tx_error_count = packet_in.payload_packet_tx_error_count;
packet1.payload_tx_bitrate = packet_in.payload_tx_bitrate;
packet1.payload_packet_rx_success_count = packet_in.payload_packet_rx_success_count;
packet1.payload_packet_rx_drop_count = packet_in.payload_packet_rx_drop_count;
packet1.payload_rx_bitrate = packet_in.payload_rx_bitrate;
packet1.main_radio_present = packet_in.main_radio_present;
packet1.payload_radio_present = packet_in.payload_radio_present;
packet1.ethernet_present = packet_in.ethernet_present;
packet1.ethernet_status = packet_in.ethernet_status;
#ifdef MAVLINK_STATUS_FLAG_OUT_MAVLINK1
......@@ -2132,12 +2151,12 @@ static void mavlink_test_receiver_tm(uint8_t system_id, uint8_t component_id, ma
MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0);
memset(&packet2, 0, sizeof(packet2));
mavlink_msg_receiver_tm_pack(system_id, component_id, &msg , packet1.timestamp , packet1.rssi , packet1.fei , packet1.rx_bitrate , packet1.tx_bitrate );
mavlink_msg_receiver_tm_pack(system_id, component_id, &msg , packet1.timestamp , packet1.main_radio_present , packet1.main_packet_tx_error_count , packet1.main_tx_bitrate , packet1.main_packet_rx_success_count , packet1.main_packet_rx_drop_count , packet1.main_rx_bitrate , packet1.main_rx_rssi , packet1.main_rx_fei , packet1.payload_radio_present , packet1.payload_packet_tx_error_count , packet1.payload_tx_bitrate , packet1.payload_packet_rx_success_count , packet1.payload_packet_rx_drop_count , packet1.payload_rx_bitrate , packet1.payload_rx_rssi , packet1.payload_rx_fei , packet1.ethernet_present , packet1.ethernet_status , packet1.battery_voltage );
mavlink_msg_receiver_tm_decode(&msg, &packet2);
MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0);
memset(&packet2, 0, sizeof(packet2));
mavlink_msg_receiver_tm_pack_chan(system_id, component_id, MAVLINK_COMM_0, &msg , packet1.timestamp , packet1.rssi , packet1.fei , packet1.rx_bitrate , packet1.tx_bitrate );
mavlink_msg_receiver_tm_pack_chan(system_id, component_id, MAVLINK_COMM_0, &msg , packet1.timestamp , packet1.main_radio_present , packet1.main_packet_tx_error_count , packet1.main_tx_bitrate , packet1.main_packet_rx_success_count , packet1.main_packet_rx_drop_count , packet1.main_rx_bitrate , packet1.main_rx_rssi , packet1.main_rx_fei , packet1.payload_radio_present , packet1.payload_packet_tx_error_count , packet1.payload_tx_bitrate , packet1.payload_packet_rx_success_count , packet1.payload_packet_rx_drop_count , packet1.payload_rx_bitrate , packet1.payload_rx_rssi , packet1.payload_rx_fei , packet1.ethernet_present , packet1.ethernet_status , packet1.battery_voltage );
mavlink_msg_receiver_tm_decode(&msg, &packet2);
MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0);
......@@ -2150,7 +2169,7 @@ static void mavlink_test_receiver_tm(uint8_t system_id, uint8_t component_id, ma
MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0);
memset(&packet2, 0, sizeof(packet2));
mavlink_msg_receiver_tm_send(MAVLINK_COMM_1 , packet1.timestamp , packet1.rssi , packet1.fei , packet1.rx_bitrate , packet1.tx_bitrate );
mavlink_msg_receiver_tm_send(MAVLINK_COMM_1 , packet1.timestamp , packet1.main_radio_present , packet1.main_packet_tx_error_count , packet1.main_tx_bitrate , packet1.main_packet_rx_success_count , packet1.main_packet_rx_drop_count , packet1.main_rx_bitrate , packet1.main_rx_rssi , packet1.main_rx_fei , packet1.payload_radio_present , packet1.payload_packet_tx_error_count , packet1.payload_tx_bitrate , packet1.payload_packet_rx_success_count , packet1.payload_packet_rx_drop_count , packet1.payload_rx_bitrate , packet1.payload_rx_rssi , packet1.payload_rx_fei , packet1.ethernet_present , packet1.ethernet_status , packet1.battery_voltage );
mavlink_msg_receiver_tm_decode(last_msg, &packet2);
MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0);
......@@ -2643,45 +2662,50 @@ static void mavlink_test_nas_tm(uint8_t system_id, uint8_t component_id, mavlink
#endif
}
static void mavlink_test_tars_tm(uint8_t system_id, uint8_t component_id, mavlink_message_t *last_msg)
static void mavlink_test_mea_tm(uint8_t system_id, uint8_t component_id, mavlink_message_t *last_msg)
{
#ifdef MAVLINK_STATUS_FLAG_OUT_MAVLINK1
mavlink_status_t *status = mavlink_get_channel_status(MAVLINK_COMM_0);
if ((status->flags & MAVLINK_STATUS_FLAG_OUT_MAVLINK1) && MAVLINK_MSG_ID_TARS_TM >= 256) {
if ((status->flags & MAVLINK_STATUS_FLAG_OUT_MAVLINK1) && MAVLINK_MSG_ID_MEA_TM >= 256) {
return;
}
#endif
mavlink_message_t msg;
uint8_t buffer[MAVLINK_MAX_PACKET_LEN];
uint16_t i;
mavlink_tars_tm_t packet_in = {
93372036854775807ULL,29
mavlink_mea_tm_t packet_in = {
93372036854775807ULL,73.0,101.0,129.0,157.0,185.0,89
};
mavlink_tars_tm_t packet1, packet2;
mavlink_mea_tm_t packet1, packet2;
memset(&packet1, 0, sizeof(packet1));
packet1.timestamp = packet_in.timestamp;
packet1.algorithm_number = packet_in.algorithm_number;
packet1.kalman_x0 = packet_in.kalman_x0;
packet1.kalman_x1 = packet_in.kalman_x1;
packet1.kalman_x2 = packet_in.kalman_x2;
packet1.mass = packet_in.mass;
packet1.corrected_pressure = packet_in.corrected_pressure;
packet1.state = packet_in.state;
#ifdef MAVLINK_STATUS_FLAG_OUT_MAVLINK1
if (status->flags & MAVLINK_STATUS_FLAG_OUT_MAVLINK1) {
// cope with extensions
memset(MAVLINK_MSG_ID_TARS_TM_MIN_LEN + (char *)&packet1, 0, sizeof(packet1)-MAVLINK_MSG_ID_TARS_TM_MIN_LEN);
memset(MAVLINK_MSG_ID_MEA_TM_MIN_LEN + (char *)&packet1, 0, sizeof(packet1)-MAVLINK_MSG_ID_MEA_TM_MIN_LEN);
}
#endif
memset(&packet2, 0, sizeof(packet2));
mavlink_msg_tars_tm_encode(system_id, component_id, &msg, &packet1);
mavlink_msg_tars_tm_decode(&msg, &packet2);
mavlink_msg_mea_tm_encode(system_id, component_id, &msg, &packet1);
mavlink_msg_mea_tm_decode(&msg, &packet2);
MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0);
memset(&packet2, 0, sizeof(packet2));
mavlink_msg_tars_tm_pack(system_id, component_id, &msg , packet1.timestamp , packet1.algorithm_number );
mavlink_msg_tars_tm_decode(&msg, &packet2);
mavlink_msg_mea_tm_pack(system_id, component_id, &msg , packet1.timestamp , packet1.state , packet1.kalman_x0 , packet1.kalman_x1 , packet1.kalman_x2 , packet1.mass , packet1.corrected_pressure );
mavlink_msg_mea_tm_decode(&msg, &packet2);
MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0);
memset(&packet2, 0, sizeof(packet2));
mavlink_msg_tars_tm_pack_chan(system_id, component_id, MAVLINK_COMM_0, &msg , packet1.timestamp , packet1.algorithm_number );
mavlink_msg_tars_tm_decode(&msg, &packet2);
mavlink_msg_mea_tm_pack_chan(system_id, component_id, MAVLINK_COMM_0, &msg , packet1.timestamp , packet1.state , packet1.kalman_x0 , packet1.kalman_x1 , packet1.kalman_x2 , packet1.mass , packet1.corrected_pressure );
mavlink_msg_mea_tm_decode(&msg, &packet2);
MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0);
memset(&packet2, 0, sizeof(packet2));
......@@ -2689,17 +2713,17 @@ static void mavlink_test_tars_tm(uint8_t system_id, uint8_t component_id, mavlin
for (i=0; i<mavlink_msg_get_send_buffer_length(&msg); i++) {
comm_send_ch(MAVLINK_COMM_0, buffer[i]);
}
mavlink_msg_tars_tm_decode(last_msg, &packet2);
mavlink_msg_mea_tm_decode(last_msg, &packet2);
MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0);
memset(&packet2, 0, sizeof(packet2));
mavlink_msg_tars_tm_send(MAVLINK_COMM_1 , packet1.timestamp , packet1.algorithm_number );
mavlink_msg_tars_tm_decode(last_msg, &packet2);
mavlink_msg_mea_tm_send(MAVLINK_COMM_1 , packet1.timestamp , packet1.state , packet1.kalman_x0 , packet1.kalman_x1 , packet1.kalman_x2 , packet1.mass , packet1.corrected_pressure );
mavlink_msg_mea_tm_decode(last_msg, &packet2);
MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0);
#ifdef MAVLINK_HAVE_GET_MESSAGE_INFO
MAVLINK_ASSERT(mavlink_get_message_info_by_name("TARS_TM") != NULL);
MAVLINK_ASSERT(mavlink_get_message_info_by_id(MAVLINK_MSG_ID_TARS_TM) != NULL);
MAVLINK_ASSERT(mavlink_get_message_info_by_name("MEA_TM") != NULL);
MAVLINK_ASSERT(mavlink_get_message_info_by_id(MAVLINK_MSG_ID_MEA_TM) != NULL);
#endif
}
......@@ -2715,7 +2739,7 @@ static void mavlink_test_rocket_flight_tm(uint8_t system_id, uint8_t component_i
uint8_t buffer[MAVLINK_MAX_PACKET_LEN];
uint16_t i;
mavlink_rocket_flight_tm_t packet_in = {
93372036854775807ULL,73.0,101.0,129.0,157.0,185.0,213.0,241.0,269.0,297.0,325.0,353.0,381.0,409.0,437.0,465.0,493.0,521.0,549.0,577.0,605.0,633.0,661.0,689.0,717.0,745.0,773.0,801.0,829.0,857.0,885.0,913.0,941.0,969.0,997.0,1025.0,1053.0,1081.0,1109.0,229,40,107,174,241,52,119,186,253,64,131
93372036854775807ULL,73.0,101.0,129.0,157.0,185.0,213.0,241.0,269.0,297.0,325.0,353.0,381.0,409.0,437.0,465.0,493.0,521.0,549.0,577.0,605.0,633.0,661.0,689.0,717.0,745.0,773.0,801.0,829.0,857.0,885.0,913.0,941.0,969.0,997.0,1025.0,1053.0,1081.0,1109.0,1137.0,241,52,119,186,253,64,131,198,9,76,143,210
};
mavlink_rocket_flight_tm_t packet1, packet2;
memset(&packet1, 0, sizeof(packet1));
......@@ -2727,6 +2751,7 @@ static void mavlink_test_rocket_flight_tm(uint8_t system_id, uint8_t component_i
packet1.airspeed_pitot = packet_in.airspeed_pitot;
packet1.altitude_agl = packet_in.altitude_agl;
packet1.ada_vert_speed = packet_in.ada_vert_speed;
packet1.mea_mass = packet_in.mea_mass;
packet1.acc_x = packet_in.acc_x;
packet1.acc_y = packet_in.acc_y;
packet1.acc_z = packet_in.acc_z;
......@@ -2740,8 +2765,6 @@ static void mavlink_test_rocket_flight_tm(uint8_t system_id, uint8_t component_i
packet1.gps_lon = packet_in.gps_lon;
packet1.gps_alt = packet_in.gps_alt;
packet1.abk_angle = packet_in.abk_angle;
packet1.abk_estimated_cd = packet_in.abk_estimated_cd;
packet1.parachute_load = packet_in.parachute_load;
packet1.nas_n = packet_in.nas_n;
packet1.nas_e = packet_in.nas_e;
packet1.nas_d = packet_in.nas_d;
......@@ -2755,14 +2778,17 @@ static void mavlink_test_rocket_flight_tm(uint8_t system_id, uint8_t component_i
packet1.nas_bias_x = packet_in.nas_bias_x;
packet1.nas_bias_y = packet_in.nas_bias_y;
packet1.nas_bias_z = packet_in.nas_bias_z;
packet1.estimated_thrust = packet_in.estimated_thrust;
packet1.vbat = packet_in.vbat;
packet1.pin_quick_connector = packet_in.pin_quick_connector;
packet1.battery_voltage = packet_in.battery_voltage;
packet1.cam_battery_voltage = packet_in.cam_battery_voltage;
packet1.current_consumption = packet_in.current_consumption;
packet1.temperature = packet_in.temperature;
packet1.ada_state = packet_in.ada_state;
packet1.fmm_state = packet_in.fmm_state;
packet1.dpl_state = packet_in.dpl_state;
packet1.abk_state = packet_in.abk_state;
packet1.nas_state = packet_in.nas_state;
packet1.mea_state = packet_in.mea_state;
packet1.gps_fix = packet_in.gps_fix;
packet1.pin_launch = packet_in.pin_launch;
packet1.pin_nosecone = packet_in.pin_nosecone;
......@@ -2783,12 +2809,12 @@ static void mavlink_test_rocket_flight_tm(uint8_t system_id, uint8_t component_i
MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0);
memset(&packet2, 0, sizeof(packet2));
mavlink_msg_rocket_flight_tm_pack(system_id, component_id, &msg , packet1.timestamp , packet1.ada_state , packet1.fmm_state , packet1.dpl_state , packet1.abk_state , packet1.nas_state , packet1.pressure_ada , packet1.pressure_digi , packet1.pressure_static , packet1.pressure_dpl , packet1.airspeed_pitot , packet1.altitude_agl , packet1.ada_vert_speed , packet1.acc_x , packet1.acc_y , packet1.acc_z , packet1.gyro_x , packet1.gyro_y , packet1.gyro_z , packet1.mag_x , packet1.mag_y , packet1.mag_z , packet1.gps_fix , packet1.gps_lat , packet1.gps_lon , packet1.gps_alt , packet1.abk_angle , packet1.abk_estimated_cd , packet1.parachute_load , packet1.nas_n , packet1.nas_e , packet1.nas_d , packet1.nas_vn , packet1.nas_ve , packet1.nas_vd , packet1.nas_qx , packet1.nas_qy , packet1.nas_qz , packet1.nas_qw , packet1.nas_bias_x , packet1.nas_bias_y , packet1.nas_bias_z , packet1.pin_launch , packet1.pin_nosecone , packet1.pin_expulsion , packet1.cutter_presence , packet1.estimated_thrust , packet1.vbat , packet1.temperature , packet1.logger_error );
