diff --git a/mavlink_lib.py b/mavlink_lib.py
index 1494d9eafe9423a09fcd065a625c214476e0a138..3881bf5e6b54804dda41ade9f485ff902f7d55cc 100644
--- a/mavlink_lib.py
+++ b/mavlink_lib.py
@@ -266,6 +266,17 @@ class EnumEntry(object):
enums = {}
+# SysIDs
+enums['SysIDs'] = {}
+MAIN = 1 #
+enums['SysIDs'][1] = EnumEntry('MAIN', '''''')
+PAYLOAD = 2 #
+enums['SysIDs'][2] = EnumEntry('PAYLOAD', '''''')
+RIG = 3 #
+enums['SysIDs'][3] = EnumEntry('RIG', '''''')
+SysIDs_ENUM_END = 4 #
+enums['SysIDs'][4] = EnumEntry('SysIDs_ENUM_END', '''''')
+
# SystemTMList
enums['SystemTMList'] = {}
MAV_SYS_ID = 1 # State of init results about system hardware/software components
@@ -285,20 +296,20 @@ MAV_ADA_ID = 7 # ADA Status
enums['SystemTMList'][7] = EnumEntry('MAV_ADA_ID', '''ADA Status''')
MAV_NAS_ID = 8 # NavigationSystem data
enums['SystemTMList'][8] = EnumEntry('MAV_NAS_ID', '''NavigationSystem data''')
-MAV_CAN_ID = 9 # Canbus stats
-enums['SystemTMList'][9] = EnumEntry('MAV_CAN_ID', '''Canbus stats''')
-MAV_FLIGHT_ID = 10 # Flight telemetry
-enums['SystemTMList'][10] = EnumEntry('MAV_FLIGHT_ID', '''Flight telemetry''')
-MAV_STATS_ID = 11 # Satistics telemetry
-enums['SystemTMList'][11] = EnumEntry('MAV_STATS_ID', '''Satistics telemetry''')
-MAV_SENSORS_STATE_ID = 12 # Sensors init state telemetry
-enums['SystemTMList'][12] = EnumEntry('MAV_SENSORS_STATE_ID', '''Sensors init state telemetry''')
-MAV_GSE_ID = 13 # Ground Segnement Equipment
-enums['SystemTMList'][13] = EnumEntry('MAV_GSE_ID', '''Ground Segnement Equipment''')
-MAV_MOTOR_ID = 14 # Rocket Motor data
-enums['SystemTMList'][14] = EnumEntry('MAV_MOTOR_ID', '''Rocket Motor data''')
-MAV_TARS_ID = 15 # TARS data
-enums['SystemTMList'][15] = EnumEntry('MAV_TARS_ID', '''TARS data''')
+MAV_MEA_ID = 9 # MEA Status
+enums['SystemTMList'][9] = EnumEntry('MAV_MEA_ID', '''MEA Status''')
+MAV_CAN_ID = 10 # Canbus stats
+enums['SystemTMList'][10] = EnumEntry('MAV_CAN_ID', '''Canbus stats''')
+MAV_FLIGHT_ID = 11 # Flight telemetry
+enums['SystemTMList'][11] = EnumEntry('MAV_FLIGHT_ID', '''Flight telemetry''')
+MAV_STATS_ID = 12 # Satistics telemetry
+enums['SystemTMList'][12] = EnumEntry('MAV_STATS_ID', '''Satistics telemetry''')
+MAV_SENSORS_STATE_ID = 13 # Sensors init state telemetry
+enums['SystemTMList'][13] = EnumEntry('MAV_SENSORS_STATE_ID', '''Sensors init state telemetry''')
+MAV_GSE_ID = 14 # Ground Segnement Equipment
+enums['SystemTMList'][14] = EnumEntry('MAV_GSE_ID', '''Ground Segnement Equipment''')
+MAV_MOTOR_ID = 15 # Rocket Motor data
+enums['SystemTMList'][15] = EnumEntry('MAV_MOTOR_ID', '''Rocket Motor data''')
SystemTMList_ENUM_END = 16 #
enums['SystemTMList'][16] = EnumEntry('SystemTMList_ENUM_END', '''''')
@@ -483,6 +494,7 @@ MAVLINK_MSG_ID_MAVLINK_STATS_TM = 203
MAVLINK_MSG_ID_TASK_STATS_TM = 204
MAVLINK_MSG_ID_ADA_TM = 205
MAVLINK_MSG_ID_NAS_TM = 206
+MAVLINK_MSG_ID_MEA_TM = 207
MAVLINK_MSG_ID_ROCKET_FLIGHT_TM = 208
MAVLINK_MSG_ID_PAYLOAD_FLIGHT_TM = 209
MAVLINK_MSG_ID_ROCKET_STATS_TM = 210
@@ -1992,29 +2004,67 @@ class MAVLink_nas_tm_message(MAVLink_message):
def pack(self, mav, force_mavlink1=False):
return MAVLink_message.pack(self, mav, 66, struct.pack('<QfffffffffffffffffB', self.timestamp, self.nas_n, self.nas_e, self.nas_d, self.nas_vn, self.nas_ve, self.nas_vd, self.nas_qx, self.nas_qy, self.nas_qz, self.nas_qw, self.nas_bias_x, self.nas_bias_y, self.nas_bias_z, self.ref_pressure, self.ref_temperature, self.ref_latitude, self.ref_longitude, self.state), force_mavlink1=force_mavlink1)
+class MAVLink_mea_tm_message(MAVLink_message):
+ '''
+ Mass Estimation Algorithm status telemetry
+ '''
+ id = MAVLINK_MSG_ID_MEA_TM
+ name = 'MEA_TM'
+ fieldnames = ['timestamp', 'state', 'kalman_x0', 'kalman_x1', 'kalman_x2', 'mass', 'corrected_pressure']
+ ordered_fieldnames = ['timestamp', 'kalman_x0', 'kalman_x1', 'kalman_x2', 'mass', 'corrected_pressure', 'state']
+ fieldtypes = ['uint64_t', 'uint8_t', 'float', 'float', 'float', 'float', 'float']
+ fielddisplays_by_name = {}
+ fieldenums_by_name = {}
+ fieldunits_by_name = {"timestamp": "us", "mass": "kg", "corrected_pressure": "kg"}
+ format = '<QfffffB'
+ native_format = bytearray('<QfffffB', 'ascii')
+ orders = [0, 6, 1, 2, 3, 4, 5]
+ lengths = [1, 1, 1, 1, 1, 1, 1]
+ array_lengths = [0, 0, 0, 0, 0, 0, 0]
+ crc_extra = 11
+ unpacker = struct.Struct('<QfffffB')
+ instance_field = None
+ instance_offset = -1
+
+ def __init__(self, timestamp, state, kalman_x0, kalman_x1, kalman_x2, mass, corrected_pressure):
+ MAVLink_message.__init__(self, MAVLink_mea_tm_message.id, MAVLink_mea_tm_message.name)
+ self._fieldnames = MAVLink_mea_tm_message.fieldnames
+ self._instance_field = MAVLink_mea_tm_message.instance_field
+ self._instance_offset = MAVLink_mea_tm_message.instance_offset
+ self.timestamp = timestamp
+ self.state = state
+ self.kalman_x0 = kalman_x0
+ self.kalman_x1 = kalman_x1
+ self.kalman_x2 = kalman_x2
+ self.mass = mass
+ self.corrected_pressure = corrected_pressure
+
+ def pack(self, mav, force_mavlink1=False):
+ return MAVLink_message.pack(self, mav, 11, struct.pack('<QfffffB', self.timestamp, self.kalman_x0, self.kalman_x1, self.kalman_x2, self.mass, self.corrected_pressure, self.state), force_mavlink1=force_mavlink1)
+
class MAVLink_rocket_flight_tm_message(MAVLink_message):
'''
High Rate Telemetry
'''
id = MAVLINK_MSG_ID_ROCKET_FLIGHT_TM
name = 'ROCKET_FLIGHT_TM'
- fieldnames = ['timestamp', 'ada_state', 'fmm_state', 'dpl_state', 'abk_state', 'nas_state', 'pressure_ada', 'pressure_digi', 'pressure_static', 'pressure_dpl', 'airspeed_pitot', 'altitude_agl', 'ada_vert_speed', 'acc_x', 'acc_y', 'acc_z', 'gyro_x', 'gyro_y', 'gyro_z', 'mag_x', 'mag_y', 'mag_z', 'gps_fix', 'gps_lat', 'gps_lon', 'gps_alt', 'abk_angle', 'abk_estimated_cd', 'parachute_load', 'nas_n', 'nas_e', 'nas_d', 'nas_vn', 'nas_ve', 'nas_vd', 'nas_qx', 'nas_qy', 'nas_qz', 'nas_qw', 'nas_bias_x', 'nas_bias_y', 'nas_bias_z', 'pin_launch', 'pin_nosecone', 'pin_expulsion', 'cutter_presence', 'estimated_thrust', 'vbat', 'temperature', 'logger_error']
- ordered_fieldnames = ['timestamp', 'pressure_ada', 'pressure_digi', 'pressure_static', 'pressure_dpl', 'airspeed_pitot', 'altitude_agl', 'ada_vert_speed', 'acc_x', 'acc_y', 'acc_z', 'gyro_x', 'gyro_y', 'gyro_z', 'mag_x', 'mag_y', 'mag_z', 'gps_lat', 'gps_lon', 'gps_alt', 'abk_angle', 'abk_estimated_cd', 'parachute_load', 'nas_n', 'nas_e', 'nas_d', 'nas_vn', 'nas_ve', 'nas_vd', 'nas_qx', 'nas_qy', 'nas_qz', 'nas_qw', 'nas_bias_x', 'nas_bias_y', 'nas_bias_z', 'estimated_thrust', 'vbat', 'temperature', 'ada_state', 'fmm_state', 'dpl_state', 'abk_state', 'nas_state', 'gps_fix', 'pin_launch', 'pin_nosecone', 'pin_expulsion', 'cutter_presence', 'logger_error']
- fieldtypes = ['uint64_t', 'uint8_t', 'uint8_t', 'uint8_t', 'uint8_t', 'uint8_t', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'uint8_t', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'uint8_t', 'uint8_t', 'uint8_t', 'uint8_t', 'float', 'float', 'float', 'int8_t']
+ fieldnames = ['timestamp', 'ada_state', 'fmm_state', 'dpl_state', 'abk_state', 'nas_state', 'mea_state', 'pressure_ada', 'pressure_digi', 'pressure_static', 'pressure_dpl', 'airspeed_pitot', 'altitude_agl', 'ada_vert_speed', 'mea_mass', 'acc_x', 'acc_y', 'acc_z', 'gyro_x', 'gyro_y', 'gyro_z', 'mag_x', 'mag_y', 'mag_z', 'gps_fix', 'gps_lat', 'gps_lon', 'gps_alt', 'abk_angle', 'nas_n', 'nas_e', 'nas_d', 'nas_vn', 'nas_ve', 'nas_vd', 'nas_qx', 'nas_qy', 'nas_qz', 'nas_qw', 'nas_bias_x', 'nas_bias_y', 'nas_bias_z', 'pin_launch', 'pin_nosecone', 'pin_expulsion', 'cutter_presence', 'battery_voltage', 'current_consumption', 'temperature', 'logger_error']
+ ordered_fieldnames = ['timestamp', 'pressure_ada', 'pressure_digi', 'pressure_static', 'pressure_dpl', 'airspeed_pitot', 'altitude_agl', 'ada_vert_speed', 'mea_mass', 'acc_x', 'acc_y', 'acc_z', 'gyro_x', 'gyro_y', 'gyro_z', 'mag_x', 'mag_y', 'mag_z', 'gps_lat', 'gps_lon', 'gps_alt', 'abk_angle', 'nas_n', 'nas_e', 'nas_d', 'nas_vn', 'nas_ve', 'nas_vd', 'nas_qx', 'nas_qy', 'nas_qz', 'nas_qw', 'nas_bias_x', 'nas_bias_y', 'nas_bias_z', 'battery_voltage', 'current_consumption', 'temperature', 'ada_state', 'fmm_state', 'dpl_state', 'abk_state', 'nas_state', 'mea_state', 'gps_fix', 'pin_launch', 'pin_nosecone', 'pin_expulsion', 'cutter_presence', 'logger_error']
+ fieldtypes = ['uint64_t', 'uint8_t', 'uint8_t', 'uint8_t', 'uint8_t', 'uint8_t', 'uint8_t', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'uint8_t', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'uint8_t', 'uint8_t', 'uint8_t', 'uint8_t', 'float', 'float', 'float', 'int8_t']
fielddisplays_by_name = {}
fieldenums_by_name = {}
- fieldunits_by_name = {"timestamp": "us", "pressure_ada": "Pa", "pressure_digi": "Pa", "pressure_static": "Pa", "pressure_dpl": "Pa", "airspeed_pitot": "m/s", "altitude_agl": "m", "ada_vert_speed": "m/s", "acc_x": "m/s^2", "acc_y": "m/s^2", "acc_z": "m/s^2", "gyro_x": "rad/s", "gyro_y": "rad/s", "gyro_z": "rad/s", "mag_x": "uT", "mag_y": "uT", "mag_z": "uT", "gps_lat": "deg", "gps_lon": "deg", "gps_alt": "m", "abk_angle": "deg", "nas_n": "deg", "nas_e": "deg", "nas_d": "m", "nas_vn": "m/s", "nas_ve": "m/s", "nas_vd": "m/s", "nas_qx": "deg", "nas_qy": "deg", "nas_qz": "deg", "nas_qw": "deg", "vbat": "V", "temperature": "degC"}
- format = '<QffffffffffffffffffffffffffffffffffffffBBBBBBBBBBb'
- native_format = bytearray('<QffffffffffffffffffffffffffffffffffffffBBBBBBBBBBb', 'ascii')
- orders = [0, 39, 40, 41, 42, 43, 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 44, 17, 18, 19, 20, 21, 22, 23, 24, 25, 26, 27, 28, 29, 30, 31, 32, 33, 34, 35, 45, 46, 47, 48, 36, 37, 38, 49]
+ fieldunits_by_name = {"timestamp": "us", "pressure_ada": "Pa", "pressure_digi": "Pa", "pressure_static": "Pa", "pressure_dpl": "Pa", "airspeed_pitot": "m/s", "altitude_agl": "m", "ada_vert_speed": "m/s", "mea_mass": "kg", "acc_x": "m/s^2", "acc_y": "m/s^2", "acc_z": "m/s^2", "gyro_x": "rad/s", "gyro_y": "rad/s", "gyro_z": "rad/s", "mag_x": "uT", "mag_y": "uT", "mag_z": "uT", "gps_lat": "deg", "gps_lon": "deg", "gps_alt": "m", "abk_angle": "deg", "nas_n": "deg", "nas_e": "deg", "nas_d": "m", "nas_vn": "m/s", "nas_ve": "m/s", "nas_vd": "m/s", "nas_qx": "deg", "nas_qy": "deg", "nas_qz": "deg", "nas_qw": "deg", "battery_voltage": "V", "current_consumption": "A", "temperature": "degC"}
+ format = '<QfffffffffffffffffffffffffffffffffffffBBBBBBBBBBBb'
+ native_format = bytearray('<QfffffffffffffffffffffffffffffffffffffBBBBBBBBBBBb', 'ascii')
+ orders = [0, 38, 39, 40, 41, 42, 43, 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17, 44, 18, 19, 20, 21, 22, 23, 24, 25, 26, 27, 28, 29, 30, 31, 32, 33, 34, 45, 46, 47, 48, 35, 36, 37, 49]
lengths = [1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1]
array_lengths = [0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0]
- crc_extra = 141
- unpacker = struct.Struct('<QffffffffffffffffffffffffffffffffffffffBBBBBBBBBBb')
+ crc_extra = 254
+ unpacker = struct.Struct('<QfffffffffffffffffffffffffffffffffffffBBBBBBBBBBBb')
instance_field = None
instance_offset = -1
- def __init__(self, timestamp, ada_state, fmm_state, dpl_state, abk_state, nas_state, pressure_ada, pressure_digi, pressure_static, pressure_dpl, airspeed_pitot, altitude_agl, ada_vert_speed, acc_x, acc_y, acc_z, gyro_x, gyro_y, gyro_z, mag_x, mag_y, mag_z, gps_fix, gps_lat, gps_lon, gps_alt, abk_angle, abk_estimated_cd, parachute_load, nas_n, nas_e, nas_d, nas_vn, nas_ve, nas_vd, nas_qx, nas_qy, nas_qz, nas_qw, nas_bias_x, nas_bias_y, nas_bias_z, pin_launch, pin_nosecone, pin_expulsion, cutter_presence, estimated_thrust, vbat, temperature, logger_error):
+ def __init__(self, timestamp, ada_state, fmm_state, dpl_state, abk_state, nas_state, mea_state, pressure_ada, pressure_digi, pressure_static, pressure_dpl, airspeed_pitot, altitude_agl, ada_vert_speed, mea_mass, acc_x, acc_y, acc_z, gyro_x, gyro_y, gyro_z, mag_x, mag_y, mag_z, gps_fix, gps_lat, gps_lon, gps_alt, abk_angle, nas_n, nas_e, nas_d, nas_vn, nas_ve, nas_vd, nas_qx, nas_qy, nas_qz, nas_qw, nas_bias_x, nas_bias_y, nas_bias_z, pin_launch, pin_nosecone, pin_expulsion, cutter_presence, battery_voltage, current_consumption, temperature, logger_error):
MAVLink_message.__init__(self, MAVLink_rocket_flight_tm_message.id, MAVLink_rocket_flight_tm_message.name)
self._fieldnames = MAVLink_rocket_flight_tm_message.fieldnames
