diff --git a/classes/@Rocket/Rocket.m b/classes/@Rocket/Rocket.m
index 825e8360ef8caa2d09ce9628731c6f6616e89d73..30c76a48b95e72217938671ddc07ed5db368dd17 100644
--- a/classes/@Rocket/Rocket.m
+++ b/classes/@Rocket/Rocket.m
@@ -52,7 +52,8 @@ classdef Rocket < Config
parachutes cell % [-] (nParachutes, nStages) Parachutes onboard
dynamicDerivatives (1, 1) logical % [-] True if dynamic derivatives will be loaded
-
+ highAOACoefficients (1, 1) logical % [-] True if highAOACoefficients are loaded
+
coefficients Coefficient % [-] Aerodynamic coefficients
coefficientsHighAOA Coefficient % [-] Aerodynamic coefficients at high angle of attack
end
@@ -150,13 +151,16 @@ classdef Rocket < Config
fullfile(mission.dataPath, 'aeroCoefficients.mat'), ...
coeffName);
- obj.coefficientsHighAOA = Coefficient( ...
- fullfile(mission.dataPath, 'aeroCoefficientsHighAOA.mat'), ...
- coeffName);
+ if obj.highAOACoefficients
+ obj.coefficientsHighAOA = Coefficient( ...
+ fullfile(mission.dataPath, 'aeroCoefficientsHighAOA.mat'), ...
+ coeffName);
+ end
answer = '';
- if isempty(obj.coefficients.static) || isempty(obj.coefficientsHighAOA.static)
+ if isempty(obj.coefficients.static) || ...
+ (obj.highAOACoefficients && isempty(obj.coefficientsHighAOA.static))
answer = questdlg(['Coefficient matrices not found. ' ...
'Do you want to create new matrices?']);
elseif options.checkGeometry
@@ -195,7 +199,7 @@ classdef Rocket < Config
parserPath = fullfile(mission.msaPath, 'autoMatricesProtub');
addpath(genpath(parserPath));
[obj.coefficients, obj.coefficientsHighAOA] = ...
- mainAutoMatProtub(obj);
+ mainAutoMatProtub(obj, 'computeHighAOA', obj.highAOACoefficients);
case 'Cancel'
error('Rocket creation aborted')
otherwise
diff --git a/missions/2021_Lynx_Portugal_October/config/rocketConfig.m b/missions/2021_Lynx_Portugal_October/config/rocketConfig.m
index 160c5b09b850ef81406e13cf89dfcda9005c2e9c..cb264015ae392fd9ed08b661398f6b5efb8f1d2e 100644
--- a/missions/2021_Lynx_Portugal_October/config/rocketConfig.m
+++ b/missions/2021_Lynx_Portugal_October/config/rocketConfig.m
@@ -20,6 +20,7 @@ rocket.lengthCenterNoMot = 1.7640; % [m]
% When false, coefficients are saved with current motor's name
% When true, coefficients are saved as 'generic'
rocket.dynamicDerivatives = false; % [-] True if dynamic derivatives will be loaded
+rocket.highAOACoefficients = false; % [-] True if separate matrix for high AOA will be loaded
%% PLD - Includes Parafoil + Nose
parafoil = Parafoil();
diff --git a/missions/2021_Lynx_Roccaraso_September/config/rocketConfig.m b/missions/2021_Lynx_Roccaraso_September/config/rocketConfig.m
index d0dc3df55356e3aebc59d51214a30794f8668dc1..0851f94e15aa603fff564f4dd2d8ed15c0e56bf8 100644
--- a/missions/2021_Lynx_Roccaraso_September/config/rocketConfig.m
+++ b/missions/2021_Lynx_Roccaraso_September/config/rocketConfig.m
@@ -20,6 +20,7 @@ rocket.lengthCenterNoMot = 1.7840; % [m]
% When false, coefficients are saved with current motor's name
% When true, coefficients are saved as 'generic'
rocket.dynamicDerivatives = false; % [-] True if dynamic derivatives will be loaded
+rocket.highAOACoefficients = false; % [-] True if separate matrix for high AOA will be loaded
%% PLD - Includes Parafoil + Nose
parafoil = Parafoil();
diff --git a/missions/2022_Pyxis_Portugal_October/config/rocketConfig.m b/missions/2022_Pyxis_Portugal_October/config/rocketConfig.m
index 2f949bfb46c9b09dd02fea6a1c87253e9c6c5b20..17d63ca520136746a7f874cb8e2d9c34c726670b 100644
--- a/missions/2022_Pyxis_Portugal_October/config/rocketConfig.m
+++ b/missions/2022_Pyxis_Portugal_October/config/rocketConfig.m
@@ -20,6 +20,7 @@ rocket.lengthCenterNoMot = 1.4470; % [m]
% When false, coefficients are saved with current motor's name
% When true, coefficients are saved as 'generic'
rocket.dynamicDerivatives = false; % [-] True if dynamic derivatives will be loaded
+rocket.highAOACoefficients = false; % [-] True if separate matrix for high AOA will be loaded
%% PLD - Includes Parafoil + Nose
parafoil = Parafoil();
diff --git a/missions/2022_Pyxis_Roccaraso_September/config/rocketConfig.m b/missions/2022_Pyxis_Roccaraso_September/config/rocketConfig.m
index ee3a3c71bd73ab263db92f3e929db488a6a5735c..5b7406a3e5a8362c54c1caddde3a35c9fa1798cc 100644
--- a/missions/2022_Pyxis_Roccaraso_September/config/rocketConfig.m
+++ b/missions/2022_Pyxis_Roccaraso_September/config/rocketConfig.m