mavlink_msg_rocket_flight_tm_pack(system_id, component_id, &msg , packet1.timestamp , packet1.ada_state , packet1.fmm_state , packet1.dpl_state , packet1.abk_state , packet1.nas_state , packet1.mea_state , packet1.pressure_ada , packet1.pressure_digi , packet1.pressure_static , packet1.pressure_dpl , packet1.airspeed_pitot , packet1.altitude_agl , packet1.ada_vert_speed , packet1.mea_mass , packet1.acc_x , packet1.acc_y , packet1.acc_z , packet1.gyro_x , packet1.gyro_y , packet1.gyro_z , packet1.mag_x , packet1.mag_y , packet1.mag_z , packet1.gps_fix , packet1.gps_lat , packet1.gps_lon , packet1.gps_alt , packet1.abk_angle , packet1.nas_n , packet1.nas_e , packet1.nas_d , packet1.nas_vn , packet1.nas_ve , packet1.nas_vd , packet1.nas_qx , packet1.nas_qy , packet1.nas_qz , packet1.nas_qw , packet1.nas_bias_x , packet1.nas_bias_y , packet1.nas_bias_z , packet1.pin_quick_connector , packet1.pin_launch , packet1.pin_nosecone , packet1.pin_expulsion , packet1.cutter_presence , packet1.battery_voltage , packet1.cam_battery_voltage , packet1.current_consumption , packet1.temperature , packet1.logger_error );
mavlink_msg_rocket_flight_tm_decode(&msg, &packet2);
MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0);
memset(&packet2, 0, sizeof(packet2));
mavlink_msg_rocket_flight_tm_pack_chan(system_id, component_id, MAVLINK_COMM_0, &msg , packet1.timestamp , packet1.ada_state , packet1.fmm_state , packet1.dpl_state , packet1.abk_state , packet1.nas_state , packet1.pressure_ada , packet1.pressure_digi , packet1.pressure_static , packet1.pressure_dpl , packet1.airspeed_pitot , packet1.altitude_agl , packet1.ada_vert_speed , packet1.acc_x , packet1.acc_y , packet1.acc_z , packet1.gyro_x , packet1.gyro_y , packet1.gyro_z , packet1.mag_x , packet1.mag_y , packet1.mag_z , packet1.gps_fix , packet1.gps_lat , packet1.gps_lon , packet1.gps_alt , packet1.abk_angle , packet1.abk_estimated_cd , packet1.parachute_load , packet1.nas_n , packet1.nas_e , packet1.nas_d , packet1.nas_vn , packet1.nas_ve , packet1.nas_vd , packet1.nas_qx , packet1.nas_qy , packet1.nas_qz , packet1.nas_qw , packet1.nas_bias_x , packet1.nas_bias_y , packet1.nas_bias_z , packet1.pin_launch , packet1.pin_nosecone , packet1.pin_expulsion , packet1.cutter_presence , packet1.estimated_thrust , packet1.vbat , packet1.temperature , packet1.logger_error );
mavlink_msg_rocket_flight_tm_pack_chan(system_id, component_id, MAVLINK_COMM_0, &msg , packet1.timestamp , packet1.ada_state , packet1.fmm_state , packet1.dpl_state , packet1.abk_state , packet1.nas_state , packet1.mea_state , packet1.pressure_ada , packet1.pressure_digi , packet1.pressure_static , packet1.pressure_dpl , packet1.airspeed_pitot , packet1.altitude_agl , packet1.ada_vert_speed , packet1.mea_mass , packet1.acc_x , packet1.acc_y , packet1.acc_z , packet1.gyro_x , packet1.gyro_y , packet1.gyro_z , packet1.mag_x , packet1.mag_y , packet1.mag_z , packet1.gps_fix , packet1.gps_lat , packet1.gps_lon , packet1.gps_alt , packet1.abk_angle , packet1.nas_n , packet1.nas_e , packet1.nas_d , packet1.nas_vn , packet1.nas_ve , packet1.nas_vd , packet1.nas_qx , packet1.nas_qy , packet1.nas_qz , packet1.nas_qw , packet1.nas_bias_x , packet1.nas_bias_y , packet1.nas_bias_z , packet1.pin_quick_connector , packet1.pin_launch , packet1.pin_nosecone , packet1.pin_expulsion , packet1.cutter_presence , packet1.battery_voltage , packet1.cam_battery_voltage , packet1.current_consumption , packet1.temperature , packet1.logger_error );
mavlink_msg_rocket_flight_tm_decode(&msg, &packet2);
MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0);
......@@ -2801,7 +2827,7 @@ static void mavlink_test_rocket_flight_tm(uint8_t system_id, uint8_t component_i
MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0);
memset(&packet2, 0, sizeof(packet2));
mavlink_msg_rocket_flight_tm_send(MAVLINK_COMM_1 , packet1.timestamp , packet1.ada_state , packet1.fmm_state , packet1.dpl_state , packet1.abk_state , packet1.nas_state , packet1.pressure_ada , packet1.pressure_digi , packet1.pressure_static , packet1.pressure_dpl , packet1.airspeed_pitot , packet1.altitude_agl , packet1.ada_vert_speed , packet1.acc_x , packet1.acc_y , packet1.acc_z , packet1.gyro_x , packet1.gyro_y , packet1.gyro_z , packet1.mag_x , packet1.mag_y , packet1.mag_z , packet1.gps_fix , packet1.gps_lat , packet1.gps_lon , packet1.gps_alt , packet1.abk_angle , packet1.abk_estimated_cd , packet1.parachute_load , packet1.nas_n , packet1.nas_e , packet1.nas_d , packet1.nas_vn , packet1.nas_ve , packet1.nas_vd , packet1.nas_qx , packet1.nas_qy , packet1.nas_qz , packet1.nas_qw , packet1.nas_bias_x , packet1.nas_bias_y , packet1.nas_bias_z , packet1.pin_launch , packet1.pin_nosecone , packet1.pin_expulsion , packet1.cutter_presence , packet1.estimated_thrust , packet1.vbat , packet1.temperature , packet1.logger_error );
mavlink_msg_rocket_flight_tm_send(MAVLINK_COMM_1 , packet1.timestamp , packet1.ada_state , packet1.fmm_state , packet1.dpl_state , packet1.abk_state , packet1.nas_state , packet1.mea_state , packet1.pressure_ada , packet1.pressure_digi , packet1.pressure_static , packet1.pressure_dpl , packet1.airspeed_pitot , packet1.altitude_agl , packet1.ada_vert_speed , packet1.mea_mass , packet1.acc_x , packet1.acc_y , packet1.acc_z , packet1.gyro_x , packet1.gyro_y , packet1.gyro_z , packet1.mag_x , packet1.mag_y , packet1.mag_z , packet1.gps_fix , packet1.gps_lat , packet1.gps_lon , packet1.gps_alt , packet1.abk_angle , packet1.nas_n , packet1.nas_e , packet1.nas_d , packet1.nas_vn , packet1.nas_ve , packet1.nas_vd , packet1.nas_qx , packet1.nas_qy , packet1.nas_qz , packet1.nas_qw , packet1.nas_bias_x , packet1.nas_bias_y , packet1.nas_bias_z , packet1.pin_quick_connector , packet1.pin_launch , packet1.pin_nosecone , packet1.pin_expulsion , packet1.cutter_presence , packet1.battery_voltage , packet1.cam_battery_voltage , packet1.current_consumption , packet1.temperature , packet1.logger_error );
mavlink_msg_rocket_flight_tm_decode(last_msg, &packet2);
MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0);
......@@ -2823,14 +2849,13 @@ static void mavlink_test_payload_flight_tm(uint8_t system_id, uint8_t component_
uint8_t buffer[MAVLINK_MAX_PACKET_LEN];
uint16_t i;
mavlink_payload_flight_tm_t packet_in = {
93372036854775807ULL,73.0,101.0,129.0,157.0,185.0,213.0,241.0,269.0,297.0,325.0,353.0,381.0,409.0,437.0,465.0,493.0,521.0,549.0,577.0,605.0,633.0,661.0,689.0,717.0,745.0,773.0,801.0,829.0,857.0,885.0,913.0,941.0,969.0,997.0,1025.0,1053.0,1081.0,217,28,95,162,229,40
93372036854775807ULL,73.0,101.0,129.0,157.0,185.0,213.0,241.0,269.0,297.0,325.0,353.0,381.0,409.0,437.0,465.0,493.0,521.0,549.0,577.0,605.0,633.0,661.0,689.0,717.0,745.0,773.0,801.0,829.0,857.0,885.0,913.0,941.0,969.0,997.0,1025.0,1053.0,1081.0,217,28,95,162,229,40,107
};
mavlink_payload_flight_tm_t packet1, packet2;
memset(&packet1, 0, sizeof(packet1));
packet1.timestamp = packet_in.timestamp;
packet1.pressure_digi = packet_in.pressure_digi;
packet1.pressure_static = packet_in.pressure_static;
packet1.pressure_dpl = packet_in.pressure_dpl;
packet1.airspeed_pitot = packet_in.airspeed_pitot;
packet1.altitude_agl = packet_in.altitude_agl;
packet1.acc_x = packet_in.acc_x;
......@@ -2862,14 +2887,16 @@ static void mavlink_test_payload_flight_tm(uint8_t system_id, uint8_t component_
packet1.nas_bias_z = packet_in.nas_bias_z;
packet1.wes_n = packet_in.wes_n;
packet1.wes_e = packet_in.wes_e;
packet1.vbat = packet_in.vbat;
packet1.vsupply_5v = packet_in.vsupply_5v;
packet1.battery_voltage = packet_in.battery_voltage;
packet1.cam_battery_voltage = packet_in.cam_battery_voltage;
packet1.current_consumption = packet_in.current_consumption;
packet1.temperature = packet_in.temperature;
packet1.fmm_state = packet_in.fmm_state;
packet1.nas_state = packet_in.nas_state;
packet1.wes_state = packet_in.wes_state;
packet1.gps_fix = packet_in.gps_fix;
packet1.pin_nosecone = packet_in.pin_nosecone;
packet1.cutter_presence = packet_in.cutter_presence;
packet1.logger_error = packet_in.logger_error;
......@@ -2885,12 +2912,12 @@ static void mavlink_test_payload_flight_tm(uint8_t system_id, uint8_t component_
MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0);
memset(&packet2, 0, sizeof(packet2));
mavlink_msg_payload_flight_tm_pack(system_id, component_id, &msg , packet1.timestamp , packet1.fmm_state , packet1.nas_state , packet1.wes_state , packet1.pressure_digi , packet1.pressure_static , packet1.pressure_dpl , packet1.airspeed_pitot , packet1.altitude_agl , packet1.acc_x , packet1.acc_y , packet1.acc_z , packet1.gyro_x , packet1.gyro_y , packet1.gyro_z , packet1.mag_x , packet1.mag_y , packet1.mag_z , packet1.gps_fix , packet1.gps_lat , packet1.gps_lon , packet1.gps_alt , packet1.left_servo_angle , packet1.right_servo_angle , packet1.nas_n , packet1.nas_e , packet1.nas_d , packet1.nas_vn , packet1.nas_ve , packet1.nas_vd , packet1.nas_qx , packet1.nas_qy , packet1.nas_qz , packet1.nas_qw , packet1.nas_bias_x , packet1.nas_bias_y , packet1.nas_bias_z , packet1.wes_n , packet1.wes_e , packet1.pin_nosecone , packet1.vbat , packet1.vsupply_5v , packet1.temperature , packet1.logger_error );
mavlink_msg_payload_flight_tm_pack(system_id, component_id, &msg , packet1.timestamp , packet1.fmm_state , packet1.nas_state , packet1.wes_state , packet1.pressure_digi , packet1.pressure_static , packet1.airspeed_pitot , packet1.altitude_agl , packet1.acc_x , packet1.acc_y , packet1.acc_z , packet1.gyro_x , packet1.gyro_y , packet1.gyro_z , packet1.mag_x , packet1.mag_y , packet1.mag_z , packet1.gps_fix , packet1.gps_lat , packet1.gps_lon , packet1.gps_alt , packet1.left_servo_angle , packet1.right_servo_angle , packet1.nas_n , packet1.nas_e , packet1.nas_d , packet1.nas_vn , packet1.nas_ve , packet1.nas_vd , packet1.nas_qx , packet1.nas_qy , packet1.nas_qz , packet1.nas_qw , packet1.nas_bias_x , packet1.nas_bias_y , packet1.nas_bias_z , packet1.wes_n , packet1.wes_e , packet1.pin_nosecone , packet1.battery_voltage , packet1.cam_battery_voltage , packet1.current_consumption , packet1.cutter_presence , packet1.temperature , packet1.logger_error );
mavlink_msg_payload_flight_tm_decode(&msg, &packet2);
MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0);
memset(&packet2, 0, sizeof(packet2));
mavlink_msg_payload_flight_tm_pack_chan(system_id, component_id, MAVLINK_COMM_0, &msg , packet1.timestamp , packet1.fmm_state , packet1.nas_state , packet1.wes_state , packet1.pressure_digi , packet1.pressure_static , packet1.pressure_dpl , packet1.airspeed_pitot , packet1.altitude_agl , packet1.acc_x , packet1.acc_y , packet1.acc_z , packet1.gyro_x , packet1.gyro_y , packet1.gyro_z , packet1.mag_x , packet1.mag_y , packet1.mag_z , packet1.gps_fix , packet1.gps_lat , packet1.gps_lon , packet1.gps_alt , packet1.left_servo_angle , packet1.right_servo_angle , packet1.nas_n , packet1.nas_e , packet1.nas_d , packet1.nas_vn , packet1.nas_ve , packet1.nas_vd , packet1.nas_qx , packet1.nas_qy , packet1.nas_qz , packet1.nas_qw , packet1.nas_bias_x , packet1.nas_bias_y , packet1.nas_bias_z , packet1.wes_n , packet1.wes_e , packet1.pin_nosecone , packet1.vbat , packet1.vsupply_5v , packet1.temperature , packet1.logger_error );