self._instance_field = MAVLink_rocket_flight_tm_message.instance_field
@@ -2025,6 +2075,7 @@ class MAVLink_rocket_flight_tm_message(MAVLink_message):
self.dpl_state = dpl_state
self.abk_state = abk_state
self.nas_state = nas_state
+ self.mea_state = mea_state
self.pressure_ada = pressure_ada
self.pressure_digi = pressure_digi
self.pressure_static = pressure_static
@@ -2032,6 +2083,7 @@ class MAVLink_rocket_flight_tm_message(MAVLink_message):
self.airspeed_pitot = airspeed_pitot
self.altitude_agl = altitude_agl
self.ada_vert_speed = ada_vert_speed
+ self.mea_mass = mea_mass
self.acc_x = acc_x
self.acc_y = acc_y
self.acc_z = acc_z
@@ -2046,8 +2098,6 @@ class MAVLink_rocket_flight_tm_message(MAVLink_message):
self.gps_lon = gps_lon
self.gps_alt = gps_alt
self.abk_angle = abk_angle
- self.abk_estimated_cd = abk_estimated_cd
- self.parachute_load = parachute_load
self.nas_n = nas_n
self.nas_e = nas_e
self.nas_d = nas_d
@@ -2065,13 +2115,13 @@ class MAVLink_rocket_flight_tm_message(MAVLink_message):
self.pin_nosecone = pin_nosecone
self.pin_expulsion = pin_expulsion
self.cutter_presence = cutter_presence
- self.estimated_thrust = estimated_thrust
- self.vbat = vbat
+ self.battery_voltage = battery_voltage
+ self.current_consumption = current_consumption
self.temperature = temperature
self.logger_error = logger_error
def pack(self, mav, force_mavlink1=False):
- return MAVLink_message.pack(self, mav, 141, struct.pack('<QffffffffffffffffffffffffffffffffffffffBBBBBBBBBBb', self.timestamp, self.pressure_ada, self.pressure_digi, self.pressure_static, self.pressure_dpl, self.airspeed_pitot, self.altitude_agl, self.ada_vert_speed, self.acc_x, self.acc_y, self.acc_z, self.gyro_x, self.gyro_y, self.gyro_z, self.mag_x, self.mag_y, self.mag_z, self.gps_lat, self.gps_lon, self.gps_alt, self.abk_angle, self.abk_estimated_cd, self.parachute_load, self.nas_n, self.nas_e, self.nas_d, self.nas_vn, self.nas_ve, self.nas_vd, self.nas_qx, self.nas_qy, self.nas_qz, self.nas_qw, self.nas_bias_x, self.nas_bias_y, self.nas_bias_z, self.estimated_thrust, self.vbat, self.temperature, self.ada_state, self.fmm_state, self.dpl_state, self.abk_state, self.nas_state, self.gps_fix, self.pin_launch, self.pin_nosecone, self.pin_expulsion, self.cutter_presence, self.logger_error), force_mavlink1=force_mavlink1)
+ return MAVLink_message.pack(self, mav, 254, struct.pack('<QfffffffffffffffffffffffffffffffffffffBBBBBBBBBBBb', self.timestamp, self.pressure_ada, self.pressure_digi, self.pressure_static, self.pressure_dpl, self.airspeed_pitot, self.altitude_agl, self.ada_vert_speed, self.mea_mass, self.acc_x, self.acc_y, self.acc_z, self.gyro_x, self.gyro_y, self.gyro_z, self.mag_x, self.mag_y, self.mag_z, self.gps_lat, self.gps_lon, self.gps_alt, self.abk_angle, self.nas_n, self.nas_e, self.nas_d, self.nas_vn, self.nas_ve, self.nas_vd, self.nas_qx, self.nas_qy, self.nas_qz, self.nas_qw, self.nas_bias_x, self.nas_bias_y, self.nas_bias_z, self.battery_voltage, self.current_consumption, self.temperature, self.ada_state, self.fmm_state, self.dpl_state, self.abk_state, self.nas_state, self.mea_state, self.gps_fix, self.pin_launch, self.pin_nosecone, self.pin_expulsion, self.cutter_presence, self.logger_error), force_mavlink1=force_mavlink1)
class MAVLink_payload_flight_tm_message(MAVLink_message):
'''
@@ -2079,23 +2129,23 @@ class MAVLink_payload_flight_tm_message(MAVLink_message):
'''
id = MAVLINK_MSG_ID_PAYLOAD_FLIGHT_TM
name = 'PAYLOAD_FLIGHT_TM'
- fieldnames = ['timestamp', 'fmm_state', 'nas_state', 'wes_state', 'pressure_digi', 'pressure_static', 'airspeed_pitot', 'altitude_agl', 'acc_x', 'acc_y', 'acc_z', 'gyro_x', 'gyro_y', 'gyro_z', 'mag_x', 'mag_y', 'mag_z', 'gps_fix', 'gps_lat', 'gps_lon', 'gps_alt', 'left_servo_angle', 'right_servo_angle', 'nas_n', 'nas_e', 'nas_d', 'nas_vn', 'nas_ve', 'nas_vd', 'nas_qx', 'nas_qy', 'nas_qz', 'nas_qw', 'nas_bias_x', 'nas_bias_y', 'nas_bias_z', 'wes_n', 'wes_e', 'pin_nosecone', 'vbat', 'vsupply_5v', 'temperature', 'logger_error']
- ordered_fieldnames = ['timestamp', 'pressure_digi', 'pressure_static', 'airspeed_pitot', 'altitude_agl', 'acc_x', 'acc_y', 'acc_z', 'gyro_x', 'gyro_y', 'gyro_z', 'mag_x', 'mag_y', 'mag_z', 'gps_lat', 'gps_lon', 'gps_alt', 'left_servo_angle', 'right_servo_angle', 'nas_n', 'nas_e', 'nas_d', 'nas_vn', 'nas_ve', 'nas_vd', 'nas_qx', 'nas_qy', 'nas_qz', 'nas_qw', 'nas_bias_x', 'nas_bias_y', 'nas_bias_z', 'wes_n', 'wes_e', 'vbat', 'vsupply_5v', 'temperature', 'fmm_state', 'nas_state', 'wes_state', 'gps_fix', 'pin_nosecone', 'logger_error']
- fieldtypes = ['uint64_t', 'uint8_t', 'uint8_t', 'uint8_t', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'uint8_t', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'uint8_t', 'float', 'float', 'float', 'int8_t']
+ fieldnames = ['timestamp', 'fmm_state', 'nas_state', 'wes_state', 'pressure_digi', 'pressure_static', 'airspeed_pitot', 'altitude_agl', 'acc_x', 'acc_y', 'acc_z', 'gyro_x', 'gyro_y', 'gyro_z', 'mag_x', 'mag_y', 'mag_z', 'gps_fix', 'gps_lat', 'gps_lon', 'gps_alt', 'left_servo_angle', 'right_servo_angle', 'nas_n', 'nas_e', 'nas_d', 'nas_vn', 'nas_ve', 'nas_vd', 'nas_qx', 'nas_qy', 'nas_qz', 'nas_qw', 'nas_bias_x', 'nas_bias_y', 'nas_bias_z', 'wes_n', 'wes_e', 'pin_nosecone', 'battery_voltage', 'current_consumption', 'vsupply_5v', 'temperature', 'logger_error']
+ ordered_fieldnames = ['timestamp', 'pressure_digi', 'pressure_static', 'airspeed_pitot', 'altitude_agl', 'acc_x', 'acc_y', 'acc_z', 'gyro_x', 'gyro_y', 'gyro_z', 'mag_x', 'mag_y', 'mag_z', 'gps_lat', 'gps_lon', 'gps_alt', 'left_servo_angle', 'right_servo_angle', 'nas_n', 'nas_e', 'nas_d', 'nas_vn', 'nas_ve', 'nas_vd', 'nas_qx', 'nas_qy', 'nas_qz', 'nas_qw', 'nas_bias_x', 'nas_bias_y', 'nas_bias_z', 'wes_n', 'wes_e', 'battery_voltage', 'current_consumption', 'vsupply_5v', 'temperature', 'fmm_state', 'nas_state', 'wes_state', 'gps_fix', 'pin_nosecone', 'logger_error']
+ fieldtypes = ['uint64_t', 'uint8_t', 'uint8_t', 'uint8_t', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'uint8_t', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'float', 'uint8_t', 'float', 'float', 'float', 'float', 'int8_t']
fielddisplays_by_name = {}
fieldenums_by_name = {}
- fieldunits_by_name = {"timestamp": "us", "pressure_digi": "Pa", "pressure_static": "Pa", "airspeed_pitot": "m/s", "altitude_agl": "m", "acc_x": "m/s^2", "acc_y": "m/s^2", "acc_z": "m/s^2", "gyro_x": "rad/s", "gyro_y": "rad/s", "gyro_z": "rad/s", "mag_x": "uT", "mag_y": "uT", "mag_z": "uT", "gps_lat": "deg", "gps_lon": "deg", "gps_alt": "m", "left_servo_angle": "deg", "right_servo_angle": "deg", "nas_n": "deg", "nas_e": "deg", "nas_d": "m", "nas_vn": "m/s", "nas_ve": "m/s", "nas_vd": "m/s", "nas_qx": "deg", "nas_qy": "deg", "nas_qz": "deg", "nas_qw": "deg", "wes_n": "m/s", "wes_e": "m/s", "vbat": "V", "vsupply_5v": "V", "temperature": "degC"}
- format = '<QffffffffffffffffffffffffffffffffffffBBBBBb'
- native_format = bytearray('<QffffffffffffffffffffffffffffffffffffBBBBBb', 'ascii')
- orders = [0, 37, 38, 39, 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 40, 14, 15, 16, 17, 18, 19, 20, 21, 22, 23, 24, 25, 26, 27, 28, 29, 30, 31, 32, 33, 41, 34, 35, 36, 42]
- lengths = [1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1]
- array_lengths = [0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0]
- crc_extra = 229
- unpacker = struct.Struct('<QffffffffffffffffffffffffffffffffffffBBBBBb')
+ fieldunits_by_name = {"timestamp": "us", "pressure_digi": "Pa", "pressure_static": "Pa", "airspeed_pitot": "m/s", "altitude_agl": "m", "acc_x": "m/s^2", "acc_y": "m/s^2", "acc_z": "m/s^2", "gyro_x": "rad/s", "gyro_y": "rad/s", "gyro_z": "rad/s", "mag_x": "uT", "mag_y": "uT", "mag_z": "uT", "gps_lat": "deg", "gps_lon": "deg", "gps_alt": "m", "left_servo_angle": "deg", "right_servo_angle": "deg", "nas_n": "deg", "nas_e": "deg", "nas_d": "m", "nas_vn": "m/s", "nas_ve": "m/s", "nas_vd": "m/s", "nas_qx": "deg", "nas_qy": "deg", "nas_qz": "deg", "nas_qw": "deg", "wes_n": "m/s", "wes_e": "m/s", "battery_voltage": "V", "current_consumption": "A", "vsupply_5v": "V", "temperature": "degC"}
+ format = '<QfffffffffffffffffffffffffffffffffffffBBBBBb'
+ native_format = bytearray('<QfffffffffffffffffffffffffffffffffffffBBBBBb', 'ascii')
+ orders = [0, 38, 39, 40, 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 41, 14, 15, 16, 17, 18, 19, 20, 21, 22, 23, 24, 25, 26, 27, 28, 29, 30, 31, 32, 33, 42, 34, 35, 36, 37, 43]
+ lengths = [1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1, 1]
+ array_lengths = [0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0]
+ crc_extra = 117
+ unpacker = struct.Struct('<QfffffffffffffffffffffffffffffffffffffBBBBBb')
instance_field = None
instance_offset = -1
- def __init__(self, timestamp, fmm_state, nas_state, wes_state, pressure_digi, pressure_static, airspeed_pitot, altitude_agl, acc_x, acc_y, acc_z, gyro_x, gyro_y, gyro_z, mag_x, mag_y, mag_z, gps_fix, gps_lat, gps_lon, gps_alt, left_servo_angle, right_servo_angle, nas_n, nas_e, nas_d, nas_vn, nas_ve, nas_vd, nas_qx, nas_qy, nas_qz, nas_qw, nas_bias_x, nas_bias_y, nas_bias_z, wes_n, wes_e, pin_nosecone, vbat, vsupply_5v, temperature, logger_error):
+ def __init__(self, timestamp, fmm_state, nas_state, wes_state, pressure_digi, pressure_static, airspeed_pitot, altitude_agl, acc_x, acc_y, acc_z, gyro_x, gyro_y, gyro_z, mag_x, mag_y, mag_z, gps_fix, gps_lat, gps_lon, gps_alt, left_servo_angle, right_servo_angle, nas_n, nas_e, nas_d, nas_vn, nas_ve, nas_vd, nas_qx, nas_qy, nas_qz, nas_qw, nas_bias_x, nas_bias_y, nas_bias_z, wes_n, wes_e, pin_nosecone, battery_voltage, current_consumption, vsupply_5v, temperature, logger_error):
MAVLink_message.__init__(self, MAVLink_payload_flight_tm_message.id, MAVLink_payload_flight_tm_message.name)
self._fieldnames = MAVLink_payload_flight_tm_message.fieldnames
self._instance_field = MAVLink_payload_flight_tm_message.instance_field
@@ -2139,13 +2189,14 @@ class MAVLink_payload_flight_tm_message(MAVLink_message):
self.wes_n = wes_n
self.wes_e = wes_e
self.pin_nosecone = pin_nosecone
- self.vbat = vbat
+ self.battery_voltage = battery_voltage
+ self.current_consumption = current_consumption
self.vsupply_5v = vsupply_5v
self.temperature = temperature
self.logger_error = logger_error
def pack(self, mav, force_mavlink1=False):
- return MAVLink_message.pack(self, mav, 229, struct.pack('<QffffffffffffffffffffffffffffffffffffBBBBBb', self.timestamp, self.pressure_digi, self.pressure_static, self.airspeed_pitot, self.altitude_agl, self.acc_x, self.acc_y, self.acc_z, self.gyro_x, self.gyro_y, self.gyro_z, self.mag_x, self.mag_y, self.mag_z, self.gps_lat, self.gps_lon, self.gps_alt, self.left_servo_angle, self.right_servo_angle, self.nas_n, self.nas_e, self.nas_d, self.nas_vn, self.nas_ve, self.nas_vd, self.nas_qx, self.nas_qy, self.nas_qz, self.nas_qw, self.nas_bias_x, self.nas_bias_y, self.nas_bias_z, self.wes_n, self.wes_e, self.vbat, self.vsupply_5v, self.temperature, self.fmm_state, self.nas_state, self.wes_state, self.gps_fix, self.pin_nosecone, self.logger_error), force_mavlink1=force_mavlink1)
+ return MAVLink_message.pack(self, mav, 117, struct.pack('<QfffffffffffffffffffffffffffffffffffffBBBBBb', self.timestamp, self.pressure_digi, self.pressure_static, self.airspeed_pitot, self.altitude_agl, self.acc_x, self.acc_y, self.acc_z, self.gyro_x, self.gyro_y, self.gyro_z, self.mag_x, self.mag_y, self.mag_z, self.gps_lat, self.gps_lon, self.gps_alt, self.left_servo_angle, self.right_servo_angle, self.nas_n, self.nas_e, self.nas_d, self.nas_vn, self.nas_ve, self.nas_vd, self.nas_qx, self.nas_qy, self.nas_qz, self.nas_qw, self.nas_bias_x, self.nas_bias_y, self.nas_bias_z, self.wes_n, self.wes_e, self.battery_voltage, self.current_consumption, self.vsupply_5v, self.temperature, self.fmm_state, self.nas_state, self.wes_state, self.gps_fix, self.pin_nosecone, self.logger_error), force_mavlink1=force_mavlink1)
class MAVLink_rocket_stats_tm_message(MAVLink_message):
'''
@@ -2296,23 +2347,23 @@ class MAVLink_motor_tm_message(MAVLink_message):
'''
id = MAVLINK_MSG_ID_MOTOR_TM
name = 'MOTOR_TM'
- fieldnames = ['timestamp', 'top_tank_pressure', 'bottom_tank_pressure', 'combustion_chamber_pressure', 'floating_level', 'tank_temperature', 'main_valve_state']
