[fins-dimensioning] small update

missions/2024_Lyra_Portugal_October/config/rocketConfig.m

@@ -9,12 +9,6 @@ rocket.inertiaNoMotor = [];                                             % [kg*m^
 rocket.xCgNoMotor = [];                                                 % [m]      OVERRIDE xCg without motor
 rocket.lengthCenterNoMot = [];                                          % [m]      OVERRIDE Center length - no nose, no motor
 
-% rocket.diameter = 0.15;                                               % [m]      Rocket diameter
-% rocket.massNoMotor = 17.0;                                            % [kg]     OVERRIDE mass without motor
-% rocket.inertiaNoMotor = [0.06535397; 17.21019828; 17.21056483];       % [kg*m^2] OVERRIDE inertia without motor - body axes reference
-% rocket.xCgNoMotor = 1.28;                                             % [m]      OVERRIDE xCg without motor
-% rocket.lengthCenterNoMot = 1.778;                                     % [m]      OVERRIDE Center length - no nose, no motor
-
 %% PLD - Includes Payload + Nose
 payload = Payload();
 
@@ -75,7 +69,7 @@ airbrakes.servoTau = 0.0374588;
 %% MOTOR
 motor = Motor();
 
-motor.name = 'HRE_ARM_SFT5_T03_T03';                                % [-] Motor name
+motor.name = 'HRE_ARM_SFT7_T03_T03';                                % [-] Motor name
 motor.cutoffTime = [];                                               % [s] OVERRIDE Cutoff time
 motor.ignitionTransient = 0.3;                                       % [s] Ignition transient
 motor.cutoffTransient = 0.3;                                         % [s] Cut-off transient

missions/2024_Lyra_Portugal_October/config/windConfig.m

@@ -11,12 +11,12 @@
 
 windCustom = WindCustom();
 
-windCustom.altitudes = [0 200 2000];                    % [m] Altitudes at which a distribution change occurs
-windCustom.magnitudeDistribution = ["u", "u", "u"];     % [-] Distribution type: "u" - uniform, "g" - gaussian
-windCustom.magnitudeParameters = [7 2 10;               % [m/s] Distribution parameters: "u" - [min; max], "g" - [mu; sigma]
-                            7 2 10];
-windCustom.azimuthDistribution = ["u", "u", "u"];       % [-] Distribution type: "u" - uniform, "g" - gaussian
-windCustom.azimuthParameters = 0*pi/180 * ones(2,3);    % [deg] Distribution parameters: "u" - [min; max], "g" - [mu; sigma]
+windCustom.altitudes = [0 4500];                    % [m] Altitudes at which a distribution change occurs
+windCustom.magnitudeDistribution = ["u", "u"];     % [-] Distribution type: "u" - uniform, "g" - gaussian
+windCustom.magnitudeParameters = [0 0;               % [m/s] Distribution parameters: "u" - [min; max], "g" - [mu; sigma]
+                            9 9];
+windCustom.azimuthDistribution = ["u", "u"];       % [-] Distribution type: "u" - uniform, "g" - gaussian
+windCustom.azimuthParameters = [0 0; 359 359]*pi/180;    % [deg] Distribution parameters: "u" - [min; max], "g" - [mu; sigma]
 
 %% MATLAB WIND MODEL