mavlink_msg_payload_flight_tm_pack_chan(system_id, component_id, MAVLINK_COMM_0, &msg , packet1.timestamp , packet1.fmm_state , packet1.nas_state , packet1.wes_state , packet1.pressure_digi , packet1.pressure_static , packet1.airspeed_pitot , packet1.altitude_agl , packet1.acc_x , packet1.acc_y , packet1.acc_z , packet1.gyro_x , packet1.gyro_y , packet1.gyro_z , packet1.mag_x , packet1.mag_y , packet1.mag_z , packet1.gps_fix , packet1.gps_lat , packet1.gps_lon , packet1.gps_alt , packet1.left_servo_angle , packet1.right_servo_angle , packet1.nas_n , packet1.nas_e , packet1.nas_d , packet1.nas_vn , packet1.nas_ve , packet1.nas_vd , packet1.nas_qx , packet1.nas_qy , packet1.nas_qz , packet1.nas_qw , packet1.nas_bias_x , packet1.nas_bias_y , packet1.nas_bias_z , packet1.wes_n , packet1.wes_e , packet1.pin_nosecone , packet1.battery_voltage , packet1.cam_battery_voltage , packet1.current_consumption , packet1.cutter_presence , packet1.temperature , packet1.logger_error );
mavlink_msg_payload_flight_tm_decode(&msg, &packet2);
MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0);
......@@ -2903,7 +2930,7 @@ static void mavlink_test_payload_flight_tm(uint8_t system_id, uint8_t component_
MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0);
memset(&packet2, 0, sizeof(packet2));
mavlink_msg_payload_flight_tm_send(MAVLINK_COMM_1 , packet1.timestamp , packet1.fmm_state , packet1.nas_state , packet1.wes_state , packet1.pressure_digi , packet1.pressure_static , packet1.pressure_dpl , packet1.airspeed_pitot , packet1.altitude_agl , packet1.acc_x , packet1.acc_y , packet1.acc_z , packet1.gyro_x , packet1.gyro_y , packet1.gyro_z , packet1.mag_x , packet1.mag_y , packet1.mag_z , packet1.gps_fix , packet1.gps_lat , packet1.gps_lon , packet1.gps_alt , packet1.left_servo_angle , packet1.right_servo_angle , packet1.nas_n , packet1.nas_e , packet1.nas_d , packet1.nas_vn , packet1.nas_ve , packet1.nas_vd , packet1.nas_qx , packet1.nas_qy , packet1.nas_qz , packet1.nas_qw , packet1.nas_bias_x , packet1.nas_bias_y , packet1.nas_bias_z , packet1.wes_n , packet1.wes_e , packet1.pin_nosecone , packet1.vbat , packet1.vsupply_5v , packet1.temperature , packet1.logger_error );
mavlink_msg_payload_flight_tm_send(MAVLINK_COMM_1 , packet1.timestamp , packet1.fmm_state , packet1.nas_state , packet1.wes_state , packet1.pressure_digi , packet1.pressure_static , packet1.airspeed_pitot , packet1.altitude_agl , packet1.acc_x , packet1.acc_y , packet1.acc_z , packet1.gyro_x , packet1.gyro_y , packet1.gyro_z , packet1.mag_x , packet1.mag_y , packet1.mag_z , packet1.gps_fix , packet1.gps_lat , packet1.gps_lon , packet1.gps_alt , packet1.left_servo_angle , packet1.right_servo_angle , packet1.nas_n , packet1.nas_e , packet1.nas_d , packet1.nas_vn , packet1.nas_ve , packet1.nas_vd , packet1.nas_qx , packet1.nas_qy , packet1.nas_qz , packet1.nas_qw , packet1.nas_bias_x , packet1.nas_bias_y , packet1.nas_bias_z , packet1.wes_n , packet1.wes_e , packet1.pin_nosecone , packet1.battery_voltage , packet1.cam_battery_voltage , packet1.current_consumption , packet1.cutter_presence , packet1.temperature , packet1.logger_error );
mavlink_msg_payload_flight_tm_decode(last_msg, &packet2);
MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0);
......@@ -3074,12 +3101,12 @@ static void mavlink_test_gse_tm(uint8_t system_id, uint8_t component_id, mavlink
uint8_t buffer[MAVLINK_MAX_PACKET_LEN];
uint16_t i;
mavlink_gse_tm_t packet_in = {
93372036854775807ULL,73.0,101.0,129.0,157.0,185.0,213.0,101,168,235,46,113,180,247
93372036854775807ULL,73.0,101.0,129.0,157.0,185.0,213.0,101,168,235,46,113,180,247,58,125,192
};
mavlink_gse_tm_t packet1, packet2;
memset(&packet1, 0, sizeof(packet1));
packet1.timestamp = packet_in.timestamp;
packet1.loadcell_tank = packet_in.loadcell_tank;
packet1.loadcell_rocket = packet_in.loadcell_rocket;
packet1.loadcell_vessel = packet_in.loadcell_vessel;
packet1.filling_pressure = packet_in.filling_pressure;
packet1.vessel_pressure = packet_in.vessel_pressure;
......@@ -3092,6 +3119,9 @@ static void mavlink_test_gse_tm(uint8_t system_id, uint8_t component_id, mavlink
packet1.main_valve_state = packet_in.main_valve_state;
packet1.ignition_state = packet_in.ignition_state;
packet1.tars_state = packet_in.tars_state;
packet1.main_board_status = packet_in.main_board_status;
packet1.payload_board_status = packet_in.payload_board_status;
packet1.motor_board_status = packet_in.motor_board_status;
#ifdef MAVLINK_STATUS_FLAG_OUT_MAVLINK1
......@@ -3106,12 +3136,12 @@ static void mavlink_test_gse_tm(uint8_t system_id, uint8_t component_id, mavlink
MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0);
memset(&packet2, 0, sizeof(packet2));
mavlink_msg_gse_tm_pack(system_id, component_id, &msg , packet1.timestamp , packet1.loadcell_tank , packet1.loadcell_vessel , packet1.filling_pressure , packet1.vessel_pressure , packet1.arming_state , packet1.filling_valve_state , packet1.venting_valve_state , packet1.release_valve_state , packet1.main_valve_state , packet1.ignition_state , packet1.tars_state , packet1.battery_voltage , packet1.current_consumption );
mavlink_msg_gse_tm_pack(system_id, component_id, &msg , packet1.timestamp , packet1.loadcell_rocket , packet1.loadcell_vessel , packet1.filling_pressure , packet1.vessel_pressure , packet1.arming_state , packet1.filling_valve_state , packet1.venting_valve_state , packet1.release_valve_state , packet1.main_valve_state , packet1.ignition_state , packet1.tars_state , packet1.battery_voltage , packet1.current_consumption , packet1.main_board_status , packet1.payload_board_status , packet1.motor_board_status );
mavlink_msg_gse_tm_decode(&msg, &packet2);
MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0);
memset(&packet2, 0, sizeof(packet2));
mavlink_msg_gse_tm_pack_chan(system_id, component_id, MAVLINK_COMM_0, &msg , packet1.timestamp , packet1.loadcell_tank , packet1.loadcell_vessel , packet1.filling_pressure , packet1.vessel_pressure , packet1.arming_state , packet1.filling_valve_state , packet1.venting_valve_state , packet1.release_valve_state , packet1.main_valve_state , packet1.ignition_state , packet1.tars_state , packet1.battery_voltage , packet1.current_consumption );
mavlink_msg_gse_tm_pack_chan(system_id, component_id, MAVLINK_COMM_0, &msg , packet1.timestamp , packet1.loadcell_rocket , packet1.loadcell_vessel , packet1.filling_pressure , packet1.vessel_pressure , packet1.arming_state , packet1.filling_valve_state , packet1.venting_valve_state , packet1.release_valve_state , packet1.main_valve_state , packet1.ignition_state , packet1.tars_state , packet1.battery_voltage , packet1.current_consumption , packet1.main_board_status , packet1.payload_board_status , packet1.motor_board_status );
mavlink_msg_gse_tm_decode(&msg, &packet2);
MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0);
......@@ -3124,7 +3154,7 @@ static void mavlink_test_gse_tm(uint8_t system_id, uint8_t component_id, mavlink
MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0);
memset(&packet2, 0, sizeof(packet2));
mavlink_msg_gse_tm_send(MAVLINK_COMM_1 , packet1.timestamp , packet1.loadcell_tank , packet1.loadcell_vessel , packet1.filling_pressure , packet1.vessel_pressure , packet1.arming_state , packet1.filling_valve_state , packet1.venting_valve_state , packet1.release_valve_state , packet1.main_valve_state , packet1.ignition_state , packet1.tars_state , packet1.battery_voltage , packet1.current_consumption );
mavlink_msg_gse_tm_send(MAVLINK_COMM_1 , packet1.timestamp , packet1.loadcell_rocket , packet1.loadcell_vessel , packet1.filling_pressure , packet1.vessel_pressure , packet1.arming_state , packet1.filling_valve_state , packet1.venting_valve_state , packet1.release_valve_state , packet1.main_valve_state , packet1.ignition_state , packet1.tars_state , packet1.battery_voltage , packet1.current_consumption , packet1.main_board_status , packet1.payload_board_status , packet1.motor_board_status );
mavlink_msg_gse_tm_decode(last_msg, &packet2);
MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0);
......@@ -3146,7 +3176,7 @@ static void mavlink_test_motor_tm(uint8_t system_id, uint8_t component_id, mavli
uint8_t buffer[MAVLINK_MAX_PACKET_LEN];
uint16_t i;
mavlink_motor_tm_t packet_in = {
93372036854775807ULL,73.0,101.0,129.0,157.0,77,144
93372036854775807ULL,73.0,101.0,129.0,157.0,185.0,213.0,101,168,235
};
mavlink_motor_tm_t packet1, packet2;
memset(&packet1, 0, sizeof(packet1));
......@@ -3155,8 +3185,11 @@ static void mavlink_test_motor_tm(uint8_t system_id, uint8_t component_id, mavli
packet1.bottom_tank_pressure = packet_in.bottom_tank_pressure;
packet1.combustion_chamber_pressure = packet_in.combustion_chamber_pressure;
packet1.tank_temperature = packet_in.tank_temperature;
packet1.battery_voltage = packet_in.battery_voltage;
packet1.current_consumption = packet_in.current_consumption;
packet1.floating_level = packet_in.floating_level;
packet1.main_valve_state = packet_in.main_valve_state;
packet1.venting_valve_state = packet_in.venting_valve_state;
#ifdef MAVLINK_STATUS_FLAG_OUT_MAVLINK1
......@@ -3171,12 +3204,12 @@ static void mavlink_test_motor_tm(uint8_t system_id, uint8_t component_id, mavli
MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0);
memset(&packet2, 0, sizeof(packet2));
mavlink_msg_motor_tm_pack(system_id, component_id, &msg , packet1.timestamp , packet1.top_tank_pressure , packet1.bottom_tank_pressure , packet1.combustion_chamber_pressure , packet1.floating_level , packet1.tank_temperature , packet1.main_valve_state );
mavlink_msg_motor_tm_pack(system_id, component_id, &msg , packet1.timestamp , packet1.top_tank_pressure , packet1.bottom_tank_pressure , packet1.combustion_chamber_pressure , packet1.floating_level , packet1.tank_temperature , packet1.main_valve_state , packet1.venting_valve_state , packet1.battery_voltage , packet1.current_consumption );
mavlink_msg_motor_tm_decode(&msg, &packet2);
MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0);
memset(&packet2, 0, sizeof(packet2));
mavlink_msg_motor_tm_pack_chan(system_id, component_id, MAVLINK_COMM_0, &msg , packet1.timestamp , packet1.top_tank_pressure , packet1.bottom_tank_pressure , packet1.combustion_chamber_pressure , packet1.floating_level , packet1.tank_temperature , packet1.main_valve_state );
mavlink_msg_motor_tm_pack_chan(system_id, component_id, MAVLINK_COMM_0, &msg , packet1.timestamp , packet1.top_tank_pressure , packet1.bottom_tank_pressure , packet1.combustion_chamber_pressure , packet1.floating_level , packet1.tank_temperature , packet1.main_valve_state , packet1.venting_valve_state , packet1.battery_voltage , packet1.current_consumption );
mavlink_msg_motor_tm_decode(&msg, &packet2);
MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0);
......@@ -3189,7 +3222,7 @@ static void mavlink_test_motor_tm(uint8_t system_id, uint8_t component_id, mavli
MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0);
memset(&packet2, 0, sizeof(packet2));
mavlink_msg_motor_tm_send(MAVLINK_COMM_1 , packet1.timestamp , packet1.top_tank_pressure , packet1.bottom_tank_pressure , packet1.combustion_chamber_pressure , packet1.floating_level , packet1.tank_temperature , packet1.main_valve_state );
mavlink_msg_motor_tm_send(MAVLINK_COMM_1 , packet1.timestamp , packet1.top_tank_pressure , packet1.bottom_tank_pressure , packet1.combustion_chamber_pressure , packet1.floating_level , packet1.tank_temperature , packet1.main_valve_state , packet1.venting_valve_state , packet1.battery_voltage , packet1.current_consumption );
mavlink_msg_motor_tm_decode(last_msg, &packet2);
MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0);
......@@ -3243,7 +3276,7 @@ static void mavlink_test_gemini(uint8_t system_id, uint8_t component_id, mavlink
mavlink_test_task_stats_tm(system_id, component_id, last_msg);
mavlink_test_ada_tm(system_id, component_id, last_msg);
mavlink_test_nas_tm(system_id, component_id, last_msg);
mavlink_test_tars_tm(system_id, component_id, last_msg);
mavlink_test_mea_tm(system_id, component_id, last_msg);
mavlink_test_rocket_flight_tm(system_id, component_id, last_msg);
mavlink_test_payload_flight_tm(system_id, component_id, last_msg);
mavlink_test_rocket_stats_tm(system_id, component_id, last_msg);
......