- ordered_fieldnames = ['timestamp', 'top_tank_pressure', 'bottom_tank_pressure', 'combustion_chamber_pressure', 'tank_temperature', 'floating_level', 'main_valve_state']
- fieldtypes = ['uint64_t', 'float', 'float', 'float', 'uint8_t', 'float', 'uint8_t']
+ fieldnames = ['timestamp', 'top_tank_pressure', 'bottom_tank_pressure', 'combustion_chamber_pressure', 'floating_level', 'tank_temperature', 'main_valve_state', 'battery_voltage', 'current_consumption']
+ ordered_fieldnames = ['timestamp', 'top_tank_pressure', 'bottom_tank_pressure', 'combustion_chamber_pressure', 'tank_temperature', 'battery_voltage', 'current_consumption', 'floating_level', 'main_valve_state']
+ fieldtypes = ['uint64_t', 'float', 'float', 'float', 'uint8_t', 'float', 'uint8_t', 'float', 'float']
fielddisplays_by_name = {}
fieldenums_by_name = {}
- fieldunits_by_name = {"timestamp": "us", "top_tank_pressure": "Bar", "bottom_tank_pressure": "Bar", "combustion_chamber_pressure": "Bar"}
- format = '<QffffBB'
- native_format = bytearray('<QffffBB', 'ascii')
- orders = [0, 1, 2, 3, 5, 4, 6]
- lengths = [1, 1, 1, 1, 1, 1, 1]
- array_lengths = [0, 0, 0, 0, 0, 0, 0]
- crc_extra = 241
- unpacker = struct.Struct('<QffffBB')
+ fieldunits_by_name = {"timestamp": "us", "top_tank_pressure": "Bar", "bottom_tank_pressure": "Bar", "combustion_chamber_pressure": "Bar", "battery_voltage": "V", "current_consumption": "A"}
+ format = '<QffffffBB'
+ native_format = bytearray('<QffffffBB', 'ascii')
+ orders = [0, 1, 2, 3, 7, 4, 8, 5, 6]
+ lengths = [1, 1, 1, 1, 1, 1, 1, 1, 1]
+ array_lengths = [0, 0, 0, 0, 0, 0, 0, 0, 0]
+ crc_extra = 196
+ unpacker = struct.Struct('<QffffffBB')
instance_field = None
instance_offset = -1
- def __init__(self, timestamp, top_tank_pressure, bottom_tank_pressure, combustion_chamber_pressure, floating_level, tank_temperature, main_valve_state):
+ def __init__(self, timestamp, top_tank_pressure, bottom_tank_pressure, combustion_chamber_pressure, floating_level, tank_temperature, main_valve_state, battery_voltage, current_consumption):
MAVLink_message.__init__(self, MAVLink_motor_tm_message.id, MAVLink_motor_tm_message.name)
self._fieldnames = MAVLink_motor_tm_message.fieldnames
self._instance_field = MAVLink_motor_tm_message.instance_field
@@ -2324,9 +2375,11 @@ class MAVLink_motor_tm_message(MAVLink_message):
self.floating_level = floating_level
self.tank_temperature = tank_temperature
self.main_valve_state = main_valve_state
+ self.battery_voltage = battery_voltage
+ self.current_consumption = current_consumption
def pack(self, mav, force_mavlink1=False):
- return MAVLink_message.pack(self, mav, 241, struct.pack('<QffffBB', self.timestamp, self.top_tank_pressure, self.bottom_tank_pressure, self.combustion_chamber_pressure, self.tank_temperature, self.floating_level, self.main_valve_state), force_mavlink1=force_mavlink1)
+ return MAVLink_message.pack(self, mav, 196, struct.pack('<QffffffBB', self.timestamp, self.top_tank_pressure, self.bottom_tank_pressure, self.combustion_chamber_pressure, self.tank_temperature, self.battery_voltage, self.current_consumption, self.floating_level, self.main_valve_state), force_mavlink1=force_mavlink1)
mavlink_map = {
@@ -2372,6 +2425,7 @@ mavlink_map = {
MAVLINK_MSG_ID_TASK_STATS_TM : MAVLink_task_stats_tm_message,
MAVLINK_MSG_ID_ADA_TM : MAVLink_ada_tm_message,
MAVLINK_MSG_ID_NAS_TM : MAVLink_nas_tm_message,
+ MAVLINK_MSG_ID_MEA_TM : MAVLink_mea_tm_message,
MAVLINK_MSG_ID_ROCKET_FLIGHT_TM : MAVLink_rocket_flight_tm_message,
MAVLINK_MSG_ID_PAYLOAD_FLIGHT_TM : MAVLink_payload_flight_tm_message,
MAVLINK_MSG_ID_ROCKET_STATS_TM : MAVLink_rocket_stats_tm_message,
@@ -3869,7 +3923,37 @@ class MAVLink(object):
'''
return self.send(self.nas_tm_encode(timestamp, state, nas_n, nas_e, nas_d, nas_vn, nas_ve, nas_vd, nas_qx, nas_qy, nas_qz, nas_qw, nas_bias_x, nas_bias_y, nas_bias_z, ref_pressure, ref_temperature, ref_latitude, ref_longitude), force_mavlink1=force_mavlink1)
- def rocket_flight_tm_encode(self, timestamp, ada_state, fmm_state, dpl_state, abk_state, nas_state, pressure_ada, pressure_digi, pressure_static, pressure_dpl, airspeed_pitot, altitude_agl, ada_vert_speed, acc_x, acc_y, acc_z, gyro_x, gyro_y, gyro_z, mag_x, mag_y, mag_z, gps_fix, gps_lat, gps_lon, gps_alt, abk_angle, abk_estimated_cd, parachute_load, nas_n, nas_e, nas_d, nas_vn, nas_ve, nas_vd, nas_qx, nas_qy, nas_qz, nas_qw, nas_bias_x, nas_bias_y, nas_bias_z, pin_launch, pin_nosecone, pin_expulsion, cutter_presence, estimated_thrust, vbat, temperature, logger_error):
+ def mea_tm_encode(self, timestamp, state, kalman_x0, kalman_x1, kalman_x2, mass, corrected_pressure):
+ '''
+ Mass Estimation Algorithm status telemetry
+
+ timestamp : When was this logged [us] (type:uint64_t)
+ state : MEA current state (type:uint8_t)
+ kalman_x0 : Kalman state variable 0 (corrected pressure) (type:float)
+ kalman_x1 : Kalman state variable 1 (type:float)
+ kalman_x2 : Kalman state variable 2 (mass) (type:float)
+ mass : Mass estimated [kg] (type:float)
+ corrected_pressure : Corrected pressure [kg] (type:float)
+
+ '''
+ return MAVLink_mea_tm_message(timestamp, state, kalman_x0, kalman_x1, kalman_x2, mass, corrected_pressure)
+
+ def mea_tm_send(self, timestamp, state, kalman_x0, kalman_x1, kalman_x2, mass, corrected_pressure, force_mavlink1=False):
+ '''
+ Mass Estimation Algorithm status telemetry
+
+ timestamp : When was this logged [us] (type:uint64_t)
+ state : MEA current state (type:uint8_t)
+ kalman_x0 : Kalman state variable 0 (corrected pressure) (type:float)
+ kalman_x1 : Kalman state variable 1 (type:float)
+ kalman_x2 : Kalman state variable 2 (mass) (type:float)
+ mass : Mass estimated [kg] (type:float)
+ corrected_pressure : Corrected pressure [kg] (type:float)
+
+ '''
+ return self.send(self.mea_tm_encode(timestamp, state, kalman_x0, kalman_x1, kalman_x2, mass, corrected_pressure), force_mavlink1=force_mavlink1)
+
+ def rocket_flight_tm_encode(self, timestamp, ada_state, fmm_state, dpl_state, abk_state, nas_state, mea_state, pressure_ada, pressure_digi, pressure_static, pressure_dpl, airspeed_pitot, altitude_agl, ada_vert_speed, mea_mass, acc_x, acc_y, acc_z, gyro_x, gyro_y, gyro_z, mag_x, mag_y, mag_z, gps_fix, gps_lat, gps_lon, gps_alt, abk_angle, nas_n, nas_e, nas_d, nas_vn, nas_ve, nas_vd, nas_qx, nas_qy, nas_qz, nas_qw, nas_bias_x, nas_bias_y, nas_bias_z, pin_launch, pin_nosecone, pin_expulsion, cutter_presence, battery_voltage, current_consumption, temperature, logger_error):
'''
High Rate Telemetry
@@ -3879,6 +3963,7 @@ class MAVLink(object):
dpl_state : Deployment Controller State (type:uint8_t)
abk_state : Airbrake FSM state (type:uint8_t)
nas_state : Navigation System FSM State (type:uint8_t)
+ mea_state : MEA Controller State (type:uint8_t)
pressure_ada : Atmospheric pressure estimated by ADA [Pa] (type:float)
pressure_digi : Pressure from digital sensor [Pa] (type:float)
pressure_static : Pressure from static port [Pa] (type:float)
@@ -3886,6 +3971,7 @@ class MAVLink(object):
airspeed_pitot : Pitot airspeed [m/s] (type:float)
altitude_agl : Altitude above ground level [m] (type:float)
ada_vert_speed : Vertical speed estimated by ADA [m/s] (type:float)
+ mea_mass : Mass estimated by MEA [kg] (type:float)
acc_x : Acceleration on X axis (body) [m/s^2] (type:float)
acc_y : Acceleration on Y axis (body) [m/s^2] (type:float)
acc_z : Acceleration on Z axis (body) [m/s^2] (type:float)
@@ -3900,8 +3986,6 @@ class MAVLink(object):
gps_lon : Longitude [deg] (type:float)
gps_alt : GPS Altitude [m] (type:float)
abk_angle : Air Brakes angle [deg] (type:float)
- abk_estimated_cd : Estimated drag coefficient (type:float)
- parachute_load : Parachute load cell value (type:float)
nas_n : Navigation system estimated noth position [deg] (type:float)
nas_e : Navigation system estimated east position [deg] (type:float)
nas_d : Navigation system estimated down position [m] (type:float)
@@ -3919,15 +4003,15 @@ class MAVLink(object):
pin_nosecone : Nosecone pin status (1 = connected, 0 = disconnected) (type:uint8_t)
pin_expulsion : Servo sensor status (1 = actuated, 0 = idle) (type:uint8_t)
cutter_presence : Cutter presence status (1 = present, 0 = missing) (type:uint8_t)
- estimated_thrust : Estimated thrust from automatic shutdown algorithm (type:float)
- vbat : Battery voltage [V] (type:float)
+ battery_voltage : Battery voltage [V] (type:float)
+ current_consumption : Battery current [A] (type:float)
temperature : Temperature [degC] (type:float)
logger_error : Logger error (0 = no error, -1 otherwise) (type:int8_t)
'''
- return MAVLink_rocket_flight_tm_message(timestamp, ada_state, fmm_state, dpl_state, abk_state, nas_state, pressure_ada, pressure_digi, pressure_static, pressure_dpl, airspeed_pitot, altitude_agl, ada_vert_speed, acc_x, acc_y, acc_z, gyro_x, gyro_y, gyro_z, mag_x, mag_y, mag_z, gps_fix, gps_lat, gps_lon, gps_alt, abk_angle, abk_estimated_cd, parachute_load, nas_n, nas_e, nas_d, nas_vn, nas_ve, nas_vd, nas_qx, nas_qy, nas_qz, nas_qw, nas_bias_x, nas_bias_y, nas_bias_z, pin_launch, pin_nosecone, pin_expulsion, cutter_presence, estimated_thrust, vbat, temperature, logger_error)
+ return MAVLink_rocket_flight_tm_message(timestamp, ada_state, fmm_state, dpl_state, abk_state, nas_state, mea_state, pressure_ada, pressure_digi, pressure_static, pressure_dpl, airspeed_pitot, altitude_agl, ada_vert_speed, mea_mass, acc_x, acc_y, acc_z, gyro_x, gyro_y, gyro_z, mag_x, mag_y, mag_z, gps_fix, gps_lat, gps_lon, gps_alt, abk_angle, nas_n, nas_e, nas_d, nas_vn, nas_ve, nas_vd, nas_qx, nas_qy, nas_qz, nas_qw, nas_bias_x, nas_bias_y, nas_bias_z, pin_launch, pin_nosecone, pin_expulsion, cutter_presence, battery_voltage, current_consumption, temperature, logger_error)
- def rocket_flight_tm_send(self, timestamp, ada_state, fmm_state, dpl_state, abk_state, nas_state, pressure_ada, pressure_digi, pressure_static, pressure_dpl, airspeed_pitot, altitude_agl, ada_vert_speed, acc_x, acc_y, acc_z, gyro_x, gyro_y, gyro_z, mag_x, mag_y, mag_z, gps_fix, gps_lat, gps_lon, gps_alt, abk_angle, abk_estimated_cd, parachute_load, nas_n, nas_e, nas_d, nas_vn, nas_ve, nas_vd, nas_qx, nas_qy, nas_qz, nas_qw, nas_bias_x, nas_bias_y, nas_bias_z, pin_launch, pin_nosecone, pin_expulsion, cutter_presence, estimated_thrust, vbat, temperature, logger_error, force_mavlink1=False):
+ def rocket_flight_tm_send(self, timestamp, ada_state, fmm_state, dpl_state, abk_state, nas_state, mea_state, pressure_ada, pressure_digi, pressure_static, pressure_dpl, airspeed_pitot, altitude_agl, ada_vert_speed, mea_mass, acc_x, acc_y, acc_z, gyro_x, gyro_y, gyro_z, mag_x, mag_y, mag_z, gps_fix, gps_lat, gps_lon, gps_alt, abk_angle, nas_n, nas_e, nas_d, nas_vn, nas_ve, nas_vd, nas_qx, nas_qy, nas_qz, nas_qw, nas_bias_x, nas_bias_y, nas_bias_z, pin_launch, pin_nosecone, pin_expulsion, cutter_presence, battery_voltage, current_consumption, temperature, logger_error, force_mavlink1=False):
'''
High Rate Telemetry
@@ -3937,6 +4021,7 @@ class MAVLink(object):
dpl_state : Deployment Controller State (type:uint8_t)
abk_state : Airbrake FSM state (type:uint8_t)
nas_state : Navigation System FSM State (type:uint8_t)
+ mea_state : MEA Controller State (type:uint8_t)
pressure_ada : Atmospheric pressure estimated by ADA [Pa] (type:float)
pressure_digi : Pressure from digital sensor [Pa] (type:float)
pressure_static : Pressure from static port [Pa] (type:float)
@@ -3944,6 +4029,7 @@ class MAVLink(object):
airspeed_pitot : Pitot airspeed [m/s] (type:float)
altitude_agl : Altitude above ground level [m] (type:float)
ada_vert_speed : Vertical speed estimated by ADA [m/s] (type:float)
+ mea_mass : Mass estimated by MEA [kg] (type:float)
acc_x : Acceleration on X axis (body) [m/s^2] (type:float)
acc_y : Acceleration on Y axis (body) [m/s^2] (type:float)
acc_z : Acceleration on Z axis (body) [m/s^2] (type:float)
@@ -3958,8 +4044,6 @@ class MAVLink(object):
gps_lon : Longitude [deg] (type:float)
gps_alt : GPS Altitude [m] (type:float)
abk_angle : Air Brakes angle [deg] (type:float)
- abk_estimated_cd : Estimated drag coefficient (type:float)
- parachute_load : Parachute load cell value (type:float)
nas_n : Navigation system estimated noth position [deg] (type:float)
nas_e : Navigation system estimated east position [deg] (type:float)
nas_d : Navigation system estimated down position [m] (type:float)
@@ -3977,15 +4061,15 @@ class MAVLink(object):
pin_nosecone : Nosecone pin status (1 = connected, 0 = disconnected) (type:uint8_t)