@@ -22,6 +22,7 @@ rocket.lengthCenterNoMot = 1.61; % [m]
% When false, coefficients are saved with current motor's name
% When true, coefficients are saved as 'generic'
rocket.dynamicDerivatives = false; % [-] True if dynamic derivatives will be loaded
+rocket.highAOACoefficients = false; % [-] True if separate matrix for high AOA will be loaded
%% PLD - Includes Parafoil + Nose
parafoil = Parafoil();
diff --git a/missions/2023_Gemini_Portugal_October/config/rocketConfig.m b/missions/2023_Gemini_Portugal_October/config/rocketConfig.m
index 401c415be5e782af00b4318e62db4d13ea6ef5ca..f9d6d4c6f95e6d93445e6289d5115b9bba35837a 100644
--- a/missions/2023_Gemini_Portugal_October/config/rocketConfig.m
+++ b/missions/2023_Gemini_Portugal_October/config/rocketConfig.m
@@ -19,7 +19,7 @@ rocket.lengthCenterNoMot = 1.517; % [m]
% When false, coefficients are saved with current motor's name
% When true, coefficients are saved as 'generic'
rocket.dynamicDerivatives = false; % [-] True if dynamic derivatives will be loaded
-
+rocket.highAOACoefficients = false; % [-] True if separate matrix for high AOA will be loaded
%% PLD - Includes Parafoil + Nose
parafoil = Parafoil();
diff --git a/missions/2023_Gemini_Roccaraso_September/config/rocketConfig.m b/missions/2023_Gemini_Roccaraso_September/config/rocketConfig.m
index fc2715bc0dd7d61dd740e20b3138c8552440dcf1..cadbc7ef2b84f7f504eae85f73766ece8a83ec9c 100644
--- a/missions/2023_Gemini_Roccaraso_September/config/rocketConfig.m
+++ b/missions/2023_Gemini_Roccaraso_September/config/rocketConfig.m
@@ -19,6 +19,7 @@ rocket.lengthCenterNoMot = 1.517; % [m]
% When false, coefficients are saved with current motor's name
% When true, coefficients are saved as 'generic'
rocket.dynamicDerivatives = false; % [-] True if dynamic derivatives will be loaded
+rocket.highAOACoefficients = false; % [-] True if separate matrix for high AOA will be loaded
%% PLD - Includes Parafoil + Nose
parafoil = Parafoil();
diff --git a/missions/2024_Lyra_Portugal_October/config/rocketConfig.m b/missions/2024_Lyra_Portugal_October/config/rocketConfig.m
index f87640c176ca52f0ab3274f1b32602462a1489ff..1d90d15565d46515b3ca9ef5bcc7677b369fd810 100644
--- a/missions/2024_Lyra_Portugal_October/config/rocketConfig.m
+++ b/missions/2024_Lyra_Portugal_October/config/rocketConfig.m
@@ -13,6 +13,7 @@ rocket.lengthCenterNoMot = []; % [m]
% When false, coefficients are saved with current motor's name
% When true, coefficients are saved as 'generic'
rocket.dynamicDerivatives = false; % [-] True if dynamic derivatives will be loaded
+rocket.highAOACoefficients = false; % [-] True if separate matrix for high AOA will be loaded
%% PLD - Includes Parafoil + Nose
parafoil = Parafoil();
diff --git a/missions/2024_Lyra_Roccaraso_September/config/rocketConfig.m b/missions/2024_Lyra_Roccaraso_September/config/rocketConfig.m
index 2939db0ce6550575817cdd355d8b2f6ca2e68943..133be74e22c422360b80e924c6fb291a147c61db 100644
--- a/missions/2024_Lyra_Roccaraso_September/config/rocketConfig.m
+++ b/missions/2024_Lyra_Roccaraso_September/config/rocketConfig.m
@@ -19,6 +19,7 @@ rocket.lengthCenterNoMot = []; % [m]
% When false, coefficients are saved with current motor's name
% When true, coefficients are saved as 'generic'
rocket.dynamicDerivatives = false; % [-] True if dynamic derivatives will be loaded
+rocket.highAOACoefficients = false; % [-] True if separate matrix for high AOA will be loaded
%% PLD - Includes Parafoil + Nose
parafoil = Parafoil();
diff --git a/missions/2025_Orion_Portugal_October/config/rocketConfig.m b/missions/2025_Orion_Portugal_October/config/rocketConfig.m
index 6a13ec2512f1ba80b938af94064c3038be076bfd..cab54fffbaec6cdfd7bc778ae599e243b2707025 100644
--- a/missions/2025_Orion_Portugal_October/config/rocketConfig.m
+++ b/missions/2025_Orion_Portugal_October/config/rocketConfig.m
@@ -12,7 +12,8 @@ rocket.diameter = 0.15; % [m]
% If dynamic derivatives are loaded, coefficient will depend on rocket xcg
% When false, coefficients are saved with current motor's name
% When true, coefficients are saved as 'generic'
-rocket.dynamicDerivatives = false; % [-] True if dynamic derivatives will be loaded
+rocket.dynamicDerivatives = false; % [-] True if dynamic derivatives will be loaded
+rocket.highAOACoefficients = false; % [-] True if separate matrix for high AOA will be loaded
%% PRF - Includes Parafoil + Nose
parafoil = Parafoil();