mavlink_lib/gemini/version.h
View file @ 7abedf97
......@@ -7,8 +7,8 @@
#ifndef MAVLINK_VERSION_H
#define MAVLINK_VERSION_H
#define MAVLINK_BUILD_DATE "Fri Apr 21 2023"
#define MAVLINK_BUILD_DATE "Wed Sep 13 2023"
#define MAVLINK_WIRE_PROTOCOL_VERSION "1.0"
#define MAVLINK_MAX_DIALECT_PAYLOAD_SIZE 171
#define MAVLINK_MAX_DIALECT_PAYLOAD_SIZE 176
#endif // MAVLINK_VERSION_H
mavlink_lib/lyra/lyra.h 0 → 100644
View file @ 7abedf97
/** @file
* @brief MAVLink comm protocol generated from lyra.xml
* @see http://mavlink.org
*/
#pragma once
#ifndef MAVLINK_LYRA_H
#define MAVLINK_LYRA_H
#ifndef MAVLINK_H
#error Wrong include order: MAVLINK_LYRA.H MUST NOT BE DIRECTLY USED. Include mavlink.h from the same directory instead or set ALL AND EVERY defines from MAVLINK.H manually accordingly, including the #define MAVLINK_H call.
#endif
#undef MAVLINK_THIS_XML_HASH
#define MAVLINK_THIS_XML_HASH -5660799532835485979
#ifdef __cplusplus
extern "C" {
#endif
// MESSAGE LENGTHS AND CRCS
#ifndef MAVLINK_MESSAGE_LENGTHS
#define MAVLINK_MESSAGE_LENGTHS {0, 8, 1, 1, 1, 1, 5, 1, 1, 4, 4, 12, 16, 8, 2, 4, 8, 1, 4, 4, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 5, 5, 7, 4, 4, 4, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 5, 5, 5, 12, 12, 1, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 2, 4, 4, 74, 64, 32, 60, 32, 32, 32, 32, 56, 22, 5, 19, 36, 36, 36, 40, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 104, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 16, 46, 28, 20, 44, 53, 77, 29, 178, 158, 180, 170, 64, 37, 76, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0}
#endif
#ifndef MAVLINK_MESSAGE_CRCS
#define MAVLINK_MESSAGE_CRCS {0, 136, 198, 165, 248, 184, 215, 226, 160, 113, 38, 71, 168, 67, 218, 44, 81, 181, 199, 221, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 110, 22, 65, 79, 167, 84, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 180, 246, 173, 183, 220, 181, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 50, 251, 51, 57, 72, 87, 229, 245, 212, 140, 148, 6, 165, 87, 255, 103, 9, 68, 234, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 239, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 48, 142, 108, 39, 19, 234, 66, 11, 235, 188, 195, 99, 87, 67, 210, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0}
#endif
#include "../protocol.h"
#define MAVLINK_ENABLED_LYRA
// ENUM DEFINITIONS
/** @brief Enum that lists all the system IDs of the various devices */
#ifndef HAVE_ENUM_SysIDs
#define HAVE_ENUM_SysIDs
typedef enum SysIDs
{
MAV_SYSID_MAIN=1, /* | */
MAV_SYSID_PAYLOAD=2, /* | */
MAV_SYSID_RIG=3, /* | */
MAV_SYSID_GS=4, /* | */
MAV_SYSID_ARP=5, /* | */
MAV_SYSID_GS_BACKUP=6, /* | */
MAV_SYSID_ARP_BACKUP=7, /* | */
SysIDs_ENUM_END=8, /* | */
} SysIDs;
#endif
/** @brief Enum list for all the telemetries that can be requested */
#ifndef HAVE_ENUM_SystemTMList
#define HAVE_ENUM_SystemTMList
typedef enum SystemTMList
{
MAV_SYS_ID=1, /* State of init results about system hardware/software components | */
MAV_PIN_OBS_ID=2, /* Pin observer data | */
MAV_LOGGER_ID=3, /* SD Logger stats | */
MAV_MAVLINK_STATS_ID=4, /* Mavlink driver stats | */
MAV_TASK_STATS_ID=5, /* Task scheduler statistics answer: n mavlink messages where n is the number of tasks | */
MAV_ADA_ID=6, /* ADA Status | */
MAV_NAS_ID=7, /* NavigationSystem data | */
MAV_MEA_ID=8, /* MEA Status | */
MAV_CAN_STATS_ID=9, /* Canbus stats | */
MAV_FLIGHT_ID=10, /* Flight telemetry | */
MAV_STATS_ID=11, /* Satistics telemetry | */
MAV_SENSORS_STATE_ID=12, /* Sensors init state telemetry | */
MAV_GSE_ID=13, /* Ground Segnement Equipment | */
MAV_MOTOR_ID=14, /* Rocket Motor data | */
MAV_REGISTRY_ID=15, /* Command to fetch all registry keys | */
MAV_REFERENCE_ID=16, /* Command to fetch reference values | */
MAV_CALIBRATION_ID=17, /* Command to fetch calibration values | */
SystemTMList_ENUM_END=18, /* | */
} SystemTMList;
#endif
/** @brief Enum list of all sensors telemetries that can be requested */
#ifndef HAVE_ENUM_SensorsTMList
#define HAVE_ENUM_SensorsTMList
typedef enum SensorsTMList
{
MAV_BMX160_ID=1, /* BMX160 IMU data | */
MAV_VN100_ID=2, /* VN100 IMU data | */
MAV_MPU9250_ID=3, /* MPU9250 IMU data | */
MAV_ADS131M08_ID=4, /* ADS 8 channel ADC data | */
MAV_MS5803_ID=5, /* MS5803 barometer data | */
MAV_BME280_ID=6, /* BME280 barometer data | */
MAV_LIS3MDL_ID=7, /* LIS3MDL compass data | */
MAV_LIS2MDL_ID=8, /* Magnetometer data | */
MAV_LPS28DFW_ID=9, /* Pressure sensor data | */
MAV_LSM6DSRX_ID=10, /* IMU data | */
MAV_H3LIS331DL_ID=11, /* 400G accelerometer | */
MAV_LPS22DF_ID=12, /* Pressure sensor data | */
MAV_GPS_ID=13, /* GPS data | */
MAV_CURRENT_SENSE_ID=14, /* Electrical current sensors data | */
MAV_BATTERY_VOLTAGE_ID=15, /* Battery voltage data | */
MAV_ROTATED_IMU_ID=16, /* Load cell data | */
MAV_DPL_PRESS_ID=17, /* Deployment pressure data | */
MAV_STATIC_PRESS_ID=18, /* Static pressure data | */
MAV_BACKUP_STATIC_PRESS_ID=19, /* Static pressure data | */
MAV_STATIC_PITOT_PRESS_ID=20, /* Pitot pressure data | */
MAV_TOTAL_PITOT_PRESS_ID=21, /* Pitot pressure data | */
MAV_DYNAMIC_PITOT_PRESS_ID=22, /* Pitot pressure data | */
MAV_LOAD_CELL_ID=23, /* Load cell data | */
MAV_TANK_TOP_PRESS_ID=24, /* Top tank pressure | */
MAV_TANK_BOTTOM_PRESS_ID=25, /* Bottom tank pressure | */
MAV_TANK_TEMP_ID=26, /* Tank temperature | */
MAV_COMBUSTION_PRESS_ID=27, /* Combustion chamber pressure | */
MAV_FILLING_PRESS_ID=28, /* Filling line pressure | */
MAV_VESSEL_PRESS_ID=29, /* Vessel pressure | */
MAV_LOAD_CELL_VESSEL_ID=30, /* Vessel tank weight | */
MAV_LOAD_CELL_TANK_ID=31, /* Tank weight | */
SensorsTMList_ENUM_END=32, /* | */
} SensorsTMList;
#endif
/** @brief Enum of the commands */
#ifndef HAVE_ENUM_MavCommandList
#define HAVE_ENUM_MavCommandList
typedef enum MavCommandList
{
MAV_CMD_ARM=1, /* Command to arm the rocket | */
MAV_CMD_DISARM=2, /* Command to disarm the rocket | */
MAV_CMD_CALIBRATE=3, /* Command to trigger the calibration | */
MAV_CMD_SAVE_CALIBRATION=4, /* Command to save the current calibration into a file | */
MAV_CMD_FORCE_INIT=5, /* Command to init the rocket | */
MAV_CMD_FORCE_LAUNCH=6, /* Command to force the launch state on the rocket | */
MAV_CMD_FORCE_ENGINE_SHUTDOWN=7, /* Command to trigger engine shutdown | */
MAV_CMD_FORCE_EXPULSION=8, /* Command to trigger nosecone expulsion | */
MAV_CMD_FORCE_DEPLOYMENT=9, /* Command to activate the thermal cutters and cut the drogue, activating both thermal cutters sequentially | */
MAV_CMD_FORCE_LANDING=10, /* Command to communicate the end of the mission and close the file descriptors in the SD card | */
MAV_CMD_START_LOGGING=11, /* Command to enable sensor logging | */
MAV_CMD_STOP_LOGGING=12, /* Command to permanently close the log file | */
MAV_CMD_FORCE_REBOOT=13, /* Command to reset the board from test status | */
MAV_CMD_ENTER_TEST_MODE=14, /* Command to enter the test mode | */
MAV_CMD_EXIT_TEST_MODE=15, /* Command to exit the test mode | */
MAV_CMD_START_RECORDING=16, /* Command to start the internal cameras recordings | */
MAV_CMD_STOP_RECORDING=17, /* Command to stop the internal cameras recordings | */
MAV_CMD_OPEN_NITROGEN=18, /* Command to open the nitrogen valve | */
MAV_CMD_REGISTRY_LOAD=19, /* Command to reload the registry from memory | */
MAV_CMD_REGISTRY_SAVE=20, /* Command to commit the registry to memory | */
MAV_CMD_REGISTRY_CLEAR=21, /* Command to clear the registry | */
MAV_CMD_ENTER_HIL=22, /* Command to enter HIL mode at next reboot | */
MAV_CMD_EXIT_HIL=23, /* Command to exit HIL mode at next reboot | */
MAV_CMD_RESET_ALGORITHM=24, /* Command to reset the set algorithm. Used for now in ARP to reset the follow algorithm and return to armed state. | */
MAV_CMD_ARP_FORCE_NO_FEEDBACK=25, /* Command to force ARP system to entern the no feedback from VN300 state | */
MAV_CMD_ARP_FOLLOW=26, /* Command to enter in the ARP's follow state and procedure to follow the rocket | */
