[design-updates][2024_Lyra_Portugal_October] Updated Euroc data

missions/2024_Lyra_Portugal_October/config/environmentConfig.m

@@ -4,11 +4,11 @@
 
 environment = Environment();
 
-environment.lat0 = 39.388727;           % [deg] Launchpad latitude
-environment.lon0 = -8.287842;           % [deg] Launchpad longitude
+environment.lat0 = 39.3901711000000;           % [deg] Launchpad latitude
+environment.lon0 = -8.28954220000000;           % [deg] Launchpad longitude
 environment.z0 = 160;                   % [m] Launchpad Altitude
-environment.omega = 85;                 % [deg] Launchpad elevation
-environment.phi = 133;                  % [deg] Launchpad azimuth
+environment.omega = 84;                 % [deg] Launchpad elevation
+environment.phi = 134.5;                  % [deg] Launchpad azimuth
 environment.pin1Length = 0.5603;        % [m] Distance from the upper pin to the upper tank cap
 environment.pin2Length = 0.2055;        % [m] Distance from the lower pin to the lower tank cap  
 environment.rampLength = 12;            % [m] Total launchpad length 

missions/2024_Lyra_Portugal_October/config/rocketConfig.m

@@ -49,7 +49,7 @@ airbrakes.mass = 0.936;                                              % [kg] Tota
 airbrakes.inertia = 1e-9*[3086650; 1931082; 1889047];                % [kg*m^2] Total bay inertia (Body reference)
 airbrakes.xCg = 30.54 * 1e-3;                                        % [m] Cg relative to bay upper side
 
-airbrakes.enabled = false;                                  % If true, multiple and smooth airbrakes opening will be simulated
+airbrakes.enabled = true;                                  % If true, multiple and smooth airbrakes opening will be simulated
 airbrakes.extension = [1];                                 % aerobrakes, 1-2-3 for 0%, 50% or 100% opened
 airbrakes.deltaTime = [0];                               % aerobrakes, configurations usage time
 
@@ -95,7 +95,7 @@ motor = Motor();
 % motor.name = 'HRE_ARM_P_67_T015_T03';
 % 
 % motor.name = 'HRE_ARM_P_40_T030_T03';
-motor.name = 'HRE_ARM_P_41_T030_T03';
+% motor.name = 'HRE_ARM_P_41_T030_T03';
 % motor.name = 'HRE_ARM_P_42_T030_T03';
 % motor.name = 'HRE_ARM_P_43_T030_T03';
 % motor.name = 'HRE_ARM_P_44_T030_T03';
@@ -105,7 +105,7 @@ motor.name = 'HRE_ARM_P_41_T030_T03';
 % motor.name = 'HRE_ARM_P_48_T030_T03';
 % motor.name = 'HRE_ARM_P_49_T030_T03';
 % motor.name = 'HRE_ARM_P_50_T030_T03';
-% motor.name = 'HRE_ARM_P_52_T030_T03';
+motor.name = 'HRE_ARM_P_52_T030_T03';
 % motor.name = 'HRE_ARM_P_53_T030_T03';
 % motor.name = 'HRE_ARM_P_54_T030_T03';
 % motor.name = 'HRE_ARM_P_55_T030_T03';

missions/2024_Lyra_Portugal_October/config/windConfig.m

@@ -11,13 +11,13 @@
 
 windCustom = WindCustom();
 
-windCustom.altitudes = [0 140 500 1000 1500 2000 2500 3000 3500 4000];                    % [m] Altitudes at which a distribution change occurs
-windCustom.magnitudeDistribution = ["u", "g", "g", "g", "g", "g", "g", "g", "g", "g"];     % [-] Distribution type: "u" - uniform, "g" - gaussian
-windCustom.magnitudeParameters = [0 7 12 13 13 14 14 15 15 15; 
-                                  8.7 1.5 3 3 3 3 3 3 3 3];               % [m/s] Distribution parameters: "u" - [min; max], "g" - [mu; sigma]
+windCustom.altitudes = [0 150 500 1000 1500 2000 2500 3000 3500 4000];                    % [m] Altitudes at which a distribution change occurs
+windCustom.magnitudeDistribution = ["g", "g", "g", "g", "g", "g", "g", "g", "g", "g"];     % [-] Distribution type: "u" - uniform, "g" - gaussian
+windCustom.magnitudeParameters = [3 4 6 7 8 11 12 14 15 18; 
+                                  1.5 1.5 2 2 2 2 2 2 2 2];               % [m/s] Distribution parameters: "u" - [min; max], "g" - [mu; sigma]
 windCustom.azimuthDistribution = ["u", "u", "u", "u", "u", "u", "u", "u", "u", "u"];       % [-] Distribution type: "u" - uniform, "g" - gaussian
-windCustom.azimuthParameters = [270 270 270 280 270 260 260 240 240 240; 
-                                290 290 290 300 290 280 280 280 280 280]*pi/180;    % [deg] Distribution parameters: "u" - [min; max], "g" - [mu; sigma]
+windCustom.azimuthParameters = [197 150 160 180 200 200 200 200 200 210; 
+                                217 170 180 200 220 220 220 220 220 230]*pi/180;    % [deg] Distribution parameters: "u" - [min; max], "g" - [mu; sigma]
 
 % windCustom.altitudes = [0 4500];
 % windCustom.magnitudeDistribution = ["u", "u"];