[fins-dimensioning][2024_Lyra_Roccaraso_September] updates

missions/2024_Lyra_Portugal_October/config/rocketConfig.m

@@ -33,9 +33,9 @@ payload.noseCMod = 1.799127e-01;                                        % [-] C
 recovery = Recovery();
 
 recovery.length = 826 * 1e-3;                                        % [m] Total bay length
-recovery.mass = 4.065;                                               % [kg] Total bay mass
-recovery.inertia = 1e-9*[13422459; 217223325; 217296702];            % [kg*m^2] Total bay inertia (Body reference)
-recovery.xCg = 549.41 * 1e-3;                                        % [m] Cg relative to bay upper side
+recovery.mass = 4.261;                                               % [kg] Total bay mass
+recovery.inertia = 1e-9*[13831051; 269596803; 269645059];            % [kg*m^2] Total bay inertia (Body reference)
+recovery.xCg = 500.38 * 1e-3;                                        % [m] Cg relative to bay upper side
 
 %% ELC
 electronics = Electronics();

missions/2024_Lyra_Roccaraso_September/config/rocketConfig.m

@@ -33,9 +33,9 @@ payload.noseCMod   = 1.799127e-01;                         % [-] C coefficient f
 recovery = Recovery();
 
 recovery.length = 826 * 1e-3;                                        % [m] Total bay length
-recovery.mass = 4.065;                                               % [kg] Total bay mass
-recovery.inertia = 1e-9*[13422459; 217223325; 217296702];            % [kg*m^2] Total bay inertia (Body reference)
-recovery.xCg = 549.41 * 1e-3;                                        % [m] Cg relative to bay upper side
+recovery.mass = 4.261;                                               % [kg] Total bay mass
+recovery.inertia = 1e-9*[13831051; 269596803; 269645059];            % [kg*m^2] Total bay inertia (Body reference)
+recovery.xCg = 500.38 * 1e-3;                                        % [m] Cg relative to bay upper side
 
 %% ELC
 electronics = Electronics();