MavCommandList_ENUM_END=27, /* | */
} MavCommandList;
#endif
/** @brief Enum of all the servos */
#ifndef HAVE_ENUM_ServosList
#define HAVE_ENUM_ServosList
typedef enum ServosList
{
AIR_BRAKES_SERVO=1, /* | */
EXPULSION_SERVO=2, /* | */
PARAFOIL_LEFT_SERVO=3, /* | */
PARAFOIL_RIGHT_SERVO=4, /* | */
MAIN_VALVE=5, /* | */
VENTING_VALVE=6, /* | */
RELEASE_VALVE=7, /* | */
FILLING_VALVE=8, /* | */
DISCONNECT_SERVO=9, /* | */
ServosList_ENUM_END=10, /* | */
} ServosList;
#endif
/** @brief Enum of all the steppers */
#ifndef HAVE_ENUM_StepperList
#define HAVE_ENUM_StepperList
typedef enum StepperList
{
STEPPER_X=1, /* | */
STEPPER_Y=2, /* | */
StepperList_ENUM_END=3, /* | */
} StepperList;
#endif
/** @brief Enum of all the pins */
#ifndef HAVE_ENUM_PinsList
#define HAVE_ENUM_PinsList
typedef enum PinsList
{
RAMP_PIN=1, /* | */
NOSECONE_PIN=2, /* | */
PinsList_ENUM_END=3, /* | */
} PinsList;
#endif
// MAVLINK VERSION
#ifndef MAVLINK_VERSION
#define MAVLINK_VERSION 1
#endif
#if (MAVLINK_VERSION == 0)
#undef MAVLINK_VERSION
#define MAVLINK_VERSION 1
#endif
// MESSAGE DEFINITIONS
#include "./mavlink_msg_ping_tc.h"
#include "./mavlink_msg_command_tc.h"
#include "./mavlink_msg_system_tm_request_tc.h"
#include "./mavlink_msg_sensor_tm_request_tc.h"
#include "./mavlink_msg_servo_tm_request_tc.h"
#include "./mavlink_msg_set_servo_angle_tc.h"
#include "./mavlink_msg_reset_servo_tc.h"
#include "./mavlink_msg_wiggle_servo_tc.h"
#include "./mavlink_msg_set_reference_altitude_tc.h"
#include "./mavlink_msg_set_reference_temperature_tc.h"
#include "./mavlink_msg_set_orientation_tc.h"
#include "./mavlink_msg_set_orientation_quat_tc.h"
#include "./mavlink_msg_set_coordinates_tc.h"
#include "./mavlink_msg_raw_event_tc.h"
#include "./mavlink_msg_set_deployment_altitude_tc.h"
#include "./mavlink_msg_set_target_coordinates_tc.h"
#include "./mavlink_msg_set_algorithm_tc.h"
#include "./mavlink_msg_set_calibration_pressure_tc.h"
#include "./mavlink_msg_set_initial_mea_mass_tc.h"
#include "./mavlink_msg_set_atomic_valve_timing_tc.h"
#include "./mavlink_msg_set_valve_maximum_aperture_tc.h"
#include "./mavlink_msg_conrig_state_tc.h"
#include "./mavlink_msg_set_ignition_time_tc.h"
#include "./mavlink_msg_set_nitrogen_time_tc.h"
#include "./mavlink_msg_set_cooling_time_tc.h"
#include "./mavlink_msg_set_stepper_angle_tc.h"
#include "./mavlink_msg_set_stepper_steps_tc.h"
#include "./mavlink_msg_set_stepper_multiplier_tc.h"
#include "./mavlink_msg_set_antenna_coordinates_arp_tc.h"
#include "./mavlink_msg_set_rocket_coordinates_arp_tc.h"
#include "./mavlink_msg_arp_command_tc.h"
#include "./mavlink_msg_ack_tm.h"
#include "./mavlink_msg_nack_tm.h"
#include "./mavlink_msg_wack_tm.h"
#include "./mavlink_msg_gps_tm.h"
#include "./mavlink_msg_imu_tm.h"
#include "./mavlink_msg_pressure_tm.h"
#include "./mavlink_msg_adc_tm.h"
#include "./mavlink_msg_voltage_tm.h"
#include "./mavlink_msg_current_tm.h"
#include "./mavlink_msg_temp_tm.h"
#include "./mavlink_msg_load_tm.h"
#include "./mavlink_msg_attitude_tm.h"
#include "./mavlink_msg_sensor_state_tm.h"
#include "./mavlink_msg_servo_tm.h"
#include "./mavlink_msg_pin_tm.h"
#include "./mavlink_msg_reference_tm.h"
#include "./mavlink_msg_registry_float_tm.h"
#include "./mavlink_msg_registry_int_tm.h"
#include "./mavlink_msg_registry_coord_tm.h"
#include "./mavlink_msg_arp_tm.h"
#include "./mavlink_msg_sys_tm.h"
#include "./mavlink_msg_logger_tm.h"
#include "./mavlink_msg_mavlink_stats_tm.h"
#include "./mavlink_msg_can_stats_tm.h"
#include "./mavlink_msg_task_stats_tm.h"
#include "./mavlink_msg_ada_tm.h"
#include "./mavlink_msg_nas_tm.h"
#include "./mavlink_msg_mea_tm.h"
#include "./mavlink_msg_rocket_flight_tm.h"
#include "./mavlink_msg_payload_flight_tm.h"
#include "./mavlink_msg_rocket_stats_tm.h"
#include "./mavlink_msg_payload_stats_tm.h"
#include "./mavlink_msg_gse_tm.h"
#include "./mavlink_msg_motor_tm.h"
#include "./mavlink_msg_calibration_tm.h"
// base include
#undef MAVLINK_THIS_XML_HASH
#define MAVLINK_THIS_XML_HASH -5660799532835485979
#if MAVLINK_THIS_XML_HASH == MAVLINK_PRIMARY_XML_HASH
# define MAVLINK_MESSAGE_INFO {{"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_PING_TC, MAVLINK_MESSAGE_INFO_COMMAND_TC, MAVLINK_MESSAGE_INFO_SYSTEM_TM_REQUEST_TC, MAVLINK_MESSAGE_INFO_SENSOR_TM_REQUEST_TC, MAVLINK_MESSAGE_INFO_SERVO_TM_REQUEST_TC, MAVLINK_MESSAGE_INFO_SET_SERVO_ANGLE_TC, MAVLINK_MESSAGE_INFO_RESET_SERVO_TC, MAVLINK_MESSAGE_INFO_WIGGLE_SERVO_TC, MAVLINK_MESSAGE_INFO_SET_REFERENCE_ALTITUDE_TC, MAVLINK_MESSAGE_INFO_SET_REFERENCE_TEMPERATURE_TC, MAVLINK_MESSAGE_INFO_SET_ORIENTATION_TC, MAVLINK_MESSAGE_INFO_SET_ORIENTATION_QUAT_TC, MAVLINK_MESSAGE_INFO_SET_COORDINATES_TC, MAVLINK_MESSAGE_INFO_RAW_EVENT_TC, MAVLINK_MESSAGE_INFO_SET_DEPLOYMENT_ALTITUDE_TC, MAVLINK_MESSAGE_INFO_SET_TARGET_COORDINATES_TC, MAVLINK_MESSAGE_INFO_SET_ALGORITHM_TC, MAVLINK_MESSAGE_INFO_SET_CALIBRATION_PRESSURE_TC, MAVLINK_MESSAGE_INFO_SET_INITIAL_MEA_MASS_TC, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_SET_ATOMIC_VALVE_TIMING_TC, MAVLINK_MESSAGE_INFO_SET_VALVE_MAXIMUM_APERTURE_TC, MAVLINK_MESSAGE_INFO_CONRIG_STATE_TC, MAVLINK_MESSAGE_INFO_SET_IGNITION_TIME_TC, MAVLINK_MESSAGE_INFO_SET_NITROGEN_TIME_TC, MAVLINK_MESSAGE_INFO_SET_COOLING_TIME_TC, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_SET_STEPPER_ANGLE_TC, MAVLINK_MESSAGE_INFO_SET_STEPPER_STEPS_TC, MAVLINK_MESSAGE_INFO_SET_STEPPER_MULTIPLIER_TC, MAVLINK_MESSAGE_INFO_SET_ANTENNA_COORDINATES_ARP_TC, MAVLINK_MESSAGE_INFO_SET_ROCKET_COORDINATES_ARP_TC, MAVLINK_MESSAGE_INFO_ARP_COMMAND_TC, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_ACK_TM, MAVLINK_MESSAGE_INFO_NACK_TM, MAVLINK_MESSAGE_INFO_WACK_TM, MAVLINK_MESSAGE_INFO_GPS_TM, MAVLINK_MESSAGE_INFO_IMU_TM, MAVLINK_MESSAGE_INFO_PRESSURE_TM, MAVLINK_MESSAGE_INFO_ADC_TM, MAVLINK_MESSAGE_INFO_VOLTAGE_TM, MAVLINK_MESSAGE_INFO_CURRENT_TM, MAVLINK_MESSAGE_INFO_TEMP_TM, MAVLINK_MESSAGE_INFO_LOAD_TM, MAVLINK_MESSAGE_INFO_ATTITUDE_TM, MAVLINK_MESSAGE_INFO_SENSOR_STATE_TM, MAVLINK_MESSAGE_INFO_SERVO_TM, MAVLINK_MESSAGE_INFO_PIN_TM, MAVLINK_MESSAGE_INFO_REFERENCE_TM, MAVLINK_MESSAGE_INFO_REGISTRY_FLOAT_TM, MAVLINK_MESSAGE_INFO_REGISTRY_INT_TM, MAVLINK_MESSAGE_INFO_REGISTRY_COORD_TM, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_ARP_TM, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, MAVLINK_MESSAGE_INFO_SYS_TM, MAVLINK_MESSAGE_INFO_LOGGER_TM, MAVLINK_MESSAGE_INFO_MAVLINK_STATS_TM, MAVLINK_MESSAGE_INFO_CAN_STATS_TM, MAVLINK_MESSAGE_INFO_TASK_STATS_TM, MAVLINK_MESSAGE_INFO_ADA_TM, MAVLINK_MESSAGE_INFO_NAS_TM, MAVLINK_MESSAGE_INFO_MEA_TM, MAVLINK_MESSAGE_INFO_ROCKET_FLIGHT_TM, MAVLINK_MESSAGE_INFO_PAYLOAD_FLIGHT_TM, MAVLINK_MESSAGE_INFO_ROCKET_STATS_TM, MAVLINK_MESSAGE_INFO_PAYLOAD_STATS_TM, MAVLINK_MESSAGE_INFO_GSE_TM, MAVLINK_MESSAGE_INFO_MOTOR_TM, MAVLINK_MESSAGE_INFO_CALIBRATION_TM, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}}
# define MAVLINK_MESSAGE_NAMES {{ "ACK_TM", 100 }, { "ADA_TM", 205 }, { "ADC_TM", 106 }, { "ARP_COMMAND_TC", 65 }, { "ARP_TM", 150 }, { "ATTITUDE_TM", 111 }, { "CALIBRATION_TM", 214 }, { "CAN_STATS_TM", 203 }, { "COMMAND_TC", 2 }, { "CONRIG_STATE_TC", 32 }, { "CURRENT_TM", 108 }, { "GPS_TM", 103 }, { "GSE_TM", 212 }, { "IMU_TM", 104 }, { "LOAD_TM", 110 }, { "LOGGER_TM", 201 }, { "MAVLINK_STATS_TM", 202 }, { "MEA_TM", 207 }, { "MOTOR_TM", 213 }, { "NACK_TM", 101 }, { "NAS_TM", 206 }, { "PAYLOAD_FLIGHT_TM", 209 }, { "PAYLOAD_STATS_TM", 211 }, { "PING_TC", 1 }, { "PIN_TM", 114 }, { "PRESSURE_TM", 105 }, { "RAW_EVENT_TC", 14 }, { "REFERENCE_TM", 115 }, { "REGISTRY_COORD_TM", 118 }, { "REGISTRY_FLOAT_TM", 116 }, { "REGISTRY_INT_TM", 117 }, { "RESET_SERVO_TC", 7 }, { "ROCKET_FLIGHT_TM", 208 }, { "ROCKET_STATS_TM", 210 }, { "SENSOR_STATE_TM", 112 }, { "SENSOR_TM_REQUEST_TC", 4 }, { "SERVO_TM", 113 }, { "SERVO_TM_REQUEST_TC", 5 }, { "SET_ALGORITHM_TC", 17 }, { "SET_ANTENNA_COORDINATES_ARP_TC", 63 }, { "SET_ATOMIC_VALVE_TIMING_TC", 30 }, { "SET_CALIBRATION_PRESSURE_TC", 18 }, { "SET_COOLING_TIME_TC", 35 }, { "SET_COORDINATES_TC", 13 }, { "SET_DEPLOYMENT_ALTITUDE_TC", 15 }, { "SET_IGNITION_TIME_TC", 33 }, { "SET_INITIAL_MEA_MASS_TC", 19 }, { "SET_NITROGEN_TIME_TC", 34 }, { "SET_ORIENTATION_QUAT_TC", 12 }, { "SET_ORIENTATION_TC", 11 }, { "SET_REFERENCE_ALTITUDE_TC", 9 }, { "SET_REFERENCE_TEMPERATURE_TC", 10 }, { "SET_ROCKET_COORDINATES_ARP_TC", 64 }, { "SET_SERVO_ANGLE_TC", 6 }, { "SET_STEPPER_ANGLE_TC", 60 }, { "SET_STEPPER_MULTIPLIER_TC", 62 }, { "SET_STEPPER_STEPS_TC", 61 }, { "SET_TARGET_COORDINATES_TC", 16 }, { "SET_VALVE_MAXIMUM_APERTURE_TC", 31 }, { "SYSTEM_TM_REQUEST_TC", 3 }, { "SYS_TM", 200 }, { "TASK_STATS_TM", 204 }, { "TEMP_TM", 109 }, { "VOLTAGE_TM", 107 }, { "WACK_TM", 102 }, { "WIGGLE_SERVO_TC", 8 }}
# if MAVLINK_COMMAND_24BIT
# include "../mavlink_get_info.h"
# endif
#endif