pin_expulsion : Servo sensor status (1 = actuated, 0 = idle) (type:uint8_t)
cutter_presence : Cutter presence status (1 = present, 0 = missing) (type:uint8_t)
- estimated_thrust : Estimated thrust from automatic shutdown algorithm (type:float)
- vbat : Battery voltage [V] (type:float)
+ battery_voltage : Battery voltage [V] (type:float)
+ current_consumption : Battery current [A] (type:float)
temperature : Temperature [degC] (type:float)
logger_error : Logger error (0 = no error, -1 otherwise) (type:int8_t)
'''
- return self.send(self.rocket_flight_tm_encode(timestamp, ada_state, fmm_state, dpl_state, abk_state, nas_state, pressure_ada, pressure_digi, pressure_static, pressure_dpl, airspeed_pitot, altitude_agl, ada_vert_speed, acc_x, acc_y, acc_z, gyro_x, gyro_y, gyro_z, mag_x, mag_y, mag_z, gps_fix, gps_lat, gps_lon, gps_alt, abk_angle, abk_estimated_cd, parachute_load, nas_n, nas_e, nas_d, nas_vn, nas_ve, nas_vd, nas_qx, nas_qy, nas_qz, nas_qw, nas_bias_x, nas_bias_y, nas_bias_z, pin_launch, pin_nosecone, pin_expulsion, cutter_presence, estimated_thrust, vbat, temperature, logger_error), force_mavlink1=force_mavlink1)
+ return self.send(self.rocket_flight_tm_encode(timestamp, ada_state, fmm_state, dpl_state, abk_state, nas_state, mea_state, pressure_ada, pressure_digi, pressure_static, pressure_dpl, airspeed_pitot, altitude_agl, ada_vert_speed, mea_mass, acc_x, acc_y, acc_z, gyro_x, gyro_y, gyro_z, mag_x, mag_y, mag_z, gps_fix, gps_lat, gps_lon, gps_alt, abk_angle, nas_n, nas_e, nas_d, nas_vn, nas_ve, nas_vd, nas_qx, nas_qy, nas_qz, nas_qw, nas_bias_x, nas_bias_y, nas_bias_z, pin_launch, pin_nosecone, pin_expulsion, cutter_presence, battery_voltage, current_consumption, temperature, logger_error), force_mavlink1=force_mavlink1)
- def payload_flight_tm_encode(self, timestamp, fmm_state, nas_state, wes_state, pressure_digi, pressure_static, airspeed_pitot, altitude_agl, acc_x, acc_y, acc_z, gyro_x, gyro_y, gyro_z, mag_x, mag_y, mag_z, gps_fix, gps_lat, gps_lon, gps_alt, left_servo_angle, right_servo_angle, nas_n, nas_e, nas_d, nas_vn, nas_ve, nas_vd, nas_qx, nas_qy, nas_qz, nas_qw, nas_bias_x, nas_bias_y, nas_bias_z, wes_n, wes_e, pin_nosecone, vbat, vsupply_5v, temperature, logger_error):
+ def payload_flight_tm_encode(self, timestamp, fmm_state, nas_state, wes_state, pressure_digi, pressure_static, airspeed_pitot, altitude_agl, acc_x, acc_y, acc_z, gyro_x, gyro_y, gyro_z, mag_x, mag_y, mag_z, gps_fix, gps_lat, gps_lon, gps_alt, left_servo_angle, right_servo_angle, nas_n, nas_e, nas_d, nas_vn, nas_ve, nas_vd, nas_qx, nas_qy, nas_qz, nas_qw, nas_bias_x, nas_bias_y, nas_bias_z, wes_n, wes_e, pin_nosecone, battery_voltage, current_consumption, vsupply_5v, temperature, logger_error):
'''
High Rate Telemetry
@@ -4028,15 +4112,16 @@ class MAVLink(object):
wes_n : Wind estimated north velocity [m/s] (type:float)
wes_e : Wind estimated east velocity [m/s] (type:float)
pin_nosecone : Nosecone pin status (1 = connected, 0 = disconnected) (type:uint8_t)
- vbat : Battery voltage [V] (type:float)
+ battery_voltage : Battery voltage [V] (type:float)
+ current_consumption : Battery current [A] (type:float)
vsupply_5v : Power supply 5V [V] (type:float)
temperature : Temperature [degC] (type:float)
logger_error : Logger error (0 = no error) (type:int8_t)
'''
- return MAVLink_payload_flight_tm_message(timestamp, fmm_state, nas_state, wes_state, pressure_digi, pressure_static, airspeed_pitot, altitude_agl, acc_x, acc_y, acc_z, gyro_x, gyro_y, gyro_z, mag_x, mag_y, mag_z, gps_fix, gps_lat, gps_lon, gps_alt, left_servo_angle, right_servo_angle, nas_n, nas_e, nas_d, nas_vn, nas_ve, nas_vd, nas_qx, nas_qy, nas_qz, nas_qw, nas_bias_x, nas_bias_y, nas_bias_z, wes_n, wes_e, pin_nosecone, vbat, vsupply_5v, temperature, logger_error)
+ return MAVLink_payload_flight_tm_message(timestamp, fmm_state, nas_state, wes_state, pressure_digi, pressure_static, airspeed_pitot, altitude_agl, acc_x, acc_y, acc_z, gyro_x, gyro_y, gyro_z, mag_x, mag_y, mag_z, gps_fix, gps_lat, gps_lon, gps_alt, left_servo_angle, right_servo_angle, nas_n, nas_e, nas_d, nas_vn, nas_ve, nas_vd, nas_qx, nas_qy, nas_qz, nas_qw, nas_bias_x, nas_bias_y, nas_bias_z, wes_n, wes_e, pin_nosecone, battery_voltage, current_consumption, vsupply_5v, temperature, logger_error)
- def payload_flight_tm_send(self, timestamp, fmm_state, nas_state, wes_state, pressure_digi, pressure_static, airspeed_pitot, altitude_agl, acc_x, acc_y, acc_z, gyro_x, gyro_y, gyro_z, mag_x, mag_y, mag_z, gps_fix, gps_lat, gps_lon, gps_alt, left_servo_angle, right_servo_angle, nas_n, nas_e, nas_d, nas_vn, nas_ve, nas_vd, nas_qx, nas_qy, nas_qz, nas_qw, nas_bias_x, nas_bias_y, nas_bias_z, wes_n, wes_e, pin_nosecone, vbat, vsupply_5v, temperature, logger_error, force_mavlink1=False):
+ def payload_flight_tm_send(self, timestamp, fmm_state, nas_state, wes_state, pressure_digi, pressure_static, airspeed_pitot, altitude_agl, acc_x, acc_y, acc_z, gyro_x, gyro_y, gyro_z, mag_x, mag_y, mag_z, gps_fix, gps_lat, gps_lon, gps_alt, left_servo_angle, right_servo_angle, nas_n, nas_e, nas_d, nas_vn, nas_ve, nas_vd, nas_qx, nas_qy, nas_qz, nas_qw, nas_bias_x, nas_bias_y, nas_bias_z, wes_n, wes_e, pin_nosecone, battery_voltage, current_consumption, vsupply_5v, temperature, logger_error, force_mavlink1=False):
'''
High Rate Telemetry
@@ -4079,13 +4164,14 @@ class MAVLink(object):
wes_n : Wind estimated north velocity [m/s] (type:float)
wes_e : Wind estimated east velocity [m/s] (type:float)
pin_nosecone : Nosecone pin status (1 = connected, 0 = disconnected) (type:uint8_t)
- vbat : Battery voltage [V] (type:float)
+ battery_voltage : Battery voltage [V] (type:float)
+ current_consumption : Battery current [A] (type:float)
vsupply_5v : Power supply 5V [V] (type:float)
temperature : Temperature [degC] (type:float)
logger_error : Logger error (0 = no error) (type:int8_t)
'''
- return self.send(self.payload_flight_tm_encode(timestamp, fmm_state, nas_state, wes_state, pressure_digi, pressure_static, airspeed_pitot, altitude_agl, acc_x, acc_y, acc_z, gyro_x, gyro_y, gyro_z, mag_x, mag_y, mag_z, gps_fix, gps_lat, gps_lon, gps_alt, left_servo_angle, right_servo_angle, nas_n, nas_e, nas_d, nas_vn, nas_ve, nas_vd, nas_qx, nas_qy, nas_qz, nas_qw, nas_bias_x, nas_bias_y, nas_bias_z, wes_n, wes_e, pin_nosecone, vbat, vsupply_5v, temperature, logger_error), force_mavlink1=force_mavlink1)
+ return self.send(self.payload_flight_tm_encode(timestamp, fmm_state, nas_state, wes_state, pressure_digi, pressure_static, airspeed_pitot, altitude_agl, acc_x, acc_y, acc_z, gyro_x, gyro_y, gyro_z, mag_x, mag_y, mag_z, gps_fix, gps_lat, gps_lon, gps_alt, left_servo_angle, right_servo_angle, nas_n, nas_e, nas_d, nas_vn, nas_ve, nas_vd, nas_qx, nas_qy, nas_qz, nas_qw, nas_bias_x, nas_bias_y, nas_bias_z, wes_n, wes_e, pin_nosecone, battery_voltage, current_consumption, vsupply_5v, temperature, logger_error), force_mavlink1=force_mavlink1)
def rocket_stats_tm_encode(self, liftoff_ts, liftoff_max_acc_ts, liftoff_max_acc, dpl_ts, dpl_max_acc, max_z_speed_ts, max_z_speed, max_airspeed_pitot, max_speed_altitude, apogee_ts, apogee_lat, apogee_lon, apogee_alt, min_pressure, ada_min_pressure, dpl_vane_max_pressure, cpu_load, free_heap):
'''
@@ -4235,7 +4321,7 @@ class MAVLink(object):
'''
return self.send(self.gse_tm_encode(timestamp, loadcell_tank, loadcell_vessel, filling_pressure, vessel_pressure, arming_state, filling_valve_state, venting_valve_state, release_valve_state, main_valve_state, ignition_state, tars_state, battery_voltage, current_consumption, main_board_status, payload_board_status, motor_board_status), force_mavlink1=force_mavlink1)
- def motor_tm_encode(self, timestamp, top_tank_pressure, bottom_tank_pressure, combustion_chamber_pressure, floating_level, tank_temperature, main_valve_state):
+ def motor_tm_encode(self, timestamp, top_tank_pressure, bottom_tank_pressure, combustion_chamber_pressure, floating_level, tank_temperature, main_valve_state, battery_voltage, current_consumption):
'''
Motor rocket telemetry
@@ -4246,11 +4332,13 @@ class MAVLink(object):
floating_level : Floating level in tank (type:uint8_t)
tank_temperature : Tank temperature (type:float)
main_valve_state : 1 If the main valve is open (type:uint8_t)
+ battery_voltage : Battery voltage [V] (type:float)
+ current_consumption : Current drained from the battery [A] (type:float)
'''
- return MAVLink_motor_tm_message(timestamp, top_tank_pressure, bottom_tank_pressure, combustion_chamber_pressure, floating_level, tank_temperature, main_valve_state)
+ return MAVLink_motor_tm_message(timestamp, top_tank_pressure, bottom_tank_pressure, combustion_chamber_pressure, floating_level, tank_temperature, main_valve_state, battery_voltage, current_consumption)
- def motor_tm_send(self, timestamp, top_tank_pressure, bottom_tank_pressure, combustion_chamber_pressure, floating_level, tank_temperature, main_valve_state, force_mavlink1=False):
+ def motor_tm_send(self, timestamp, top_tank_pressure, bottom_tank_pressure, combustion_chamber_pressure, floating_level, tank_temperature, main_valve_state, battery_voltage, current_consumption, force_mavlink1=False):
'''
Motor rocket telemetry
@@ -4261,7 +4349,9 @@ class MAVLink(object):
floating_level : Floating level in tank (type:uint8_t)
tank_temperature : Tank temperature (type:float)
main_valve_state : 1 If the main valve is open (type:uint8_t)
+ battery_voltage : Battery voltage [V] (type:float)
+ current_consumption : Current drained from the battery [A] (type:float)
'''
- return self.send(self.motor_tm_encode(timestamp, top_tank_pressure, bottom_tank_pressure, combustion_chamber_pressure, floating_level, tank_temperature, main_valve_state), force_mavlink1=force_mavlink1)
+ return self.send(self.motor_tm_encode(timestamp, top_tank_pressure, bottom_tank_pressure, combustion_chamber_pressure, floating_level, tank_temperature, main_valve_state, battery_voltage, current_consumption), force_mavlink1=force_mavlink1)
diff --git a/mavlink_lib/gemini/gemini.h b/mavlink_lib/gemini/gemini.h
index 74c55f0c08c5a353f32a29a28adbd13d9811b41f..fef31169347724007acfc639a89ac528349b08da 100644
--- a/mavlink_lib/gemini/gemini.h
+++ b/mavlink_lib/gemini/gemini.h
@@ -11,7 +11,7 @@
#endif
#undef MAVLINK_THIS_XML_HASH
-#define MAVLINK_THIS_XML_HASH -129419792422964465
+#define MAVLINK_THIS_XML_HASH -2036237758109455771
#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, 46, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 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, 0, 171, 158, 92, 76, 42, 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, 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, 46, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 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, 168, 162, 92, 76, 42, 34, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 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, 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, 183, 242, 142, 108, 133, 234, 66, 0, 141, 229, 245, 115, 89, 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, 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, 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, 183, 242, 142, 108, 133, 234, 66, 11, 254, 117, 245, 115, 89, 196, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 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 +34,18 @@ 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
+{
+ MAIN=1, /* | */
+ PAYLOAD=2, /* | */
+ RIG=3, /* | */
+ SysIDs_ENUM_END=4, /* | */
+} SysIDs;
+#endif
+
/** @brief Enum list for all the telemetries that can be requested */
#ifndef HAVE_ENUM_SystemTMList
#define HAVE_ENUM_SystemTMList
@@ -47,13 +59,13 @@ 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
@@ -205,6 +217,7 @@ 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_mea_tm.h"
#include "./mavlink_msg_rocket_flight_tm.h"
#include "./mavlink_msg_payload_flight_tm.h"
#include "./mavlink_msg_rocket_stats_tm.h"
@@ -216,11 +229,11 @@ typedef enum PinsList
#undef MAVLINK_THIS_XML_HASH
-#define MAVLINK_THIS_XML_HASH -129419792422964465
+#define MAVLINK_THIS_XML_HASH -2036237758109455771
#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, {"EMPTY",0,{{"","",MAVLINK_TYPE_CHAR,0,0,0}}}, 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 }, { "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
