diff --git a/classes/Component.m b/classes/Component.m
index f297c21b0aab25587c9538a41798d2acf3c4ea69..0a1e53fcffc0b4f885faa26c024bbf5ccc32ab38 100644
--- a/classes/Component.m
+++ b/classes/Component.m
@@ -6,10 +6,6 @@ classdef Component < Config
% Insert dependencies here
mission Mission
end
-
- properties(Access = protected)
- variableName string = '';
- end
methods
function obj = Component(mission, varsIn)
@@ -44,7 +40,8 @@ classdef Component < Config
% obj.loadConfig(vars) - To load from given variables
fileName = obj.configName;
- obj.variableName = strtok(fileName, 'C');
+ varName = obj.variableName;
+ if isempty(varName), varName = strtok(fileName, 'C'); end
switch nargin
case 1
@@ -56,9 +53,9 @@ classdef Component < Config
end
run(fileName);
- configObj = eval(obj.variableName);
+ configObj = eval(varName);
case 2
- configObj = varargin{1}.(obj.variableName);
+ configObj = varargin{1}.(varName);
otherwise
error('Too many input arguments.')
end
diff --git a/classes/Config.m b/classes/Config.m
index 0b8af1abcf291b77a05501e488f22967f76a5c33..ae525c4d864c7a5cbddfeb5ee380be998711c56a 100644
--- a/classes/Config.m
+++ b/classes/Config.m
@@ -5,6 +5,7 @@ classdef(Abstract) Config < handle
properties(Abstract, Access = protected)
configName {mustBeTextScalar}
+ variableName char
end
methods(Abstract, Access = protected)
diff --git a/classes/Mission.m b/classes/Mission.m
index 2ffe2f8ca86078509c6433c2060585592acff288..d3198c0a5f7019c5e437ebd781a021320324e7d3 100644
--- a/classes/Mission.m
+++ b/classes/Mission.m
@@ -19,6 +19,7 @@ classdef Mission < Config
properties(Access = protected)
configName = 'missionConfig.m'
+ variableName = ''
end
methods
diff --git a/classes/Rocket.m b/classes/Rocket.m
index 7f40c78b9a39157f208eeb18fdddd7b7ee2994fb..bddf2d7bf55f0f0f28b53747d008d351848e62a2 100644
--- a/classes/Rocket.m
+++ b/classes/Rocket.m
@@ -17,11 +17,13 @@ classdef Rocket < Bay
length
diameter
mass
+ massNoMotor
inertia
end
properties(Access = protected)
configName = 'rocketConfig.m'
+ variableName = ''
mission Mission
end
diff --git a/classes/bays/Airbrakes.m b/classes/bays/Airbrakes.m
index 1a5adea18fab2e522a7eb96d8b8dcac573808105..d7e5e7f4ec0e05e157d0a60ae75652566b096a2f 100644
--- a/classes/bays/Airbrakes.m
+++ b/classes/bays/Airbrakes.m
@@ -21,7 +21,8 @@ classdef Airbrakes < Bay
end
properties(Access = protected)
- configName = 'airbrakesConfig.m'
- mission
+ configName = 'rocketConfig.m'
+ variableName = 'airbrakes'
+ mission Mission = Mission()
end
end
\ No newline at end of file
diff --git a/classes/bays/Boat.m b/classes/bays/Boat.m
index 386988879ccfa38bd8e3bcf7887f018f088bdde2..4747c7ad131e778dda8b39c068010158684fbf6b 100644
--- a/classes/bays/Boat.m
+++ b/classes/bays/Boat.m
@@ -9,7 +9,8 @@ classdef Boat < Bay
end
properties(Access = protected)
- configName = 'boatConfig.m'
- mission
+ configName = 'rocketConfig.m'
+ variableName = 'boat'
+ mission Mission = Mission()
end
end
\ No newline at end of file
diff --git a/classes/bays/Electronics.m b/classes/bays/Electronics.m
index 7f1237359ae8a82e0e99428bff47718f6a8e9fba..30add52a8a51543b85cd22e2cafa34cd5e4d3326 100644
--- a/classes/bays/Electronics.m
+++ b/classes/bays/Electronics.m
@@ -10,7 +10,8 @@ classdef Electronics < Bay
end