#ifdef __cplusplus
}
#endif // __cplusplus
#endif // MAVLINK_LYRA_H
mavlink_lib/lyra/mavlink.h 0 → 100644
View file @ 7abedf97
/** @file
* @brief MAVLink comm protocol built from lyra.xml
* @see http://mavlink.org
*/
#pragma once
#ifndef MAVLINK_H
#define MAVLINK_H
#define MAVLINK_PRIMARY_XML_HASH -5660799532835485979
#ifndef MAVLINK_STX
#define MAVLINK_STX 254
#endif
#ifndef MAVLINK_ENDIAN
#define MAVLINK_ENDIAN MAVLINK_LITTLE_ENDIAN
#endif
#ifndef MAVLINK_ALIGNED_FIELDS
#define MAVLINK_ALIGNED_FIELDS 1
#endif
#ifndef MAVLINK_CRC_EXTRA
#define MAVLINK_CRC_EXTRA 1
#endif
#ifndef MAVLINK_COMMAND_24BIT
#define MAVLINK_COMMAND_24BIT 0
#endif
#include "version.h"
#include "lyra.h"
#endif // MAVLINK_H
mavlink_lib/lyra/mavlink_msg_ack_tm.h 0 → 100644
View file @ 7abedf97
#pragma once
// MESSAGE ACK_TM PACKING
#define MAVLINK_MSG_ID_ACK_TM 100
typedef struct __mavlink_ack_tm_t {
uint8_t recv_msgid; /*< Message id of the received message*/
uint8_t seq_ack; /*< Sequence number of the received message*/
} mavlink_ack_tm_t;
#define MAVLINK_MSG_ID_ACK_TM_LEN 2
#define MAVLINK_MSG_ID_ACK_TM_MIN_LEN 2
#define MAVLINK_MSG_ID_100_LEN 2
#define MAVLINK_MSG_ID_100_MIN_LEN 2
#define MAVLINK_MSG_ID_ACK_TM_CRC 50
#define MAVLINK_MSG_ID_100_CRC 50
#if MAVLINK_COMMAND_24BIT
#define MAVLINK_MESSAGE_INFO_ACK_TM { \
100, \
"ACK_TM", \
2, \
{ { "recv_msgid", NULL, MAVLINK_TYPE_UINT8_T, 0, 0, offsetof(mavlink_ack_tm_t, recv_msgid) }, \
{ "seq_ack", NULL, MAVLINK_TYPE_UINT8_T, 0, 1, offsetof(mavlink_ack_tm_t, seq_ack) }, \
} \
}
#else
#define MAVLINK_MESSAGE_INFO_ACK_TM { \
"ACK_TM", \
2, \
{ { "recv_msgid", NULL, MAVLINK_TYPE_UINT8_T, 0, 0, offsetof(mavlink_ack_tm_t, recv_msgid) }, \
{ "seq_ack", NULL, MAVLINK_TYPE_UINT8_T, 0, 1, offsetof(mavlink_ack_tm_t, seq_ack) }, \
} \
}
#endif
/**
* @brief Pack a ack_tm message
* @param system_id ID of this system
* @param component_id ID of this component (e.g. 200 for IMU)
* @param msg The MAVLink message to compress the data into
*
* @param recv_msgid Message id of the received message
* @param seq_ack Sequence number of the received message
* @return length of the message in bytes (excluding serial stream start sign)
*/
static inline uint16_t mavlink_msg_ack_tm_pack(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg,
uint8_t recv_msgid, uint8_t seq_ack)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char buf[MAVLINK_MSG_ID_ACK_TM_LEN];
_mav_put_uint8_t(buf, 0, recv_msgid);
_mav_put_uint8_t(buf, 1, seq_ack);
memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_ACK_TM_LEN);
#else
mavlink_ack_tm_t packet;
packet.recv_msgid = recv_msgid;
packet.seq_ack = seq_ack;
memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_ACK_TM_LEN);
#endif
msg->msgid = MAVLINK_MSG_ID_ACK_TM;
return mavlink_finalize_message(msg, system_id, component_id, MAVLINK_MSG_ID_ACK_TM_MIN_LEN, MAVLINK_MSG_ID_ACK_TM_LEN, MAVLINK_MSG_ID_ACK_TM_CRC);
}
/**
* @brief Pack a ack_tm message on a channel
* @param system_id ID of this system
* @param component_id ID of this component (e.g. 200 for IMU)
* @param chan The MAVLink channel this message will be sent over
* @param msg The MAVLink message to compress the data into
* @param recv_msgid Message id of the received message
* @param seq_ack Sequence number of the received message
* @return length of the message in bytes (excluding serial stream start sign)
*/
static inline uint16_t mavlink_msg_ack_tm_pack_chan(uint8_t system_id, uint8_t component_id, uint8_t chan,
mavlink_message_t* msg,
uint8_t recv_msgid,uint8_t seq_ack)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char buf[MAVLINK_MSG_ID_ACK_TM_LEN];
_mav_put_uint8_t(buf, 0, recv_msgid);
_mav_put_uint8_t(buf, 1, seq_ack);
memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_ACK_TM_LEN);
#else
mavlink_ack_tm_t packet;
packet.recv_msgid = recv_msgid;
packet.seq_ack = seq_ack;
memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_ACK_TM_LEN);
#endif
msg->msgid = MAVLINK_MSG_ID_ACK_TM;
return mavlink_finalize_message_chan(msg, system_id, component_id, chan, MAVLINK_MSG_ID_ACK_TM_MIN_LEN, MAVLINK_MSG_ID_ACK_TM_LEN, MAVLINK_MSG_ID_ACK_TM_CRC);
}
/**
* @brief Encode a ack_tm struct
*
* @param system_id ID of this system
* @param component_id ID of this component (e.g. 200 for IMU)
* @param msg The MAVLink message to compress the data into
* @param ack_tm C-struct to read the message contents from
*/
static inline uint16_t mavlink_msg_ack_tm_encode(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg, const mavlink_ack_tm_t* ack_tm)
{
return mavlink_msg_ack_tm_pack(system_id, component_id, msg, ack_tm->recv_msgid, ack_tm->seq_ack);
}
/**
* @brief Encode a ack_tm struct on a channel
*
* @param system_id ID of this system
* @param component_id ID of this component (e.g. 200 for IMU)
* @param chan The MAVLink channel this message will be sent over
* @param msg The MAVLink message to compress the data into
* @param ack_tm C-struct to read the message contents from
*/
static inline uint16_t mavlink_msg_ack_tm_encode_chan(uint8_t system_id, uint8_t component_id, uint8_t chan, mavlink_message_t* msg, const mavlink_ack_tm_t* ack_tm)
{
return mavlink_msg_ack_tm_pack_chan(system_id, component_id, chan, msg, ack_tm->recv_msgid, ack_tm->seq_ack);
}
/**
* @brief Send a ack_tm message
* @param chan MAVLink channel to send the message
*
* @param recv_msgid Message id of the received message
* @param seq_ack Sequence number of the received message
*/
#ifdef MAVLINK_USE_CONVENIENCE_FUNCTIONS
static inline void mavlink_msg_ack_tm_send(mavlink_channel_t chan, uint8_t recv_msgid, uint8_t seq_ack)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char buf[MAVLINK_MSG_ID_ACK_TM_LEN];
_mav_put_uint8_t(buf, 0, recv_msgid);
_mav_put_uint8_t(buf, 1, seq_ack);
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_ACK_TM, buf, MAVLINK_MSG_ID_ACK_TM_MIN_LEN, MAVLINK_MSG_ID_ACK_TM_LEN, MAVLINK_MSG_ID_ACK_TM_CRC);
#else
mavlink_ack_tm_t packet;
packet.recv_msgid = recv_msgid;
packet.seq_ack = seq_ack;
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_ACK_TM, (const char *)&packet, MAVLINK_MSG_ID_ACK_TM_MIN_LEN, MAVLINK_MSG_ID_ACK_TM_LEN, MAVLINK_MSG_ID_ACK_TM_CRC);
#endif
}
/**
* @brief Send a ack_tm message
* @param chan MAVLink channel to send the message
* @param struct The MAVLink struct to serialize
*/
static inline void mavlink_msg_ack_tm_send_struct(mavlink_channel_t chan, const mavlink_ack_tm_t* ack_tm)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
mavlink_msg_ack_tm_send(chan, ack_tm->recv_msgid, ack_tm->seq_ack);
#else
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_ACK_TM, (const char *)ack_tm, MAVLINK_MSG_ID_ACK_TM_MIN_LEN, MAVLINK_MSG_ID_ACK_TM_LEN, MAVLINK_MSG_ID_ACK_TM_CRC);
#endif
}
#if MAVLINK_MSG_ID_ACK_TM_LEN <= MAVLINK_MAX_PAYLOAD_LEN
/*
This variant of _send() can be used to save stack space by re-using
memory from the receive buffer. The caller provides a
mavlink_message_t which is the size of a full mavlink message. This
is usually the receive buffer for the channel, and allows a reply to an
incoming message with minimum stack space usage.