diff --git a/mavlink_lib/gemini/mavlink.h b/mavlink_lib/gemini/mavlink.h
index 328a3cc1a1cbe26094823ba69a54a6944c2177fd..29670cec5272e6543d1d4739240aaafa485b5043 100644
--- a/mavlink_lib/gemini/mavlink.h
+++ b/mavlink_lib/gemini/mavlink.h
@@ -6,7 +6,7 @@
#ifndef MAVLINK_H
#define MAVLINK_H
-#define MAVLINK_PRIMARY_XML_HASH -129419792422964465
+#define MAVLINK_PRIMARY_XML_HASH -2036237758109455771
#ifndef MAVLINK_STX
#define MAVLINK_STX 254
diff --git a/mavlink_lib/gemini/mavlink_msg_mea_tm.h b/mavlink_lib/gemini/mavlink_msg_mea_tm.h
new file mode 100644
index 0000000000000000000000000000000000000000..a3887d7e6363b14616deca868632f1fc6c0d3b26
--- /dev/null
+++ b/mavlink_lib/gemini/mavlink_msg_mea_tm.h
@@ -0,0 +1,363 @@
+#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
+}
diff --git a/mavlink_lib/gemini/mavlink_msg_motor_tm.h b/mavlink_lib/gemini/mavlink_msg_motor_tm.h
index 508ce65e21679c49c95c240cb5fb0f05ade61e0f..969ea55c63bfcf709aff006824978ba6a7361312 100644
--- a/mavlink_lib/gemini/mavlink_msg_motor_tm.h
+++ b/mavlink_lib/gemini/mavlink_msg_motor_tm.h
@@ -10,17 +10,19 @@ 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 main_valve_state; /*< 1 If the main 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 34
+#define MAVLINK_MSG_ID_MOTOR_TM_MIN_LEN 34
+#define MAVLINK_MSG_ID_213_LEN 34
+#define MAVLINK_MSG_ID_213_MIN_LEN 34
-#define MAVLINK_MSG_ID_MOTOR_TM_CRC 241
-#define MAVLINK_MSG_ID_213_CRC 241
+#define MAVLINK_MSG_ID_MOTOR_TM_CRC 196
+#define MAVLINK_MSG_ID_213_CRC 196
@@ -28,27 +30,31 @@ typedef struct __mavlink_motor_tm_t {
#define MAVLINK_MESSAGE_INFO_MOTOR_TM { \
213, \
"MOTOR_TM", \
- 7, \
+ 9, \
{ { "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) }, \
+ { "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, \
+ 9, \
{ { "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) }, \
+ { "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
@@ -65,11 +71,13 @@ typedef struct __mavlink_motor_tm_t {
* @param combustion_chamber_pressure [Bar] Pressure inside the combustion chamber used for automatic shutdown
* @param floating_level Floating level in tank
* @param tank_temperature Tank temperature
- * @param main_valve_state 1 If the main valve is open
+ * @param main_valve_state 1 If the main 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, float battery_voltage, float current_consumption)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char buf[MAVLINK_MSG_ID_MOTOR_TM_LEN];
@@ -78,8 +86,10 @@ 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);
memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_MOTOR_TM_LEN);
#else
@@ -89,6 +99,8 @@ 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;
@@ -111,12 +123,14 @@ static inline uint16_t mavlink_msg_motor_tm_pack(uint8_t system_id, uint8_t comp
* @param combustion_chamber_pressure [Bar] Pressure inside the combustion chamber used for automatic shutdown
* @param floating_level Floating level in tank
* @param tank_temperature Tank temperature
- * @param main_valve_state 1 If the main valve is open
+ * @param main_valve_state 1 If the main 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,float battery_voltage,float current_consumption)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char buf[MAVLINK_MSG_ID_MOTOR_TM_LEN];
@@ -125,8 +139,10 @@ 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);
memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_MOTOR_TM_LEN);
#else
@@ -136,6 +152,8 @@ 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;
@@ -156,7 +174,7 @@ 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->battery_voltage, motor_tm->current_consumption);
}
/**
@@ -170,7 +188,7 @@ 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->battery_voltage, motor_tm->current_consumption);
}
/**
@@ -183,11 +201,13 @@ static inline uint16_t mavlink_msg_motor_tm_encode_chan(uint8_t system_id, uint8
* @param combustion_chamber_pressure [Bar] Pressure inside the combustion chamber used for automatic shutdown
* @param floating_level Floating level in tank
* @param tank_temperature Tank temperature
- * @param main_valve_state 1 If the main valve is open
+ * @param main_valve_state 1 If the main 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, float battery_voltage, float current_consumption)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char buf[MAVLINK_MSG_ID_MOTOR_TM_LEN];
@@ -196,8 +216,10 @@ 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_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
@@ -207,6 +229,8 @@ 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;
@@ -222,7 +246,7 @@ 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->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 +260,7 @@ 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, float battery_voltage, float current_consumption)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char *buf = (char *)msgbuf;
@@ -245,8 +269,10 @@ 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_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
@@ -256,6 +282,8 @@ 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;
@@ -316,7 +344,7 @@ 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);
}
/**
@@ -332,11 +360,31 @@ static inline float mavlink_msg_motor_tm_get_tank_temperature(const mavlink_mess
/**
* @brief Get field main_valve_state from motor_tm message
*
- * @return 1 If the main valve is open
+ * @return 1 If the main valve is open
*/
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 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);
}
/**
@@ -353,6 +401,8 @@ 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);
#else
diff --git a/mavlink_lib/gemini/mavlink_msg_payload_flight_tm.h b/mavlink_lib/gemini/mavlink_msg_payload_flight_tm.h
index f68e04122267929b30941d865e5f6860c9bef31a..ae98a6d0783f07377a58995ba4861a86d39e9c22 100644
--- a/mavlink_lib/gemini/mavlink_msg_payload_flight_tm.h
+++ b/mavlink_lib/gemini/mavlink_msg_payload_flight_tm.h
@@ -39,7 +39,8 @@ 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 battery_voltage; /*< [V] Battery voltage*/
+ float current_consumption; /*< [A] Battery current*/
float vsupply_5v; /*< [V] Power supply 5V*/
float temperature; /*< [degC] Temperature*/
uint8_t fmm_state; /*< Flight Mode Manager State*/
@@ -50,13 +51,13 @@ typedef struct __mavlink_payload_flight_tm_t {
int8_t logger_error; /*< Logger error (0 = no error)*/
} mavlink_payload_flight_tm_t;
-#define MAVLINK_MSG_ID_PAYLOAD_FLIGHT_TM_LEN 158
-#define MAVLINK_MSG_ID_PAYLOAD_FLIGHT_TM_MIN_LEN 158
-#define MAVLINK_MSG_ID_209_LEN 158
-#define MAVLINK_MSG_ID_209_MIN_LEN 158
+#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_CRC 229
-#define MAVLINK_MSG_ID_209_CRC 229
+#define MAVLINK_MSG_ID_PAYLOAD_FLIGHT_TM_CRC 117
+#define MAVLINK_MSG_ID_209_CRC 117
@@ -64,11 +65,11 @@ typedef struct __mavlink_payload_flight_tm_t {
#define MAVLINK_MESSAGE_INFO_PAYLOAD_FLIGHT_TM { \
209, \
"PAYLOAD_FLIGHT_TM", \
- 43, \
+ 44, \
{ { "timestamp", NULL, MAVLINK_TYPE_UINT64_T, 0, 0, offsetof(mavlink_payload_flight_tm_t, timestamp) }, \
- { "fmm_state", NULL, MAVLINK_TYPE_UINT8_T, 0, 152, offsetof(mavlink_payload_flight_tm_t, fmm_state) }, \
- { "nas_state", NULL, MAVLINK_TYPE_UINT8_T, 0, 153, offsetof(mavlink_payload_flight_tm_t, nas_state) }, \
- { "wes_state", NULL, MAVLINK_TYPE_UINT8_T, 0, 154, offsetof(mavlink_payload_flight_tm_t, wes_state) }, \
+ { "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) }, \
{ "airspeed_pitot", NULL, MAVLINK_TYPE_FLOAT, 0, 16, offsetof(mavlink_payload_flight_tm_t, airspeed_pitot) }, \
@@ -82,7 +83,7 @@ typedef struct __mavlink_payload_flight_tm_t {
{ "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, 155, offsetof(mavlink_payload_flight_tm_t, gps_fix) }, \
+ { "gps_fix", NULL, MAVLINK_TYPE_UINT8_T, 0, 159, offsetof(mavlink_payload_flight_tm_t, gps_fix) }, \
{ "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) }, \
@@ -103,21 +104,22 @@ typedef struct __mavlink_payload_flight_tm_t {
{ "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, 156, offsetof(mavlink_payload_flight_tm_t, pin_nosecone) }, \
- { "vbat", NULL, MAVLINK_TYPE_FLOAT, 0, 140, offsetof(mavlink_payload_flight_tm_t, vbat) }, \
- { "vsupply_5v", NULL, MAVLINK_TYPE_FLOAT, 0, 144, offsetof(mavlink_payload_flight_tm_t, vsupply_5v) }, \
- { "temperature", NULL, MAVLINK_TYPE_FLOAT, 0, 148, offsetof(mavlink_payload_flight_tm_t, temperature) }, \
- { "logger_error", NULL, MAVLINK_TYPE_INT8_T, 0, 157, offsetof(mavlink_payload_flight_tm_t, logger_error) }, \
+ { "pin_nosecone", NULL, MAVLINK_TYPE_UINT8_T, 0, 160, offsetof(mavlink_payload_flight_tm_t, pin_nosecone) }, \
+ { "battery_voltage", NULL, MAVLINK_TYPE_FLOAT, 0, 140, offsetof(mavlink_payload_flight_tm_t, battery_voltage) }, \
+ { "current_consumption", NULL, MAVLINK_TYPE_FLOAT, 0, 144, offsetof(mavlink_payload_flight_tm_t, current_consumption) }, \
+ { "vsupply_5v", NULL, MAVLINK_TYPE_FLOAT, 0, 148, offsetof(mavlink_payload_flight_tm_t, vsupply_5v) }, \
+ { "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) }, \
} \
}
#else
#define MAVLINK_MESSAGE_INFO_PAYLOAD_FLIGHT_TM { \
"PAYLOAD_FLIGHT_TM", \
- 43, \
+ 44, \
{ { "timestamp", NULL, MAVLINK_TYPE_UINT64_T, 0, 0, offsetof(mavlink_payload_flight_tm_t, timestamp) }, \
- { "fmm_state", NULL, MAVLINK_TYPE_UINT8_T, 0, 152, offsetof(mavlink_payload_flight_tm_t, fmm_state) }, \
- { "nas_state", NULL, MAVLINK_TYPE_UINT8_T, 0, 153, offsetof(mavlink_payload_flight_tm_t, nas_state) }, \
- { "wes_state", NULL, MAVLINK_TYPE_UINT8_T, 0, 154, offsetof(mavlink_payload_flight_tm_t, wes_state) }, \
+ { "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) }, \
{ "airspeed_pitot", NULL, MAVLINK_TYPE_FLOAT, 0, 16, offsetof(mavlink_payload_flight_tm_t, airspeed_pitot) }, \
@@ -131,7 +133,7 @@ typedef struct __mavlink_payload_flight_tm_t {
{ "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, 155, offsetof(mavlink_payload_flight_tm_t, gps_fix) }, \
+ { "gps_fix", NULL, MAVLINK_TYPE_UINT8_T, 0, 159, offsetof(mavlink_payload_flight_tm_t, gps_fix) }, \
{ "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) }, \
@@ -152,11 +154,12 @@ typedef struct __mavlink_payload_flight_tm_t {
{ "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, 156, offsetof(mavlink_payload_flight_tm_t, pin_nosecone) }, \
- { "vbat", NULL, MAVLINK_TYPE_FLOAT, 0, 140, offsetof(mavlink_payload_flight_tm_t, vbat) }, \
- { "vsupply_5v", NULL, MAVLINK_TYPE_FLOAT, 0, 144, offsetof(mavlink_payload_flight_tm_t, vsupply_5v) }, \
- { "temperature", NULL, MAVLINK_TYPE_FLOAT, 0, 148, offsetof(mavlink_payload_flight_tm_t, temperature) }, \
- { "logger_error", NULL, MAVLINK_TYPE_INT8_T, 0, 157, offsetof(mavlink_payload_flight_tm_t, logger_error) }, \
+ { "pin_nosecone", NULL, MAVLINK_TYPE_UINT8_T, 0, 160, offsetof(mavlink_payload_flight_tm_t, pin_nosecone) }, \
+ { "battery_voltage", NULL, MAVLINK_TYPE_FLOAT, 0, 140, offsetof(mavlink_payload_flight_tm_t, battery_voltage) }, \
+ { "current_consumption", NULL, MAVLINK_TYPE_FLOAT, 0, 144, offsetof(mavlink_payload_flight_tm_t, current_consumption) }, \
+ { "vsupply_5v", NULL, MAVLINK_TYPE_FLOAT, 0, 148, offsetof(mavlink_payload_flight_tm_t, vsupply_5v) }, \
+ { "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) }, \
} \
}
#endif
@@ -206,14 +209,15 @@ 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 battery_voltage [V] Battery voltage
+ * @param current_consumption [A] Battery current
* @param vsupply_5v [V] Power supply 5V
* @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 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 current_consumption, float vsupply_5v, float temperature, int8_t logger_error)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char buf[MAVLINK_MSG_ID_PAYLOAD_FLIGHT_TM_LEN];
@@ -251,15 +255,16 @@ static inline uint16_t mavlink_msg_payload_flight_tm_pack(uint8_t system_id, uin
_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, vbat);
- _mav_put_float(buf, 144, vsupply_5v);
- _mav_put_float(buf, 148, temperature);
- _mav_put_uint8_t(buf, 152, fmm_state);
- _mav_put_uint8_t(buf, 153, nas_state);
- _mav_put_uint8_t(buf, 154, wes_state);
- _mav_put_uint8_t(buf, 155, gps_fix);
- _mav_put_uint8_t(buf, 156, pin_nosecone);
- _mav_put_int8_t(buf, 157, logger_error);
+ _mav_put_float(buf, 140, battery_voltage);
+ _mav_put_float(buf, 144, current_consumption);
