[design-updates] Updated aerodynamic coefficients

- Updated fins with new design constraint
- Updated aerodynamic coefficients for new fins

missions/2025_Orion_Portugal_October/config/rocketConfig.m

@@ -14,7 +14,7 @@ parafoil = Parafoil();
 
 parafoil.length = 646.2 * 1e-3;                                         % [m] Total bay length
 parafoil.mass = 5.2;                                                   % [kg] Total bay mass
-parafoil.inertia = 1e-9*[12531966; 109986813; 109930516];                % [kg*m^2] Total bay inertia (Body reference)
+parafoil.inertia = 1e-9*[10514313; 92235828; 92322682];                % [kg*m^2] Total bay inertia (Body reference)
 parafoil.xCg = 453.55 * 1e-3;                                            % [m] Cg relative to bay upper side
 
 parafoil.noseLength = 0.327;                                              % [m] Nosecone length
@@ -28,7 +28,7 @@ recovery = Recovery();
 
 recovery.length = 826 * 1e-3;                                        % [m] Total bay length
 recovery.mass = 4.42;                                               % [kg] Total bay mass
-recovery.inertia = 1e-9*[13831051; 269596803; 269645059];            % [kg*m^2] Total bay inertia (Body reference)
+recovery.inertia = 1e-9*[11870797; 264801282; 265519904];            % [kg*m^2] Total bay inertia (Body reference)
 recovery.xCg = 459 * 1e-3;                                        % [m] Cg relative to bay upper side
 
 %% ELC
@@ -36,7 +36,7 @@ electronics = Electronics();
 
 electronics.length = 422.5 * 1e-3;                                   % [m] Total bay length
 electronics.mass = 3.5;                                            % [kg] Total bay mass
-electronics.inertia = 1e-9*[9358415; 49265825; 48770607];            % [kg*m^2] Total bay inertia (Body reference)
+electronics.inertia = 1e-9*[10041478; 49742634; 50292878];            % [kg*m^2] Total bay inertia (Body reference)
 electronics.xCg = 221.11 * 1e-3;                                     % [m] Cg relative to bay upper side
 
 %% ARB
@@ -46,10 +46,10 @@ airbrakes.identification = false;                           % Control parameter
 
 airbrakes.length = 54.8 * 1e-3;                                      % [m] Total bay length
 airbrakes.mass = 0.96;                                              % [kg] Total bay mass
-airbrakes.inertia = 1e-9*[3086650; 1931082; 1889047];                % [kg*m^2] Total bay inertia (Body reference)
+airbrakes.inertia = 1e-9*[1886729; 1931082; 3088968];                % [kg*m^2] Total bay inertia (Body reference)
 airbrakes.xCg = 35.2 * 1e-3;                                        % [m] Cg relative to bay upper side
 
-airbrakes.enabled = true;                                  % If true, multiple and smooth airbrakes opening will be simulated
+airbrakes.enabled = false;                                  % 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 = [0.5];                               % aerobrakes, configurations usage time
 
@@ -82,14 +82,14 @@ rear.position = 1.2468;                                               % [m] offs
 rear.length = 547 * 1e-3;                                            % [m] Total bay length
 rear.mass = 1.71;                                                    % [kg] Total bay mass
 rear.inertia = 1e-9*[13074201; 44271226; 44270124];                  % [kg*m^2] Total bay inertia (Body reference)
-rear.xCg = 253.77 * 1e-3;                                                                                               % [m] Cg relative to bay upper side
+rear.xCg = 276.98 * 1e-3;                                                                                               % [m] Cg relative to bay upper side
 
 rear.boatType = 'OGIVE';                                             % [-] Boat type
 rear.boatLength = 0.240;                                             % [m] Boat length
 rear.boatFinalDiameter = 0.076;                                      % [m] Boat end diameter
 
 rear.finsRootChord = 0.3;                                            % [m] attached chord length
-rear.finsFreeChord = 0.21;                                           % [m] free chord length
+rear.finsFreeChord = 0.11;                                           % [m] free chord length
 rear.finsHeight = 0.15;                                              % [m] fin height
 % rear.finsDeltaXRootChord = 0.205;
 rear.finsDeltaXFreeChord = 0.16;                                     % [m] start of Chord 2 measured from start of Chord 1