[code-refactoring][missions] WIP

- added configs
- added HREmotors.mat

missions/2024_Lyra_Roccaraso_September/config/geometryConfig.m

@@ -5,13 +5,13 @@
 %% Boat-tail
 % The boat-tail is simulated as a trunc of cone with the major diameter
 % equal to the rocket one (settings.C)
-geometry.boat.Length = 000;                                       % [m] Boat-tail length
-geometry.boat.Diameter = 000;                                     % [m] Boat-tail base diameter
+geometry.boat.length = 000;                                       % [m] Boat-tail length
+geometry.boat.diameter = 000;                                     % [m] Boat-tail base diameter
 
 %% Rocket ogive and central body
 geometry.center.length = 000; %1.517;                             % [m] Central body length
 geometry.center.caliber = 000;                                          % [m] Caliber (Fuselage Diameter)
-geometry.center.crossSection = pi*geometry.C^2/4;                       % [m^2] Cross-sectional Surface
+geometry.center.crossSection = pi*geometry.center.caliber^2/4;                       % [m^2] Cross-sectional Surface
 
 geometry.nose.length = 000;                                       % [m] Nosecone Length
 geometry.nose.ogiveType = 'MHAACK';                                   % [-] Nosecone shape

missions/2024_Lyra_Roccaraso_September/config/inertiaConfig.m

@@ -12,9 +12,9 @@ inertia.rocket.Iyy = 12.07664659;                             % [kg*m^2] Inertia
 inertia.rocket.Izz = 12.07701314;                             % [kg*m^2] Inertia to z-axis
 
 %%% Inertias for engine only
-inertia.engine.Ixx = HREmotors(iMotor).Ixx;                            % [kg*m^2] Inertia to x-axis
-inertia.engine.Iyy = HREmotors(iMotor).Iyy;                            % [kg*m^2] Inertia to y-axis
-inertia.engine.Izz = HREmotors(iMotor).Izz;                            % [kg*m^2] Inertia to z-axis
+% inertia.engine.Ixx = HREmotors(iMotor).Ixx;                            % [kg*m^2] Inertia to x-axis
+% inertia.engine.Iyy = HREmotors(iMotor).Iyy;                            % [kg*m^2] Inertia to y-axis
+% inertia.engine.Izz = HREmotors(iMotor).Izz;                            % [kg*m^2] Inertia to z-axis
 
 % %%% Total inertias
 % inertia.Ixx = inertia.rocketIxx + engineIxx;