+ _mav_put_float(buf, 148, vsupply_5v);
+ _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);
memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_PAYLOAD_FLIGHT_TM_LEN);
#else
@@ -298,7 +303,8 @@ 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.battery_voltage = battery_voltage;
+ packet.current_consumption = current_consumption;
packet.vsupply_5v = vsupply_5v;
packet.temperature = temperature;
packet.fmm_state = fmm_state;
@@ -360,7 +366,8 @@ 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 battery_voltage [V] Battery voltage
+ * @param current_consumption [A] Battery current
* @param vsupply_5v [V] Power supply 5V
* @param temperature [degC] Temperature
* @param logger_error Logger error (0 = no error)
@@ -368,7 +375,7 @@ static inline uint16_t mavlink_msg_payload_flight_tm_pack(uint8_t system_id, uin
*/
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 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 current_consumption,float vsupply_5v,float temperature,int8_t logger_error)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char buf[MAVLINK_MSG_ID_PAYLOAD_FLIGHT_TM_LEN];
@@ -406,15 +413,16 @@ static inline uint16_t mavlink_msg_payload_flight_tm_pack_chan(uint8_t system_id
_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, vbat);
- _mav_put_float(buf, 144, vsupply_5v);
- _mav_put_float(buf, 148, temperature);
- _mav_put_uint8_t(buf, 152, fmm_state);
- _mav_put_uint8_t(buf, 153, nas_state);
- _mav_put_uint8_t(buf, 154, wes_state);
- _mav_put_uint8_t(buf, 155, gps_fix);
- _mav_put_uint8_t(buf, 156, pin_nosecone);
- _mav_put_int8_t(buf, 157, logger_error);
+ _mav_put_float(buf, 140, battery_voltage);
+ _mav_put_float(buf, 144, current_consumption);
+ _mav_put_float(buf, 148, vsupply_5v);
+ _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);
memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_PAYLOAD_FLIGHT_TM_LEN);
#else
@@ -453,7 +461,8 @@ 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.battery_voltage = battery_voltage;
+ packet.current_consumption = current_consumption;
packet.vsupply_5v = vsupply_5v;
packet.temperature = temperature;
packet.fmm_state = fmm_state;
@@ -480,7 +489,7 @@ 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->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->current_consumption, payload_flight_tm->vsupply_5v, payload_flight_tm->temperature, payload_flight_tm->logger_error);
}
/**
@@ -494,7 +503,7 @@ 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->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->current_consumption, payload_flight_tm->vsupply_5v, payload_flight_tm->temperature, payload_flight_tm->logger_error);
}
/**
@@ -540,14 +549,15 @@ 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 battery_voltage [V] Battery voltage
+ * @param current_consumption [A] Battery current
* @param vsupply_5v [V] Power supply 5V
* @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 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 current_consumption, float vsupply_5v, float temperature, int8_t logger_error)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char buf[MAVLINK_MSG_ID_PAYLOAD_FLIGHT_TM_LEN];
@@ -585,15 +595,16 @@ static inline void mavlink_msg_payload_flight_tm_send(mavlink_channel_t chan, ui
_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, vbat);
- _mav_put_float(buf, 144, vsupply_5v);
- _mav_put_float(buf, 148, temperature);
- _mav_put_uint8_t(buf, 152, fmm_state);
- _mav_put_uint8_t(buf, 153, nas_state);
- _mav_put_uint8_t(buf, 154, wes_state);
- _mav_put_uint8_t(buf, 155, gps_fix);
- _mav_put_uint8_t(buf, 156, pin_nosecone);
- _mav_put_int8_t(buf, 157, logger_error);
+ _mav_put_float(buf, 140, battery_voltage);
+ _mav_put_float(buf, 144, current_consumption);
+ _mav_put_float(buf, 148, vsupply_5v);
+ _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_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
@@ -632,7 +643,8 @@ 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.battery_voltage = battery_voltage;
+ packet.current_consumption = current_consumption;
packet.vsupply_5v = vsupply_5v;
packet.temperature = temperature;
packet.fmm_state = fmm_state;
@@ -654,7 +666,7 @@ 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->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->current_consumption, payload_flight_tm->vsupply_5v, 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
@@ -668,7 +680,7 @@ 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 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 current_consumption, float vsupply_5v, float temperature, int8_t logger_error)
{
#if MAVLINK_NEED_BYTE_SWAP || !MAVLINK_ALIGNED_FIELDS
char *buf = (char *)msgbuf;
@@ -706,15 +718,16 @@ static inline void mavlink_msg_payload_flight_tm_send_buf(mavlink_message_t *msg
_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, vbat);
- _mav_put_float(buf, 144, vsupply_5v);
- _mav_put_float(buf, 148, temperature);
- _mav_put_uint8_t(buf, 152, fmm_state);
- _mav_put_uint8_t(buf, 153, nas_state);
- _mav_put_uint8_t(buf, 154, wes_state);
- _mav_put_uint8_t(buf, 155, gps_fix);
- _mav_put_uint8_t(buf, 156, pin_nosecone);
- _mav_put_int8_t(buf, 157, logger_error);
+ _mav_put_float(buf, 140, battery_voltage);
+ _mav_put_float(buf, 144, current_consumption);
+ _mav_put_float(buf, 148, vsupply_5v);
+ _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_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
@@ -753,7 +766,8 @@ 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->battery_voltage = battery_voltage;
+ packet->current_consumption = current_consumption;
packet->vsupply_5v = vsupply_5v;
packet->temperature = temperature;
packet->fmm_state = fmm_state;
@@ -790,7 +804,7 @@ static inline uint64_t mavlink_msg_payload_flight_tm_get_timestamp(const mavlink
*/
static inline uint8_t mavlink_msg_payload_flight_tm_get_fmm_state(const mavlink_message_t* msg)
{
- return _MAV_RETURN_uint8_t(msg, 152);
+ return _MAV_RETURN_uint8_t(msg, 156);
}
/**
@@ -800,7 +814,7 @@ static inline uint8_t mavlink_msg_payload_flight_tm_get_fmm_state(const mavlink_
*/
static inline uint8_t mavlink_msg_payload_flight_tm_get_nas_state(const mavlink_message_t* msg)
{
- return _MAV_RETURN_uint8_t(msg, 153);
+ return _MAV_RETURN_uint8_t(msg, 157);
}
/**
@@ -810,7 +824,7 @@ static inline uint8_t mavlink_msg_payload_flight_tm_get_nas_state(const mavlink_
*/
static inline uint8_t mavlink_msg_payload_flight_tm_get_wes_state(const mavlink_message_t* msg)
{
- return _MAV_RETURN_uint8_t(msg, 154);
+ return _MAV_RETURN_uint8_t(msg, 158);
}
/**
@@ -950,7 +964,7 @@ static inline float mavlink_msg_payload_flight_tm_get_mag_z(const mavlink_messag
*/
static inline uint8_t mavlink_msg_payload_flight_tm_get_gps_fix(const mavlink_message_t* msg)
{
- return _MAV_RETURN_uint8_t(msg, 155);
+ return _MAV_RETURN_uint8_t(msg, 159);
}
/**
@@ -1160,19 +1174,29 @@ static inline float mavlink_msg_payload_flight_tm_get_wes_e(const mavlink_messag
*/
static inline uint8_t mavlink_msg_payload_flight_tm_get_pin_nosecone(const mavlink_message_t* msg)
{
- return _MAV_RETURN_uint8_t(msg, 156);
+ return _MAV_RETURN_uint8_t(msg, 160);
}
/**
- * @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 current_consumption from payload_flight_tm message
+ *
+ * @return [A] Battery current
+ */
+static inline float mavlink_msg_payload_flight_tm_get_current_consumption(const mavlink_message_t* msg)
+{
+ return _MAV_RETURN_float(msg, 144);
+}
+
/**
* @brief Get field vsupply_5v from payload_flight_tm message
*
@@ -1180,7 +1204,7 @@ static inline float mavlink_msg_payload_flight_tm_get_vbat(const mavlink_message
*/
static inline float mavlink_msg_payload_flight_tm_get_vsupply_5v(const mavlink_message_t* msg)
{
- return _MAV_RETURN_float(msg, 144);
+ return _MAV_RETURN_float(msg, 148);
}
/**
@@ -1190,7 +1214,7 @@ static inline float mavlink_msg_payload_flight_tm_get_vsupply_5v(const mavlink_m
*/
static inline float mavlink_msg_payload_flight_tm_get_temperature(const mavlink_message_t* msg)
{
- return _MAV_RETURN_float(msg, 148);
+ return _MAV_RETURN_float(msg, 152);
}
/**
@@ -1200,7 +1224,7 @@ 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, 157);
+ return _MAV_RETURN_int8_t(msg, 161);
}
/**
@@ -1246,7 +1270,8 @@ 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->battery_voltage = mavlink_msg_payload_flight_tm_get_battery_voltage(msg);
+ payload_flight_tm->current_consumption = mavlink_msg_payload_flight_tm_get_current_consumption(msg);
payload_flight_tm->vsupply_5v = mavlink_msg_payload_flight_tm_get_vsupply_5v(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);
diff --git a/mavlink_lib/gemini/mavlink_msg_rocket_flight_tm.h b/mavlink_lib/gemini/mavlink_msg_rocket_flight_tm.h
index 953906c964b8e081277504f3be7600769eb79591..f5194aa57b65c88c02c5672cb0a8db41de6c9034 100644
--- a/mavlink_lib/gemini/mavlink_msg_rocket_flight_tm.h
+++ b/mavlink_lib/gemini/mavlink_msg_rocket_flight_tm.h
@@ -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 +40,15 @@ 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 battery_voltage; /*< [V] 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 +57,13 @@ 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 168
+#define MAVLINK_MSG_ID_ROCKET_FLIGHT_TM_MIN_LEN 168
+#define MAVLINK_MSG_ID_208_LEN 168
+#define MAVLINK_MSG_ID_208_MIN_LEN 168
-#define MAVLINK_MSG_ID_ROCKET_FLIGHT_TM_CRC 141
-#define MAVLINK_MSG_ID_208_CRC 141
+#define MAVLINK_MSG_ID_ROCKET_FLIGHT_TM_CRC 254
+#define MAVLINK_MSG_ID_208_CRC 254
@@ -73,11 +73,12 @@ typedef struct __mavlink_rocket_flight_tm_t {
"ROCKET_FLIGHT_TM", \
50, \
{ { "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, 156, offsetof(mavlink_rocket_flight_tm_t, ada_state) }, \
+ { "fmm_state", NULL, MAVLINK_TYPE_UINT8_T, 0, 157, offsetof(mavlink_rocket_flight_tm_t, fmm_state) }, \
+ { "dpl_state", NULL, MAVLINK_TYPE_UINT8_T, 0, 158, offsetof(mavlink_rocket_flight_tm_t, dpl_state) }, \
+ { "abk_state", NULL, MAVLINK_TYPE_UINT8_T, 0, 159, offsetof(mavlink_rocket_flight_tm_t, abk_state) }, \
+ { "nas_state", NULL, MAVLINK_TYPE_UINT8_T, 0, 160, offsetof(mavlink_rocket_flight_tm_t, nas_state) }, \
+ { "mea_state", NULL, MAVLINK_TYPE_UINT8_T, 0, 161, 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) }, \
@@ -85,43 +86,42 @@ 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, 162, 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_launch", NULL, MAVLINK_TYPE_UINT8_T, 0, 163, offsetof(mavlink_rocket_flight_tm_t, pin_launch) }, \
+ { "pin_nosecone", NULL, MAVLINK_TYPE_UINT8_T, 0, 164, offsetof(mavlink_rocket_flight_tm_t, pin_nosecone) }, \
+ { "pin_expulsion", NULL, MAVLINK_TYPE_UINT8_T, 0, 165, offsetof(mavlink_rocket_flight_tm_t, pin_expulsion) }, \
+ { "cutter_presence", NULL, MAVLINK_TYPE_UINT8_T, 0, 166, offsetof(mavlink_rocket_flight_tm_t, cutter_presence) }, \
+ { "battery_voltage", NULL, MAVLINK_TYPE_FLOAT, 0, 144, offsetof(mavlink_rocket_flight_tm_t, battery_voltage) }, \
+ { "current_consumption", NULL, MAVLINK_TYPE_FLOAT, 0, 148, offsetof(mavlink_rocket_flight_tm_t, current_consumption) }, \
+ { "temperature", NULL, MAVLINK_TYPE_FLOAT, 0, 152, offsetof(mavlink_rocket_flight_tm_t, temperature) }, \
+ { "logger_error", NULL, MAVLINK_TYPE_INT8_T, 0, 167, offsetof(mavlink_rocket_flight_tm_t, logger_error) }, \
} \
}
#else
@@ -129,11 +129,12 @@ typedef struct __mavlink_rocket_flight_tm_t {
"ROCKET_FLIGHT_TM", \
50, \
{ { "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, 156, offsetof(mavlink_rocket_flight_tm_t, ada_state) }, \
+ { "fmm_state", NULL, MAVLINK_TYPE_UINT8_T, 0, 157, offsetof(mavlink_rocket_flight_tm_t, fmm_state) }, \
+ { "dpl_state", NULL, MAVLINK_TYPE_UINT8_T, 0, 158, offsetof(mavlink_rocket_flight_tm_t, dpl_state) }, \
+ { "abk_state", NULL, MAVLINK_TYPE_UINT8_T, 0, 159, offsetof(mavlink_rocket_flight_tm_t, abk_state) }, \
+ { "nas_state", NULL, MAVLINK_TYPE_UINT8_T, 0, 160, offsetof(mavlink_rocket_flight_tm_t, nas_state) }, \
+ { "mea_state", NULL, MAVLINK_TYPE_UINT8_T, 0, 161, 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 +142,42 @@ 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, 162, 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_launch", NULL, MAVLINK_TYPE_UINT8_T, 0, 163, offsetof(mavlink_rocket_flight_tm_t, pin_launch) }, \
+ { "pin_nosecone", NULL, MAVLINK_TYPE_UINT8_T, 0, 164, offsetof(mavlink_rocket_flight_tm_t, pin_nosecone) }, \