properties(Access = protected)
- configName = 'electronicsConfig.m'
- mission
+ configName = 'rocketConfig.m'
+ variableName = 'electronics'
+ mission Mission = Mission()
end
end
\ No newline at end of file
diff --git a/classes/bays/Motor.m b/classes/bays/Motor.m
index bfc6728c39d8819629ecf302d5ffb3e71cb2170c..f07892b76d8093bdbe2b4186ddd24bbb332d1baf 100644
--- a/classes/bays/Motor.m
+++ b/classes/bays/Motor.m
@@ -29,7 +29,8 @@ classdef Motor < Bay
properties(Access = protected)
configName = 'motorConfig.m'
- mission
+ variableName = ''
+ mission Mission = Mission()
end
methods
diff --git a/classes/bays/Nose.m b/classes/bays/Nose.m
index 6085b1bfb6b2a6f290cb19dec947946473a173e5..297c2246cf8ab0ce9fa9e5c46036706b65ed3d59 100644
--- a/classes/bays/Nose.m
+++ b/classes/bays/Nose.m
@@ -14,7 +14,8 @@ classdef Nose < Bay
end
properties(Access = protected)
- configName = 'noseConfig.m'
- mission
+ configName = 'rocketConfig.m'
+ variableName = 'nose'
+ mission Mission = Mission()
end
end
\ No newline at end of file
diff --git a/classes/bays/Payload.m b/classes/bays/Payload.m
index 3f120f19cc92a4a5643e0c26ab3e3dd97f7e37c8..9aedec37dfbf1b2e40489de689f6a2f7e9ba4047 100644
--- a/classes/bays/Payload.m
+++ b/classes/bays/Payload.m
@@ -9,7 +9,8 @@ classdef Payload < Bay
end
properties(Access = protected)
- configName = 'payloadConfig.m'
- mission
+ configName = 'rocketConfig.m'
+ variableName = 'payload'
+ mission Mission = Mission()
end
end
\ No newline at end of file
diff --git a/classes/bays/Recovery.m b/classes/bays/Recovery.m
index d76416f07e18320041b9e5bd035c1a6b0307a4e5..802272bea549696521efb76d325a01a0629b9a8b 100644
--- a/classes/bays/Recovery.m
+++ b/classes/bays/Recovery.m
@@ -9,7 +9,8 @@ classdef Recovery < Bay
end
properties(Access = protected)
- configName = 'recoveryConfig.m'
- mission
+ configName = 'rocketConfig.m'
+ variableName = 'recovery'
+ mission Mission = Mission()
end
end
\ No newline at end of file
diff --git a/classes/components/Fins.m b/classes/components/Fins.m
index e641595c72f10f6b59980b0806671c047d6ba9d6..bf20b0685bc2086ef5904d0b2be1c65f453e5d8b 100644
--- a/classes/components/Fins.m
+++ b/classes/components/Fins.m
@@ -15,7 +15,8 @@ classdef Fins < Component
end
properties(Access = protected)
- configName = 'finsConfig.m'
- mission Mission
+ configName = 'rocketConfig.m'
+ variableName = 'fins'
+ mission Mission = Mission()
end
end
\ No newline at end of file
diff --git a/classes/components/Pitot.m b/classes/components/Pitot.m
index 33d877f80d2539380cd3500f29716bb8a2ded6e3..eca6f94d4eb434ee2dda0d682a1a2ac9a1df167e 100644
--- a/classes/components/Pitot.m
+++ b/classes/components/Pitot.m
@@ -12,7 +12,8 @@ classdef Pitot < Component
end
properties(Access = protected)
- configName = 'pitotConfig.m'
- mission Mission
+ configName = 'rocketConfig.m'
+ variableName = 'pitot'
+ mission Mission = Mission()
end
end
\ No newline at end of file
diff --git a/missions/2024_Lyra_Roccaraso_September/config/airbrakesConfig.m b/missions/2024_Lyra_Roccaraso_September/config/old/airbrakesConfig.m
similarity index 100%
rename from missions/2024_Lyra_Roccaraso_September/config/airbrakesConfig.m
rename to missions/2024_Lyra_Roccaraso_September/config/old/airbrakesConfig.m