*/
static inline void mavlink_msg_ack_tm_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint8_t recv_msgid, uint8_t seq_ack)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char *buf = (char *)msgbuf;
_mav_put_uint8_t(buf, 0, recv_msgid);
_mav_put_uint8_t(buf, 1, seq_ack);
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_ACK_TM, buf, MAVLINK_MSG_ID_ACK_TM_MIN_LEN, MAVLINK_MSG_ID_ACK_TM_LEN, MAVLINK_MSG_ID_ACK_TM_CRC);
#else
mavlink_ack_tm_t *packet = (mavlink_ack_tm_t *)msgbuf;
packet->recv_msgid = recv_msgid;
packet->seq_ack = seq_ack;
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_ACK_TM, (const char *)packet, MAVLINK_MSG_ID_ACK_TM_MIN_LEN, MAVLINK_MSG_ID_ACK_TM_LEN, MAVLINK_MSG_ID_ACK_TM_CRC);
#endif
}
#endif
#endif
// MESSAGE ACK_TM UNPACKING
/**
* @brief Get field recv_msgid from ack_tm message
*
* @return Message id of the received message
*/
static inline uint8_t mavlink_msg_ack_tm_get_recv_msgid(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint8_t(msg, 0);
}
/**
* @brief Get field seq_ack from ack_tm message
*
* @return Sequence number of the received message
*/
static inline uint8_t mavlink_msg_ack_tm_get_seq_ack(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint8_t(msg, 1);
}
/**
* @brief Decode a ack_tm message into a struct
*
* @param msg The message to decode
* @param ack_tm C-struct to decode the message contents into
*/
static inline void mavlink_msg_ack_tm_decode(const mavlink_message_t* msg, mavlink_ack_tm_t* ack_tm)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
ack_tm->recv_msgid = mavlink_msg_ack_tm_get_recv_msgid(msg);
ack_tm->seq_ack = mavlink_msg_ack_tm_get_seq_ack(msg);
#else
uint8_t len = msg->len < MAVLINK_MSG_ID_ACK_TM_LEN? msg->len : MAVLINK_MSG_ID_ACK_TM_LEN;
memset(ack_tm, 0, MAVLINK_MSG_ID_ACK_TM_LEN);
memcpy(ack_tm, _MAV_PAYLOAD(msg), len);
#endif
}
mavlink_lib/lyra/mavlink_msg_ada_tm.h 0 → 100644
View file @ 7abedf97
#pragma once
// MESSAGE ADA_TM PACKING
#define MAVLINK_MSG_ID_ADA_TM 205
typedef struct __mavlink_ada_tm_t {
uint64_t timestamp; /*< [us] When was this logged*/
float kalman_x0; /*< Kalman state variable 0 (pressure)*/
float kalman_x1; /*< Kalman state variable 1 (pressure velocity)*/
float kalman_x2; /*< Kalman state variable 2 (pressure acceleration)*/
float vertical_speed; /*< [m/s] Vertical speed computed by the ADA*/
float msl_altitude; /*< [m] Altitude w.r.t. mean sea level*/
float ref_pressure; /*< [Pa] Calibration pressure*/
float ref_altitude; /*< [m] Calibration altitude*/
float ref_temperature; /*< [degC] Calibration temperature*/
float msl_pressure; /*< [Pa] Expected pressure at mean sea level*/
float msl_temperature; /*< [degC] Expected temperature at mean sea level*/
float dpl_altitude; /*< [m] Main parachute deployment altituyde*/
uint8_t state; /*< ADA current state*/
} mavlink_ada_tm_t;
#define MAVLINK_MSG_ID_ADA_TM_LEN 53
#define MAVLINK_MSG_ID_ADA_TM_MIN_LEN 53
#define MAVLINK_MSG_ID_205_LEN 53
#define MAVLINK_MSG_ID_205_MIN_LEN 53
#define MAVLINK_MSG_ID_ADA_TM_CRC 234
#define MAVLINK_MSG_ID_205_CRC 234
#if MAVLINK_COMMAND_24BIT
#define MAVLINK_MESSAGE_INFO_ADA_TM { \
205, \
"ADA_TM", \
13, \
{ { "timestamp", NULL, MAVLINK_TYPE_UINT64_T, 0, 0, offsetof(mavlink_ada_tm_t, timestamp) }, \
{ "state", NULL, MAVLINK_TYPE_UINT8_T, 0, 52, offsetof(mavlink_ada_tm_t, state) }, \
{ "kalman_x0", NULL, MAVLINK_TYPE_FLOAT, 0, 8, offsetof(mavlink_ada_tm_t, kalman_x0) }, \
{ "kalman_x1", NULL, MAVLINK_TYPE_FLOAT, 0, 12, offsetof(mavlink_ada_tm_t, kalman_x1) }, \
{ "kalman_x2", NULL, MAVLINK_TYPE_FLOAT, 0, 16, offsetof(mavlink_ada_tm_t, kalman_x2) }, \
{ "vertical_speed", NULL, MAVLINK_TYPE_FLOAT, 0, 20, offsetof(mavlink_ada_tm_t, vertical_speed) }, \
{ "msl_altitude", NULL, MAVLINK_TYPE_FLOAT, 0, 24, offsetof(mavlink_ada_tm_t, msl_altitude) }, \
{ "ref_pressure", NULL, MAVLINK_TYPE_FLOAT, 0, 28, offsetof(mavlink_ada_tm_t, ref_pressure) }, \
{ "ref_altitude", NULL, MAVLINK_TYPE_FLOAT, 0, 32, offsetof(mavlink_ada_tm_t, ref_altitude) }, \
{ "ref_temperature", NULL, MAVLINK_TYPE_FLOAT, 0, 36, offsetof(mavlink_ada_tm_t, ref_temperature) }, \
{ "msl_pressure", NULL, MAVLINK_TYPE_FLOAT, 0, 40, offsetof(mavlink_ada_tm_t, msl_pressure) }, \
{ "msl_temperature", NULL, MAVLINK_TYPE_FLOAT, 0, 44, offsetof(mavlink_ada_tm_t, msl_temperature) }, \
{ "dpl_altitude", NULL, MAVLINK_TYPE_FLOAT, 0, 48, offsetof(mavlink_ada_tm_t, dpl_altitude) }, \
} \
}
#else
#define MAVLINK_MESSAGE_INFO_ADA_TM { \
"ADA_TM", \
13, \
{ { "timestamp", NULL, MAVLINK_TYPE_UINT64_T, 0, 0, offsetof(mavlink_ada_tm_t, timestamp) }, \
{ "state", NULL, MAVLINK_TYPE_UINT8_T, 0, 52, offsetof(mavlink_ada_tm_t, state) }, \
{ "kalman_x0", NULL, MAVLINK_TYPE_FLOAT, 0, 8, offsetof(mavlink_ada_tm_t, kalman_x0) }, \
{ "kalman_x1", NULL, MAVLINK_TYPE_FLOAT, 0, 12, offsetof(mavlink_ada_tm_t, kalman_x1) }, \
{ "kalman_x2", NULL, MAVLINK_TYPE_FLOAT, 0, 16, offsetof(mavlink_ada_tm_t, kalman_x2) }, \
{ "vertical_speed", NULL, MAVLINK_TYPE_FLOAT, 0, 20, offsetof(mavlink_ada_tm_t, vertical_speed) }, \
{ "msl_altitude", NULL, MAVLINK_TYPE_FLOAT, 0, 24, offsetof(mavlink_ada_tm_t, msl_altitude) }, \
{ "ref_pressure", NULL, MAVLINK_TYPE_FLOAT, 0, 28, offsetof(mavlink_ada_tm_t, ref_pressure) }, \
{ "ref_altitude", NULL, MAVLINK_TYPE_FLOAT, 0, 32, offsetof(mavlink_ada_tm_t, ref_altitude) }, \
{ "ref_temperature", NULL, MAVLINK_TYPE_FLOAT, 0, 36, offsetof(mavlink_ada_tm_t, ref_temperature) }, \
{ "msl_pressure", NULL, MAVLINK_TYPE_FLOAT, 0, 40, offsetof(mavlink_ada_tm_t, msl_pressure) }, \
{ "msl_temperature", NULL, MAVLINK_TYPE_FLOAT, 0, 44, offsetof(mavlink_ada_tm_t, msl_temperature) }, \
{ "dpl_altitude", NULL, MAVLINK_TYPE_FLOAT, 0, 48, offsetof(mavlink_ada_tm_t, dpl_altitude) }, \
} \
}
#endif
/**
* @brief Pack a ada_tm message
* @param system_id ID of this system
* @param component_id ID of this component (e.g. 200 for IMU)
* @param msg The MAVLink message to compress the data into
*
* @param timestamp [us] When was this logged
* @param state ADA current state
* @param kalman_x0 Kalman state variable 0 (pressure)
* @param kalman_x1 Kalman state variable 1 (pressure velocity)
* @param kalman_x2 Kalman state variable 2 (pressure acceleration)
* @param vertical_speed [m/s] Vertical speed computed by the ADA
* @param msl_altitude [m] Altitude w.r.t. mean sea level
* @param ref_pressure [Pa] Calibration pressure
* @param ref_altitude [m] Calibration altitude
* @param ref_temperature [degC] Calibration temperature
* @param msl_pressure [Pa] Expected pressure at mean sea level
* @param msl_temperature [degC] Expected temperature at mean sea level
* @param dpl_altitude [m] Main parachute deployment altituyde
* @return length of the message in bytes (excluding serial stream start sign)
*/
static inline uint16_t mavlink_msg_ada_tm_pack(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg,
uint64_t timestamp, uint8_t state, float kalman_x0, float kalman_x1, float kalman_x2, float vertical_speed, float msl_altitude, float ref_pressure, float ref_altitude, float ref_temperature, float msl_pressure, float msl_temperature, float dpl_altitude)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char buf[MAVLINK_MSG_ID_ADA_TM_LEN];
_mav_put_uint64_t(buf, 0, timestamp);
_mav_put_float(buf, 8, kalman_x0);
_mav_put_float(buf, 12, kalman_x1);
_mav_put_float(buf, 16, kalman_x2);
_mav_put_float(buf, 20, vertical_speed);
_mav_put_float(buf, 24, msl_altitude);
_mav_put_float(buf, 28, ref_pressure);
_mav_put_float(buf, 32, ref_altitude);
_mav_put_float(buf, 36, ref_temperature);
_mav_put_float(buf, 40, msl_pressure);
_mav_put_float(buf, 44, msl_temperature);
_mav_put_float(buf, 48, dpl_altitude);
_mav_put_uint8_t(buf, 52, state);
memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_ADA_TM_LEN);
#else
mavlink_ada_tm_t packet;
packet.timestamp = timestamp;
packet.kalman_x0 = kalman_x0;
packet.kalman_x1 = kalman_x1;
packet.kalman_x2 = kalman_x2;
packet.vertical_speed = vertical_speed;
packet.msl_altitude = msl_altitude;
packet.ref_pressure = ref_pressure;
packet.ref_altitude = ref_altitude;
packet.ref_temperature = ref_temperature;
packet.msl_pressure = msl_pressure;
packet.msl_temperature = msl_temperature;
packet.dpl_altitude = dpl_altitude;
packet.state = state;
memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_ADA_TM_LEN);
#endif
msg->msgid = MAVLINK_MSG_ID_ADA_TM;
return mavlink_finalize_message(msg, system_id, component_id, MAVLINK_MSG_ID_ADA_TM_MIN_LEN, MAVLINK_MSG_ID_ADA_TM_LEN, MAVLINK_MSG_ID_ADA_TM_CRC);
}
/**
* @brief Pack a ada_tm message on a channel
* @param system_id ID of this system
* @param component_id ID of this component (e.g. 200 for IMU)
* @param chan The MAVLink channel this message will be sent over
* @param msg The MAVLink message to compress the data into
* @param timestamp [us] When was this logged
* @param state ADA current state
* @param kalman_x0 Kalman state variable 0 (pressure)
* @param kalman_x1 Kalman state variable 1 (pressure velocity)
* @param kalman_x2 Kalman state variable 2 (pressure acceleration)
* @param vertical_speed [m/s] Vertical speed computed by the ADA
* @param msl_altitude [m] Altitude w.r.t. mean sea level
* @param ref_pressure [Pa] Calibration pressure
* @param ref_altitude [m] Calibration altitude
* @param ref_temperature [degC] Calibration temperature
* @param msl_pressure [Pa] Expected pressure at mean sea level
* @param msl_temperature [degC] Expected temperature at mean sea level
* @param dpl_altitude [m] Main parachute deployment altituyde
* @return length of the message in bytes (excluding serial stream start sign)
*/
static inline uint16_t mavlink_msg_ada_tm_pack_chan(uint8_t system_id, uint8_t component_id, uint8_t chan,
mavlink_message_t* msg,
uint64_t timestamp,uint8_t state,float kalman_x0,float kalman_x1,float kalman_x2,float vertical_speed,float msl_altitude,float ref_pressure,float ref_altitude,float ref_temperature,float msl_pressure,float msl_temperature,float dpl_altitude)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char buf[MAVLINK_MSG_ID_ADA_TM_LEN];
_mav_put_uint64_t(buf, 0, timestamp);
_mav_put_float(buf, 8, kalman_x0);
_mav_put_float(buf, 12, kalman_x1);
_mav_put_float(buf, 16, kalman_x2);
_mav_put_float(buf, 20, vertical_speed);
_mav_put_float(buf, 24, msl_altitude);
_mav_put_float(buf, 28, ref_pressure);
_mav_put_float(buf, 32, ref_altitude);
_mav_put_float(buf, 36, ref_temperature);
_mav_put_float(buf, 40, msl_pressure);
_mav_put_float(buf, 44, msl_temperature);
_mav_put_float(buf, 48, dpl_altitude);
_mav_put_uint8_t(buf, 52, state);
memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_ADA_TM_LEN);
#else
mavlink_ada_tm_t packet;
packet.timestamp = timestamp;
packet.kalman_x0 = kalman_x0;
packet.kalman_x1 = kalman_x1;
packet.kalman_x2 = kalman_x2;
packet.vertical_speed = vertical_speed;
packet.msl_altitude = msl_altitude;
packet.ref_pressure = ref_pressure;
packet.ref_altitude = ref_altitude;
packet.ref_temperature = ref_temperature;
packet.msl_pressure = msl_pressure;
packet.msl_temperature = msl_temperature;
packet.dpl_altitude = dpl_altitude;
packet.state = state;
memcpy(_MAV_PAYLOAD_NON_CONST(msg), &packet, MAVLINK_MSG_ID_ADA_TM_LEN);
#endif
msg->msgid = MAVLINK_MSG_ID_ADA_TM;
return mavlink_finalize_message_chan(msg, system_id, component_id, chan, MAVLINK_MSG_ID_ADA_TM_MIN_LEN, MAVLINK_MSG_ID_ADA_TM_LEN, MAVLINK_MSG_ID_ADA_TM_CRC);
}
/**