+ { "pin_expulsion", NULL, MAVLINK_TYPE_UINT8_T, 0, 165, offsetof(mavlink_rocket_flight_tm_t, pin_expulsion) }, \
+ { "cutter_presence", NULL, MAVLINK_TYPE_UINT8_T, 0, 166, offsetof(mavlink_rocket_flight_tm_t, cutter_presence) }, \
+ { "battery_voltage", NULL, MAVLINK_TYPE_FLOAT, 0, 144, offsetof(mavlink_rocket_flight_tm_t, battery_voltage) }, \
+ { "current_consumption", NULL, MAVLINK_TYPE_FLOAT, 0, 148, offsetof(mavlink_rocket_flight_tm_t, current_consumption) }, \
+ { "temperature", NULL, MAVLINK_TYPE_FLOAT, 0, 152, offsetof(mavlink_rocket_flight_tm_t, temperature) }, \
+ { "logger_error", NULL, MAVLINK_TYPE_INT8_T, 0, 167, offsetof(mavlink_rocket_flight_tm_t, logger_error) }, \
} \
}
#endif
@@ -194,6 +194,7 @@ 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 +202,7 @@ 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 +217,6 @@ 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
@@ -234,14 +234,14 @@ typedef struct __mavlink_rocket_flight_tm_t {
* @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 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, uint8_t pin_launch, uint8_t pin_nosecone, uint8_t pin_expulsion, uint8_t cutter_presence, float 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 +253,48 @@ 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, battery_voltage);
+ _mav_put_float(buf, 148, current_consumption);
+ _mav_put_float(buf, 152, temperature);
+ _mav_put_uint8_t(buf, 156, ada_state);
+ _mav_put_uint8_t(buf, 157, fmm_state);
+ _mav_put_uint8_t(buf, 158, dpl_state);
+ _mav_put_uint8_t(buf, 159, abk_state);
+ _mav_put_uint8_t(buf, 160, nas_state);
+ _mav_put_uint8_t(buf, 161, mea_state);
+ _mav_put_uint8_t(buf, 162, gps_fix);
+ _mav_put_uint8_t(buf, 163, pin_launch);
+ _mav_put_uint8_t(buf, 164, pin_nosecone);
+ _mav_put_uint8_t(buf, 165, pin_expulsion);
+ _mav_put_uint8_t(buf, 166, cutter_presence);
+ _mav_put_int8_t(buf, 167, logger_error);
memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_ROCKET_FLIGHT_TM_LEN);
#else
@@ -307,6 +307,7 @@ 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 +321,6 @@ 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 +334,15 @@ 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.battery_voltage = 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 +369,7 @@ 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 +377,7 @@ 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 +392,6 @@ 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
@@ -409,15 +409,15 @@ static inline uint16_t mavlink_msg_rocket_flight_tm_pack(uint8_t system_id, uint
* @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 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,uint8_t pin_launch,uint8_t pin_nosecone,uint8_t pin_expulsion,uint8_t cutter_presence,float 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 +429,48 @@ 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, battery_voltage);
+ _mav_put_float(buf, 148, current_consumption);
+ _mav_put_float(buf, 152, temperature);
+ _mav_put_uint8_t(buf, 156, ada_state);
+ _mav_put_uint8_t(buf, 157, fmm_state);
+ _mav_put_uint8_t(buf, 158, dpl_state);
+ _mav_put_uint8_t(buf, 159, abk_state);
+ _mav_put_uint8_t(buf, 160, nas_state);
+ _mav_put_uint8_t(buf, 161, mea_state);
+ _mav_put_uint8_t(buf, 162, gps_fix);
+ _mav_put_uint8_t(buf, 163, pin_launch);
+ _mav_put_uint8_t(buf, 164, pin_nosecone);
+ _mav_put_uint8_t(buf, 165, pin_expulsion);
+ _mav_put_uint8_t(buf, 166, cutter_presence);
+ _mav_put_int8_t(buf, 167, logger_error);
memcpy(_MAV_PAYLOAD_NON_CONST(msg), buf, MAVLINK_MSG_ID_ROCKET_FLIGHT_TM_LEN);
#else
@@ -483,6 +483,7 @@ 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 +497,6 @@ 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 +510,15 @@ 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.battery_voltage = 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 +543,7 @@ 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_launch, rocket_flight_tm->pin_nosecone, rocket_flight_tm->pin_expulsion, rocket_flight_tm->cutter_presence, rocket_flight_tm->battery_voltage, rocket_flight_tm->current_consumption, rocket_flight_tm->temperature, rocket_flight_tm->logger_error);
}
/**
@@ -557,7 +557,7 @@ 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_launch, rocket_flight_tm->pin_nosecone, rocket_flight_tm->pin_expulsion, rocket_flight_tm->cutter_presence, rocket_flight_tm->battery_voltage, rocket_flight_tm->current_consumption, rocket_flight_tm->temperature, rocket_flight_tm->logger_error);
}
/**
@@ -570,6 +570,7 @@ 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 +578,7 @@ 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 +593,6 @@ 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
@@ -610,14 +610,14 @@ static inline uint16_t mavlink_msg_rocket_flight_tm_encode_chan(uint8_t system_i
* @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 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, uint8_t pin_launch, uint8_t pin_nosecone, uint8_t pin_expulsion, uint8_t cutter_presence, float 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 +629,48 @@ 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, battery_voltage);
+ _mav_put_float(buf, 148, current_consumption);
+ _mav_put_float(buf, 152, temperature);
+ _mav_put_uint8_t(buf, 156, ada_state);
+ _mav_put_uint8_t(buf, 157, fmm_state);
+ _mav_put_uint8_t(buf, 158, dpl_state);
+ _mav_put_uint8_t(buf, 159, abk_state);
+ _mav_put_uint8_t(buf, 160, nas_state);
+ _mav_put_uint8_t(buf, 161, mea_state);
+ _mav_put_uint8_t(buf, 162, gps_fix);
+ _mav_put_uint8_t(buf, 163, pin_launch);
+ _mav_put_uint8_t(buf, 164, pin_nosecone);
+ _mav_put_uint8_t(buf, 165, pin_expulsion);
+ _mav_put_uint8_t(buf, 166, cutter_presence);
+ _mav_put_int8_t(buf, 167, 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 +683,7 @@ 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 +697,6 @@ 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 +710,15 @@ 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.battery_voltage = 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 +738,7 @@ 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_launch, rocket_flight_tm->pin_nosecone, rocket_flight_tm->pin_expulsion, rocket_flight_tm->cutter_presence, rocket_flight_tm->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 +752,7 @@ 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, uint8_t pin_launch, uint8_t pin_nosecone, uint8_t pin_expulsion, uint8_t cutter_presence, float 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 +764,48 @@ 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, battery_voltage);
+ _mav_put_float(buf, 148, current_consumption);
+ _mav_put_float(buf, 152, temperature);
+ _mav_put_uint8_t(buf, 156, ada_state);
+ _mav_put_uint8_t(buf, 157, fmm_state);
+ _mav_put_uint8_t(buf, 158, dpl_state);
+ _mav_put_uint8_t(buf, 159, abk_state);
+ _mav_put_uint8_t(buf, 160, nas_state);
+ _mav_put_uint8_t(buf, 161, mea_state);
+ _mav_put_uint8_t(buf, 162, gps_fix);
+ _mav_put_uint8_t(buf, 163, pin_launch);
+ _mav_put_uint8_t(buf, 164, pin_nosecone);
+ _mav_put_uint8_t(buf, 165, pin_expulsion);
+ _mav_put_uint8_t(buf, 166, cutter_presence);
+ _mav_put_int8_t(buf, 167, 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 +818,7 @@ 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 +832,6 @@ 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 +845,15 @@ 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->battery_voltage = 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 +888,7 @@ 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, 156);
}
/**
@@ -898,7 +898,7 @@ 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, 157);
}
/**
@@ -908,7 +908,7 @@ 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, 158);
}
/**
@@ -918,7 +918,7 @@ 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, 159);
}
/**
@@ -928,7 +928,17 @@ 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, 160);
+}
+
+/**
+ * @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, 161);
}
/**
@@ -1001,6 +1011,16 @@ 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 +1028,7 @@ 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 +1038,7 @@ 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 +1048,7 @@ 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 +1058,7 @@ 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 +1068,7 @@ 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 +1078,7 @@ 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 +1088,7 @@ 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 +1098,7 @@ 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 +1108,7 @@ 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 +1118,7 @@ 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, 162);
}
/**
@@ -1108,7 +1128,7 @@ 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 +1138,7 @@ 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 +1148,7 @@ 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 +1157,10 @@ 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 +1168,7 @@ 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 +1178,7 @@ 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 +1188,7 @@ 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 +1198,7 @@ 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 +1208,7 @@ 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 +1218,7 @@ 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 +1228,7 @@ 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 +1238,7 @@ 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 +1248,7 @@ 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 +1258,7 @@ 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 +1268,7 @@ 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 +1278,7 @@ 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);
}
/**
@@ -1288,7 +1288,7 @@ static inline float mavlink_msg_rocket_flight_tm_get_nas_bias_y(const mavlink_me
*/
static inline float mavlink_msg_rocket_flight_tm_get_nas_bias_z(const mavlink_message_t* msg)
{
- return _MAV_RETURN_float(msg, 144);
+ return _MAV_RETURN_float(msg, 140);
}
/**
@@ -1298,7 +1298,7 @@ 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, 163);
}
/**
@@ -1308,7 +1308,7 @@ 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, 164);
}
/**
@@ -1318,7 +1318,7 @@ 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, 165);
}
/**
@@ -1328,27 +1328,27 @@ 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, 166);
}
/**
- * @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);
+ return _MAV_RETURN_float(msg, 144);
}
/**
- * @brief Get field vbat from rocket_flight_tm message
+ * @brief Get field current_consumption from rocket_flight_tm message
*
- * @return [V] Battery voltage
+ * @return [A] Battery current
*/
-static inline float mavlink_msg_rocket_flight_tm_get_vbat(const mavlink_message_t* msg)
+static inline float mavlink_msg_rocket_flight_tm_get_current_consumption(const mavlink_message_t* msg)
{
- return _MAV_RETURN_float(msg, 152);
+ return _MAV_RETURN_float(msg, 148);
}
/**
@@ -1358,7 +1358,7 @@ 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, 152);
}
/**
@@ -1368,7 +1368,7 @@ 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, 167);
}
/**
@@ -1388,6 +1388,7 @@ 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 +1402,6 @@ 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 +1415,15 @@ 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->battery_voltage = mavlink_msg_rocket_flight_tm_get_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);
diff --git a/mavlink_lib/gemini/testsuite.h b/mavlink_lib/gemini/testsuite.h
index 1e8930dd99b1ae3a60bd73487f544cde99bb5df1..f6c6fed37b01d2d522fdf7e08ec46cc5d6f995d6 100644
--- a/mavlink_lib/gemini/testsuite.h
+++ b/mavlink_lib/gemini/testsuite.h
@@ -2655,6 +2655,71 @@ static void mavlink_test_nas_tm(uint8_t system_id, uint8_t component_id, mavlink
#endif
}
+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_MEA_TM >= 256) {
+ return;
+ }
+#endif
+ mavlink_message_t msg;
+ uint8_t buffer[MAVLINK_MAX_PACKET_LEN];
+ uint16_t i;
+ mavlink_mea_tm_t packet_in = {
+ 93372036854775807ULL,73.0,101.0,129.0,157.0,185.0,89
+ };
+ mavlink_mea_tm_t packet1, packet2;
+ memset(&packet1, 0, sizeof(packet1));
+ packet1.timestamp = packet_in.timestamp;
+ 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_MEA_TM_MIN_LEN + (char *)&packet1, 0, sizeof(packet1)-MAVLINK_MSG_ID_MEA_TM_MIN_LEN);