diff --git a/missions/2024_Lyra_Roccaraso_September/config/boatConfig.m b/missions/2024_Lyra_Roccaraso_September/config/old/boatConfig.m
similarity index 100%
rename from missions/2024_Lyra_Roccaraso_September/config/boatConfig.m
rename to missions/2024_Lyra_Roccaraso_September/config/old/boatConfig.m
diff --git a/missions/2024_Lyra_Roccaraso_September/config/electronicsConfig.m b/missions/2024_Lyra_Roccaraso_September/config/old/electronicsConfig.m
similarity index 100%
rename from missions/2024_Lyra_Roccaraso_September/config/electronicsConfig.m
rename to missions/2024_Lyra_Roccaraso_September/config/old/electronicsConfig.m
diff --git a/missions/2024_Lyra_Roccaraso_September/config/finsConfig.m b/missions/2024_Lyra_Roccaraso_September/config/old/finsConfig.m
similarity index 100%
rename from missions/2024_Lyra_Roccaraso_September/config/finsConfig.m
rename to missions/2024_Lyra_Roccaraso_September/config/old/finsConfig.m
diff --git a/missions/2024_Lyra_Roccaraso_September/config/motorConfig.m b/missions/2024_Lyra_Roccaraso_September/config/old/motorConfig.m
similarity index 100%
rename from missions/2024_Lyra_Roccaraso_September/config/motorConfig.m
rename to missions/2024_Lyra_Roccaraso_September/config/old/motorConfig.m
diff --git a/missions/2024_Lyra_Roccaraso_September/config/noseConfig.m b/missions/2024_Lyra_Roccaraso_September/config/old/noseConfig.m
similarity index 100%
rename from missions/2024_Lyra_Roccaraso_September/config/noseConfig.m
rename to missions/2024_Lyra_Roccaraso_September/config/old/noseConfig.m
diff --git a/missions/2024_Lyra_Roccaraso_September/config/payloadConfig.m b/missions/2024_Lyra_Roccaraso_September/config/old/payloadConfig.m
similarity index 100%
rename from missions/2024_Lyra_Roccaraso_September/config/payloadConfig.m
rename to missions/2024_Lyra_Roccaraso_September/config/old/payloadConfig.m
diff --git a/missions/2024_Lyra_Roccaraso_September/config/pitotConfig.m b/missions/2024_Lyra_Roccaraso_September/config/old/pitotConfig.m
similarity index 100%
rename from missions/2024_Lyra_Roccaraso_September/config/pitotConfig.m
rename to missions/2024_Lyra_Roccaraso_September/config/old/pitotConfig.m
diff --git a/missions/2024_Lyra_Roccaraso_September/config/recoveryConfig.m b/missions/2024_Lyra_Roccaraso_September/config/old/recoveryConfig.m
similarity index 100%
rename from missions/2024_Lyra_Roccaraso_September/config/recoveryConfig.m
rename to missions/2024_Lyra_Roccaraso_September/config/old/recoveryConfig.m
diff --git a/missions/2024_Lyra_Roccaraso_September/config/rocketConfig.m b/missions/2024_Lyra_Roccaraso_September/config/rocketConfig.m
index b8a2bbc62074a32bc4e6cd6aee9fc9f9b6a4fbdc..5f16058a899b345ed9c8d6d06f6b8047c22257a0 100644
--- a/missions/2024_Lyra_Roccaraso_September/config/rocketConfig.m
+++ b/missions/2024_Lyra_Roccaraso_September/config/rocketConfig.m
@@ -1,17 +1,105 @@
% CONFIG - This script sets up control parameters
+%% ROCKET - OVERRIDES BAYS CONFIG
rocket = Rocket();
-nose = Nose();
-payload = Payload();
-recovery = Recovery();
-electronics = Electronics();
-airbrakes = Airbrakes();
-motor = Motor();
-boat = Boat();
-fins = Fins();
-pitot = Pitot();
-
-rocket.length = 000;
-rocket.diameter = 000;
-rocket.mass = 000;
-rocket.inertia = 000;
+
+rocket.length = NaN; % [m] OVERRIDE total length