* @brief Encode a ada_tm struct
*
* @param system_id ID of this system
* @param component_id ID of this component (e.g. 200 for IMU)
* @param msg The MAVLink message to compress the data into
* @param ada_tm C-struct to read the message contents from
*/
static inline uint16_t mavlink_msg_ada_tm_encode(uint8_t system_id, uint8_t component_id, mavlink_message_t* msg, const mavlink_ada_tm_t* ada_tm)
{
return mavlink_msg_ada_tm_pack(system_id, component_id, msg, ada_tm->timestamp, ada_tm->state, ada_tm->kalman_x0, ada_tm->kalman_x1, ada_tm->kalman_x2, ada_tm->vertical_speed, ada_tm->msl_altitude, ada_tm->ref_pressure, ada_tm->ref_altitude, ada_tm->ref_temperature, ada_tm->msl_pressure, ada_tm->msl_temperature, ada_tm->dpl_altitude);
}
/**
* @brief Encode a ada_tm struct on a channel
*
* @param system_id ID of this system
* @param component_id ID of this component (e.g. 200 for IMU)
* @param chan The MAVLink channel this message will be sent over
* @param msg The MAVLink message to compress the data into
* @param ada_tm C-struct to read the message contents from
*/
static inline uint16_t mavlink_msg_ada_tm_encode_chan(uint8_t system_id, uint8_t component_id, uint8_t chan, mavlink_message_t* msg, const mavlink_ada_tm_t* ada_tm)
{
return mavlink_msg_ada_tm_pack_chan(system_id, component_id, chan, msg, ada_tm->timestamp, ada_tm->state, ada_tm->kalman_x0, ada_tm->kalman_x1, ada_tm->kalman_x2, ada_tm->vertical_speed, ada_tm->msl_altitude, ada_tm->ref_pressure, ada_tm->ref_altitude, ada_tm->ref_temperature, ada_tm->msl_pressure, ada_tm->msl_temperature, ada_tm->dpl_altitude);
}
/**
* @brief Send a ada_tm message
* @param chan MAVLink channel to send the message
*
* @param timestamp [us] When was this logged
* @param state ADA current state
* @param kalman_x0 Kalman state variable 0 (pressure)
* @param kalman_x1 Kalman state variable 1 (pressure velocity)
* @param kalman_x2 Kalman state variable 2 (pressure acceleration)
* @param vertical_speed [m/s] Vertical speed computed by the ADA
* @param msl_altitude [m] Altitude w.r.t. mean sea level
* @param ref_pressure [Pa] Calibration pressure
* @param ref_altitude [m] Calibration altitude
* @param ref_temperature [degC] Calibration temperature
* @param msl_pressure [Pa] Expected pressure at mean sea level
* @param msl_temperature [degC] Expected temperature at mean sea level
* @param dpl_altitude [m] Main parachute deployment altituyde
*/
#ifdef MAVLINK_USE_CONVENIENCE_FUNCTIONS
static inline void mavlink_msg_ada_tm_send(mavlink_channel_t chan, uint64_t timestamp, uint8_t state, float kalman_x0, float kalman_x1, float kalman_x2, float vertical_speed, float msl_altitude, float ref_pressure, float ref_altitude, float ref_temperature, float msl_pressure, float msl_temperature, float dpl_altitude)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char buf[MAVLINK_MSG_ID_ADA_TM_LEN];
_mav_put_uint64_t(buf, 0, timestamp);
_mav_put_float(buf, 8, kalman_x0);
_mav_put_float(buf, 12, kalman_x1);
_mav_put_float(buf, 16, kalman_x2);
_mav_put_float(buf, 20, vertical_speed);
_mav_put_float(buf, 24, msl_altitude);
_mav_put_float(buf, 28, ref_pressure);
_mav_put_float(buf, 32, ref_altitude);
_mav_put_float(buf, 36, ref_temperature);
_mav_put_float(buf, 40, msl_pressure);
_mav_put_float(buf, 44, msl_temperature);
_mav_put_float(buf, 48, dpl_altitude);
_mav_put_uint8_t(buf, 52, state);
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_ADA_TM, buf, MAVLINK_MSG_ID_ADA_TM_MIN_LEN, MAVLINK_MSG_ID_ADA_TM_LEN, MAVLINK_MSG_ID_ADA_TM_CRC);
#else
mavlink_ada_tm_t packet;
packet.timestamp = timestamp;
packet.kalman_x0 = kalman_x0;
packet.kalman_x1 = kalman_x1;
packet.kalman_x2 = kalman_x2;
packet.vertical_speed = vertical_speed;
packet.msl_altitude = msl_altitude;
packet.ref_pressure = ref_pressure;
packet.ref_altitude = ref_altitude;
packet.ref_temperature = ref_temperature;
packet.msl_pressure = msl_pressure;
packet.msl_temperature = msl_temperature;
packet.dpl_altitude = dpl_altitude;
packet.state = state;
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_ADA_TM, (const char *)&packet, MAVLINK_MSG_ID_ADA_TM_MIN_LEN, MAVLINK_MSG_ID_ADA_TM_LEN, MAVLINK_MSG_ID_ADA_TM_CRC);
#endif
}
/**
* @brief Send a ada_tm message
* @param chan MAVLink channel to send the message
* @param struct The MAVLink struct to serialize
*/
static inline void mavlink_msg_ada_tm_send_struct(mavlink_channel_t chan, const mavlink_ada_tm_t* ada_tm)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
mavlink_msg_ada_tm_send(chan, ada_tm->timestamp, ada_tm->state, ada_tm->kalman_x0, ada_tm->kalman_x1, ada_tm->kalman_x2, ada_tm->vertical_speed, ada_tm->msl_altitude, ada_tm->ref_pressure, ada_tm->ref_altitude, ada_tm->ref_temperature, ada_tm->msl_pressure, ada_tm->msl_temperature, ada_tm->dpl_altitude);
#else
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_ADA_TM, (const char *)ada_tm, MAVLINK_MSG_ID_ADA_TM_MIN_LEN, MAVLINK_MSG_ID_ADA_TM_LEN, MAVLINK_MSG_ID_ADA_TM_CRC);
#endif
}
#if MAVLINK_MSG_ID_ADA_TM_LEN <= MAVLINK_MAX_PAYLOAD_LEN
/*
This variant of _send() can be used to save stack space by re-using
memory from the receive buffer. The caller provides a
mavlink_message_t which is the size of a full mavlink message. This
is usually the receive buffer for the channel, and allows a reply to an
incoming message with minimum stack space usage.
*/
static inline void mavlink_msg_ada_tm_send_buf(mavlink_message_t *msgbuf, mavlink_channel_t chan, uint64_t timestamp, uint8_t state, float kalman_x0, float kalman_x1, float kalman_x2, float vertical_speed, float msl_altitude, float ref_pressure, float ref_altitude, float ref_temperature, float msl_pressure, float msl_temperature, float dpl_altitude)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char *buf = (char *)msgbuf;
_mav_put_uint64_t(buf, 0, timestamp);
_mav_put_float(buf, 8, kalman_x0);
_mav_put_float(buf, 12, kalman_x1);
_mav_put_float(buf, 16, kalman_x2);
_mav_put_float(buf, 20, vertical_speed);
_mav_put_float(buf, 24, msl_altitude);
_mav_put_float(buf, 28, ref_pressure);
_mav_put_float(buf, 32, ref_altitude);
_mav_put_float(buf, 36, ref_temperature);
_mav_put_float(buf, 40, msl_pressure);
_mav_put_float(buf, 44, msl_temperature);
_mav_put_float(buf, 48, dpl_altitude);
_mav_put_uint8_t(buf, 52, state);
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_ADA_TM, buf, MAVLINK_MSG_ID_ADA_TM_MIN_LEN, MAVLINK_MSG_ID_ADA_TM_LEN, MAVLINK_MSG_ID_ADA_TM_CRC);
#else
mavlink_ada_tm_t *packet = (mavlink_ada_tm_t *)msgbuf;
packet->timestamp = timestamp;
packet->kalman_x0 = kalman_x0;
packet->kalman_x1 = kalman_x1;
packet->kalman_x2 = kalman_x2;
packet->vertical_speed = vertical_speed;
packet->msl_altitude = msl_altitude;
packet->ref_pressure = ref_pressure;
packet->ref_altitude = ref_altitude;
packet->ref_temperature = ref_temperature;
packet->msl_pressure = msl_pressure;
packet->msl_temperature = msl_temperature;
packet->dpl_altitude = dpl_altitude;
packet->state = state;
_mav_finalize_message_chan_send(chan, MAVLINK_MSG_ID_ADA_TM, (const char *)packet, MAVLINK_MSG_ID_ADA_TM_MIN_LEN, MAVLINK_MSG_ID_ADA_TM_LEN, MAVLINK_MSG_ID_ADA_TM_CRC);
#endif
}
#endif
#endif
// MESSAGE ADA_TM UNPACKING
/**
* @brief Get field timestamp from ada_tm message
*
* @return [us] When was this logged
*/
static inline uint64_t mavlink_msg_ada_tm_get_timestamp(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint64_t(msg, 0);
}
/**
* @brief Get field state from ada_tm message
*
* @return ADA current state
*/
static inline uint8_t mavlink_msg_ada_tm_get_state(const mavlink_message_t* msg)
{
return _MAV_RETURN_uint8_t(msg, 52);
}
/**
* @brief Get field kalman_x0 from ada_tm message
*
* @return Kalman state variable 0 (pressure)
*/
static inline float mavlink_msg_ada_tm_get_kalman_x0(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 8);
}
/**
* @brief Get field kalman_x1 from ada_tm message
*
* @return Kalman state variable 1 (pressure velocity)
*/
static inline float mavlink_msg_ada_tm_get_kalman_x1(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 12);
}
/**
* @brief Get field kalman_x2 from ada_tm message
*
* @return Kalman state variable 2 (pressure acceleration)
*/
static inline float mavlink_msg_ada_tm_get_kalman_x2(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 16);
}
/**
* @brief Get field vertical_speed from ada_tm message
*
* @return [m/s] Vertical speed computed by the ADA
*/
static inline float mavlink_msg_ada_tm_get_vertical_speed(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 20);
}
/**
* @brief Get field msl_altitude from ada_tm message
*
* @return [m] Altitude w.r.t. mean sea level
*/
static inline float mavlink_msg_ada_tm_get_msl_altitude(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 24);
}
/**
* @brief Get field ref_pressure from ada_tm message
*
* @return [Pa] Calibration pressure
*/
static inline float mavlink_msg_ada_tm_get_ref_pressure(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 28);
}
/**
* @brief Get field ref_altitude from ada_tm message
*
* @return [m] Calibration altitude
*/
static inline float mavlink_msg_ada_tm_get_ref_altitude(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 32);
}
/**
* @brief Get field ref_temperature from ada_tm message
*
* @return [degC] Calibration temperature
*/
static inline float mavlink_msg_ada_tm_get_ref_temperature(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 36);
}
/**
* @brief Get field msl_pressure from ada_tm message
*
* @return [Pa] Expected pressure at mean sea level
*/
static inline float mavlink_msg_ada_tm_get_msl_pressure(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 40);
}
/**
* @brief Get field msl_temperature from ada_tm message
*
* @return [degC] Expected temperature at mean sea level
*/
static inline float mavlink_msg_ada_tm_get_msl_temperature(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 44);
}
/**
* @brief Get field dpl_altitude from ada_tm message
*
* @return [m] Main parachute deployment altituyde
*/
static inline float mavlink_msg_ada_tm_get_dpl_altitude(const mavlink_message_t* msg)
{
return _MAV_RETURN_float(msg, 48);
}
/**
* @brief Decode a ada_tm message into a struct
*
* @param msg The message to decode
* @param ada_tm C-struct to decode the message contents into
*/
static inline void mavlink_msg_ada_tm_decode(const mavlink_message_t* msg, mavlink_ada_tm_t* ada_tm)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
ada_tm->timestamp = mavlink_msg_ada_tm_get_timestamp(msg);
ada_tm->kalman_x0 = mavlink_msg_ada_tm_get_kalman_x0(msg);
ada_tm->kalman_x1 = mavlink_msg_ada_tm_get_kalman_x1(msg);
ada_tm->kalman_x2 = mavlink_msg_ada_tm_get_kalman_x2(msg);
ada_tm->vertical_speed = mavlink_msg_ada_tm_get_vertical_speed(msg);
ada_tm->msl_altitude = mavlink_msg_ada_tm_get_msl_altitude(msg);
ada_tm->ref_pressure = mavlink_msg_ada_tm_get_ref_pressure(msg);
ada_tm->ref_altitude = mavlink_msg_ada_tm_get_ref_altitude(msg);
ada_tm->ref_temperature = mavlink_msg_ada_tm_get_ref_temperature(msg);
ada_tm->msl_pressure = mavlink_msg_ada_tm_get_msl_pressure(msg);
ada_tm->msl_temperature = mavlink_msg_ada_tm_get_msl_temperature(msg);
ada_tm->dpl_altitude = mavlink_msg_ada_tm_get_dpl_altitude(msg);
ada_tm->state = mavlink_msg_ada_tm_get_state(msg);
#else
uint8_t len = msg->len < MAVLINK_MSG_ID_ADA_TM_LEN? msg->len : MAVLINK_MSG_ID_ADA_TM_LEN;
memset(ada_tm, 0, MAVLINK_MSG_ID_ADA_TM_LEN);
memcpy(ada_tm, _MAV_PAYLOAD(msg), len);
#endif
}