+ }
+#endif
+ memset(&packet2, 0, sizeof(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_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_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));
+ mavlink_msg_to_send_buffer(buffer, &msg);
+ for (i=0; i<mavlink_msg_get_send_buffer_length(&msg); i++) {
+ comm_send_ch(MAVLINK_COMM_0, buffer[i]);
+ }
+ mavlink_msg_mea_tm_decode(last_msg, &packet2);
+ MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0);
+
+ memset(&packet2, 0, sizeof(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("MEA_TM") != NULL);
+ MAVLINK_ASSERT(mavlink_get_message_info_by_id(MAVLINK_MSG_ID_MEA_TM) != NULL);
+#endif
+}
+
static void mavlink_test_rocket_flight_tm(uint8_t system_id, uint8_t component_id, mavlink_message_t *last_msg)
{
#ifdef MAVLINK_STATUS_FLAG_OUT_MAVLINK1
@@ -2667,7 +2732,7 @@ 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,73.0,101.0,129.0,157.0,185.0,213.0,241.0,269.0,297.0,325.0,353.0,381.0,409.0,437.0,465.0,493.0,521.0,549.0,577.0,605.0,633.0,661.0,689.0,717.0,745.0,773.0,801.0,829.0,857.0,885.0,913.0,941.0,969.0,997.0,1025.0,1053.0,1081.0,217,28,95,162,229,40,107,174,241,52,119,186
};
mavlink_rocket_flight_tm_t packet1, packet2;
memset(&packet1, 0, sizeof(packet1));
@@ -2679,6 +2744,7 @@ 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;
@@ -2692,8 +2758,6 @@ 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;
@@ -2707,14 +2771,15 @@ 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.battery_voltage = packet_in.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;
@@ -2735,12 +2800,12 @@ 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_launch , packet1.pin_nosecone , packet1.pin_expulsion , packet1.cutter_presence , packet1.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_launch , packet1.pin_nosecone , packet1.pin_expulsion , packet1.cutter_presence , packet1.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);
@@ -2753,7 +2818,7 @@ 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_launch , packet1.pin_nosecone , packet1.pin_expulsion , packet1.cutter_presence , packet1.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);
@@ -2775,7 +2840,7 @@ 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,73.0,101.0,129.0,157.0,185.0,213.0,241.0,269.0,297.0,325.0,353.0,381.0,409.0,437.0,465.0,493.0,521.0,549.0,577.0,605.0,633.0,661.0,689.0,717.0,745.0,773.0,801.0,829.0,857.0,885.0,913.0,941.0,969.0,997.0,1025.0,1053.0,205,16,83,150,217,28
+ 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
};
mavlink_payload_flight_tm_t packet1, packet2;
memset(&packet1, 0, sizeof(packet1));
@@ -2813,7 +2878,8 @@ 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.battery_voltage = packet_in.battery_voltage;
+ packet1.current_consumption = packet_in.current_consumption;
packet1.vsupply_5v = packet_in.vsupply_5v;
packet1.temperature = packet_in.temperature;
packet1.fmm_state = packet_in.fmm_state;
@@ -2836,12 +2902,12 @@ 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.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.current_consumption , packet1.vsupply_5v , 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.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.current_consumption , packet1.vsupply_5v , packet1.temperature , packet1.logger_error );
mavlink_msg_payload_flight_tm_decode(&msg, &packet2);
MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0);
@@ -2854,7 +2920,7 @@ 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.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.current_consumption , packet1.vsupply_5v , packet1.temperature , packet1.logger_error );
mavlink_msg_payload_flight_tm_decode(last_msg, &packet2);
MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0);
@@ -3100,7 +3166,7 @@ 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
};
mavlink_motor_tm_t packet1, packet2;
memset(&packet1, 0, sizeof(packet1));
@@ -3109,6 +3175,8 @@ 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;
@@ -3125,12 +3193,12 @@ 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.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.battery_voltage , packet1.current_consumption );
mavlink_msg_motor_tm_decode(&msg, &packet2);
MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0);
@@ -3143,7 +3211,7 @@ 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.battery_voltage , packet1.current_consumption );
mavlink_msg_motor_tm_decode(last_msg, &packet2);
MAVLINK_ASSERT(memcmp(&packet1, &packet2, sizeof(packet1)) == 0);
@@ -3197,6 +3265,7 @@ 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_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);
diff --git a/mavlink_lib/gemini/version.h b/mavlink_lib/gemini/version.h
index b22a23faeee0b6dcb23da5656347c64683eb926c..5452bc687b90261633a04de500f8f03118cfc8ef 100644
--- a/mavlink_lib/gemini/version.h
+++ b/mavlink_lib/gemini/version.h
@@ -7,8 +7,8 @@
#ifndef MAVLINK_VERSION_H
#define MAVLINK_VERSION_H
-#define MAVLINK_BUILD_DATE "Sun Aug 27 2023"
+#define MAVLINK_BUILD_DATE "Mon Aug 28 2023"
#define MAVLINK_WIRE_PROTOCOL_VERSION "1.0"
-#define MAVLINK_MAX_DIALECT_PAYLOAD_SIZE 171
+#define MAVLINK_MAX_DIALECT_PAYLOAD_SIZE 168
#endif // MAVLINK_VERSION_H
diff --git a/message_definitions/gemini.xml b/message_definitions/gemini.xml
index 1ee102500f24086650697a4b624d466fb4bdd1ad..cb2617c2b84b2d3a1adc1003c34282c25599733e 100644
--- a/message_definitions/gemini.xml
+++ b/message_definitions/gemini.xml
@@ -2,6 +2,12 @@
<mavlink>
<version>1</version>
<enums>
+ <enum name="SysIDs">
+ <description>Enum that lists all the system IDs of the various devices</description>
+ <entry name="MAIN" value="1"></entry>
+ <entry name="PAYLOAD" value="2"></entry>
+ <entry name="RIG" value="3"></entry>
+ </enum>
<enum name="SystemTMList">
<description>Enum list for all the telemetries that can be requested</description>
<entry name="MAV_SYS_ID" value="1">
@@ -28,27 +34,27 @@
<entry name="MAV_NAS_ID" value="8">
<description>NavigationSystem data</description>
</entry>
- <entry name="MAV_CAN_ID" value="9">
+ <entry name="MAV_MEA_ID" value="9">
+ <description>MEA Status</description>
+ </entry>
+ <entry name="MAV_CAN_ID" value="10">
<description>Canbus stats</description>
</entry>
- <entry name="MAV_FLIGHT_ID" value="10">
+ <entry name="MAV_FLIGHT_ID" value="11">
<description>Flight telemetry</description>
</entry>
- <entry name="MAV_STATS_ID" value="11">
+ <entry name="MAV_STATS_ID" value="12">
<description>Satistics telemetry</description>
</entry>
- <entry name="MAV_SENSORS_STATE_ID" value="12">
+ <entry name="MAV_SENSORS_STATE_ID" value="13">
<description>Sensors init state telemetry</description>
</entry>
- <entry name="MAV_GSE_ID" value="13">
+ <entry name="MAV_GSE_ID" value="14">
<description>Ground Segnement Equipment</description>
</entry>
- <entry name="MAV_MOTOR_ID" value="14">
+ <entry name="MAV_MOTOR_ID" value="15">
<description>Rocket Motor data</description>
</entry>
- <entry name="MAV_TARS_ID" value="15">
- <description>TARS data</description>
- </entry>
</enum>
<enum name="SensorsTMList">
<description>Enum list of all sensors telemetries that can be requested</description>
@@ -541,6 +547,16 @@
<field name="ref_latitude" type="float" units="deg">Calibration latitude</field>
<field name="ref_longitude" type="float" units="deg">Calibration longitude</field>
</message>
+ <message id="207" name="MEA_TM">
+ <description>Mass Estimation Algorithm status telemetry</description>
+ <field name="timestamp" type="uint64_t" units="us">When was this logged</field>
+ <field name="state" type="uint8_t">MEA current state</field>
+ <field name="kalman_x0" type="float">Kalman state variable 0 (corrected pressure)</field>
+ <field name="kalman_x1" type="float">Kalman state variable 1 </field>
+ <field name="kalman_x2" type="float">Kalman state variable 2 (mass)</field>
+ <field name="mass" type="float" units="kg">Mass estimated</field>
+ <field name="corrected_pressure" type="float" units="kg">Corrected pressure</field>
+ </message>
<message id="208" name="ROCKET_FLIGHT_TM">
<description>High Rate Telemetry</description>
<field name="timestamp" type="uint64_t" units="us">Timestamp in microseconds</field>
@@ -549,6 +565,7 @@
<field name="dpl_state" type="uint8_t">Deployment Controller State</field>
<field name="abk_state" type="uint8_t">Airbrake FSM state</field>
<field name="nas_state" type="uint8_t">Navigation System FSM State</field>
+ <field name="mea_state" type="uint8_t">MEA Controller State</field>
<field name="pressure_ada" type="float" units="Pa">Atmospheric pressure estimated by ADA</field>
<field name="pressure_digi" type="float" units="Pa">Pressure from digital sensor</field>
<field name="pressure_static" type="float" units="Pa">Pressure from static port</field>
@@ -556,6 +573,7 @@
<field name="airspeed_pitot" type="float" units="m/s">Pitot airspeed</field>
<field name="altitude_agl" type="float" units="m">Altitude above ground level</field>
<field name="ada_vert_speed" type="float" units="m/s">Vertical speed estimated by ADA</field>
+ <field name="mea_mass" type="float" units="kg">Mass estimated by MEA</field>
<field name="acc_x" type="float" units="m/s^2">Acceleration on X axis (body)</field>
<field name="acc_y" type="float" units="m/s^2">Acceleration on Y axis (body)</field>
<field name="acc_z" type="float" units="m/s^2">Acceleration on Z axis (body)</field>
@@ -570,8 +588,6 @@
<field name="gps_lon" type="float" units="deg">Longitude</field>
<field name="gps_alt" type="float" units="m">GPS Altitude</field>
<field name="abk_angle" type="float" units="deg">Air Brakes angle</field>
- <field name="abk_estimated_cd" type="float">Estimated drag coefficient</field>
- <field name="parachute_load" type="float">Parachute load cell value</field>
<field name="nas_n" type="float" units="deg">Navigation system estimated noth position</field>
<field name="nas_e" type="float" units="deg">Navigation system estimated east position</field>
<field name="nas_d" type="float" units="m">Navigation system estimated down position</field>
@@ -589,8 +605,8 @@
<field name="pin_nosecone" type="uint8_t">Nosecone pin status (1 = connected, 0 = disconnected)</field>
<field name="pin_expulsion" type="uint8_t">Servo sensor status (1 = actuated, 0 = idle)</field>
<field name="cutter_presence" type="uint8_t">Cutter presence status (1 = present, 0 = missing)</field>
- <field name="estimated_thrust" type="float">Estimated thrust from automatic shutdown algorithm</field>
- <field name="vbat" type="float" units="V">Battery voltage</field>
+ <field name="battery_voltage" type="float" units="V">Battery voltage</field>
+ <field name="current_consumption" type="float" units="A">Battery current</field>
<field name="temperature" type="float" units="degC">Temperature</field>
<field name="logger_error" type="int8_t">Logger error (0 = no error, -1 otherwise)</field>
</message>
@@ -635,7 +651,8 @@
<field name="wes_n" type="float" units="m/s">Wind estimated north velocity</field>
<field name="wes_e" type="float" units="m/s">Wind estimated east velocity</field>
<field name="pin_nosecone" type="uint8_t">Nosecone pin status (1 = connected, 0 = disconnected)</field>
- <field name="vbat" type="float" units="V">Battery voltage</field>
+ <field name="battery_voltage" type="float" units="V">Battery voltage</field>
+ <field name="current_consumption" type="float" units="A">Battery current</field>
<field name="vsupply_5v" type="float" units="V">Power supply 5V</field>
<field name="temperature" type="float" units="degC">Temperature</field>
<field name="logger_error" type="int8_t">Logger error (0 = no error)</field>
@@ -707,7 +724,9 @@
<field name="combustion_chamber_pressure" type="float" units="Bar">Pressure inside the combustion chamber used for automatic shutdown</field>
<field name="floating_level" type="uint8_t">Floating level in tank</field>
<field name="tank_temperature" type="float">Tank temperature</field>
- <field name="main_valve_state" type="uint8_t"> 1 If the main valve is open </field>
+ <field name="main_valve_state" type="uint8_t">1 If the main valve is open </field>
+ <field name="battery_voltage" type="float" units="V">Battery voltage</field>
+ <field name="current_consumption" type="float" units="A">Current drained from the battery</field>
</message>
</messages>
</mavlink>