+rocket.diameter = NaN; % [m] OVERRIDE diameter
+rocket.mass = NaN; % [kg] OVERRIDE total mass
+rocket.massNoMotor = NaN; % [kg] OVERRIDE mass without motor
+rocket.inertia = NaN; % [] OVERRIDE total inertia
+
+%% NOSE
+nose = Nose();
+
+nose.length = 000; % [m] Nosecone Length
+nose.diameter = 000; % [m] Nosecone Diameter
+nose.mass = 000; % [m] Nosecone Inertia
+nose.inertia = 000; % [m] Nosecone Mass
+nose.ogiveType = 'MHAACK'; % [-] Nosecone shape
+nose.power = 000; %3/4; % [-] Nosecone power type parameter
+nose.p = 000; %1.250152e+00; % [-] P coefficient for modified nosecone shapes
+nose.c = 000; %1.799127e-01; % [-] C coefficient for modified nosecone shapes
+
+%% PLD
+payload = Payload();
+
+payload.length = 0;
+payload.diameter = 0;
+payload.mass = 0;
+payload.inertia = 0;
+
+%% ELC
+electronics = Electronics();
+
+electronics.length = 000;
+electronics.diameter = 000;
+electronics.mass = 000;
+electronics.inertia = 000;
+
+%% RCS
+recovery = Recovery();
+
+recovery.length = 0;
+recovery.diameter = 0;
+recovery.mass = 0;
+recovery.inertia = 0;
+
+%% ARB
+airbrakes = Airbrakes();
+
+airbrakes.multipleAB = false; % If true, multiple and smooth airbrakes opening will be simulated
+airbrakes.opening = [1 3]; % aerobrakes, 1-2-3 for 0%, 50% or 100% opened
+airbrakes.deltaTime = [10]; % aerobrakes, configurations usage time
+
+airbrakes.n = 3; % [-] number of brakes
+airbrakes.brakeWidth = 0.1002754821; % [m] brakes width (normal)
+airbrakes.brakeLength = 0.008; % [m] brakes thickness
+airbrakes.xDistance = 1.517; % [m] axial position from nosecone base
+
+airbrakes.length = 000;
+airbrakes.diameter = 000;
+airbrakes.mass = 000;
+airbrakes.inertia = 000;
+
+%% AIRBRAKES CONTROL SETTINGS
+airbrakes.minTime = 0; % [s] time after which the airbrakes can be used
+airbrakes.maxMach = 0.8; % [-] Maximum Mach at which airbrakes can be used
+airbrakes.servoOmega = 150*pi/180; % [rad/s] Servo-motor angular velocity
+airbrakes.height = linspace(0, 0.0363, 3); % [m] Block airbrakes opening coordinate ( First entry must be 0! )
+
+%% MOTOR
+motor = Motor();
+
+motor.name = 'HRE_FURIA-Rv2-T04T03';
+motor.ignitionTime = 0.4; % [s] Ignition transient
+motor.cutoffTime = 0.3; % [s] Cut-off transient
+
+%% BOAT
+boat = Boat();
+
+boat.length = 0;
+boat.diameter = 0;
+boat.mass = 0;
+boat.inertia = 0;
+
+%% FINS
+fins = Fins();
+
+fins.rootChord = 0.30; % [m] attached chord length
+fins.freeChord = 0.14; % [m] free chord length
+fins.height = 0.11; % [m] fin heigth
+fins.deltaXFreeChord = 0.13; % [m] start of Chord 2 measured from start of Chord 1
+fins.nPanel = 3; % [m] number of fins
+fins.leadingEdgeRadius = [0 0]; % [deg] Leading edge radius at each span station
+fins.axialDistance = 0.012; % [m] distance between end of root chord and end of center body
+fins.semiThickness = 0.00175; % [m] fin semi-thickness
+fins.maxThicknessPosition = 0.00175; % [m] Fraction of chord from leading edge to max thickness
+
+%% PITOT
+pitot = Pitot();
+
+protuberances.xDistance = 1.517; % [m] axial position from nosecone base
+protuberances.n = 3; % [-] number of brakes
+protuberances.length = 0.008; % [m] brakes thickness
+protuberances.width = 0.1002754821; % [m] brakes width (normal)
\ No newline at end of file