diff --git a/classes/@Rocket/Rocket.m b/classes/@Rocket/Rocket.m
index a06283be4bc00d80338e94a9fc570771dfda416d..7e39e879fb8a463b4548fcc69f138efdb8c08da4 100644
--- a/classes/@Rocket/Rocket.m
+++ b/classes/@Rocket/Rocket.m
@@ -50,9 +50,11 @@ classdef Rocket < Config
properties
pitot Pitot % [-] Pitot component
parachutes cell % [-] (nParachutes, nStages) Parachutes onboard
+
+ dynamicDerivatives (1, 1) logical % [-] True if dynamic derivatives will be loaded
- coefficients struct % [-] Aerodynamic coefficients
- coefficientsHighAOA struct % [-] Aerodynamic coefficients at high angle of attack
+ coefficients Coefficient % [-] Aerodynamic coefficients
+ coefficientsHighAOA Coefficient % [-] Aerodynamic coefficients at high angle of attack
end
properties(Access = private)
@@ -138,9 +140,20 @@ classdef Rocket < Config
obj.parachutes = paraLoader.parachutes;
if options.loadCoefficients
- obj = obj.loadData();
+ if obj.dynamicDerivatives, coeffName = obj.motor.name;
+ else, coeffName = 'generic';
+ end
+
+ obj.coefficients = Coefficient( ...
+ fullfile(mission.dataPath, 'aeroCoefficients.mat'), ...
+ coeffName);
+
+ obj.coefficientsHighAOA = Coefficient( ...
+ fullfile(mission.dataPath, 'aeroCoefficientsHighAOA.mat'), ...
+ coeffName);
+
answer = '';
- if isempty(obj.coefficients) || isempty(obj.coefficientsHighAOA)
+ if isempty(obj.coefficients.static) || isempty(obj.coefficientsHighAOA.static)
answer = questdlg(['Coefficient matrices not found. ' ...
'Do you want to create new matrices?']);
elseif options.checkGeometry && ~all(obj.checkGeometry())
@@ -153,7 +166,14 @@ classdef Rocket < Config
parserPath = fullfile(mission.msaPath, 'autoMatricesProtub');
addpath(genpath(parserPath));
mainAutoMatProtub(obj);
- obj = obj.loadData();
+
+ obj.coefficients = Coefficient( ...
+ fullfile(mission.dataPath, 'aeroCoefficients.mat'), ...
+ coeffName);
+
+ obj.coefficientsHighAOA = Coefficient( ...
+ fullfile(mission.dataPath, 'aeroCoefficientsHighAOA.mat'), ...
+ coeffName);
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 4df34a1b48f4d03c4a6cdcb791b8c8c5985a17ec..160c5b09b850ef81406e13cf89dfcda9005c2e9c 100644
--- a/missions/2021_Lynx_Portugal_October/config/rocketConfig.m
+++ b/missions/2021_Lynx_Portugal_October/config/rocketConfig.m
@@ -16,6 +16,11 @@ rocket.inertiaNoMotor = [0.0786; 12.972; 12.972]; % [kg*m^2] OVERRIDE iner
rocket.xCgNoMotor = 1.6025; % [m] OVERRIDE xCg without motor
rocket.lengthCenterNoMot = 1.7640; % [m] OVERRIDE Center length - no nose, no motor
+% 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
+
%% 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 83f64760123f82fd1703c408e2543fa3d76f8e12..d0dc3df55356e3aebc59d51214a30794f8668dc1 100644
--- a/missions/2021_Lynx_Roccaraso_September/config/rocketConfig.m
+++ b/missions/2021_Lynx_Roccaraso_September/config/rocketConfig.m
@@ -16,6 +16,11 @@ rocket.inertiaNoMotor = [0.06; 7.511; 7.512]; % [kg*m^2] OVERRIDE inertia
rocket.xCgNoMotor = 1.1986; % [m] OVERRIDE xCg without motor
rocket.lengthCenterNoMot = 1.7840; % [m] OVERRIDE Center length - no nose, no motor
+% 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
+
%% 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 8cdcf2b5942b6f6ef50f8c2a627b7111452abc46..2f949bfb46c9b09dd02fea6a1c87253e9c6c5b20 100644
--- a/missions/2022_Pyxis_Portugal_October/config/rocketConfig.m
+++ b/missions/2022_Pyxis_Portugal_October/config/rocketConfig.m
@@ -16,6 +16,11 @@ rocket.inertiaNoMotor = [0.06303; 9.62497; 9.62524]; % [kg*m^2] OVERRIDE i
rocket.xCgNoMotor = 1.2239; % [m] OVERRIDE xCg without motor
rocket.lengthCenterNoMot = 1.4470; % [m] OVERRIDE Center length - no nose, no motor
+% 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
+
%% 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 bec3d20b753eb2ec6b956c9924e12353c7cd6e2b..ee3a3c71bd73ab263db92f3e929db488a6a5735c 100644
--- a/missions/2022_Pyxis_Roccaraso_September/config/rocketConfig.m
+++ b/missions/2022_Pyxis_Roccaraso_September/config/rocketConfig.m
@@ -18,6 +18,11 @@ rocket.xCgNoMotor = 1.2957; % [m]
% settings.Lcenter - motors(iMotor).L/1000
rocket.lengthCenterNoMot = 1.61; % [m] OVERRIDE Center length - no nose, no motor
+% 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
+
%% 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 610966af09dd387c856d5e559e8b6bd6020f4e8e..401c415be5e782af00b4318e62db4d13ea6ef5ca 100644
--- a/missions/2023_Gemini_Portugal_October/config/rocketConfig.m
+++ b/missions/2023_Gemini_Portugal_October/config/rocketConfig.m
@@ -15,6 +15,12 @@ rocket.inertiaNoMotor = [0.06535397; 17.21019828; 17.21056483]; % [kg*m^2]
rocket.xCgNoMotor = 1.254; % [m] OVERRIDE xCg without motor
rocket.lengthCenterNoMot = 1.517; % [m] OVERRIDE Center length - no nose, no motor
+% 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
+
+
%% 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 600065acce5a8ab60dc9e917019745567596d1d1..fc2715bc0dd7d61dd740e20b3138c8552440dcf1 100644
--- a/missions/2023_Gemini_Roccaraso_September/config/rocketConfig.m
+++ b/missions/2023_Gemini_Roccaraso_September/config/rocketConfig.m
@@ -15,6 +15,11 @@ rocket.inertiaNoMotor = [0.06535397; 12.07664659; 12.07701314]; % [kg*m^2]
rocket.xCgNoMotor = 1.149; % [m] OVERRIDE xCg without motor
rocket.lengthCenterNoMot = 1.517; % [m] OVERRIDE Center length - no nose, no motor
+% 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
+
%% 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 2369c08ce6c490b4ff849c682698f0d112a784d3..f87640c176ca52f0ab3274f1b32602462a1489ff 100644
--- a/missions/2024_Lyra_Portugal_October/config/rocketConfig.m
+++ b/missions/2024_Lyra_Portugal_October/config/rocketConfig.m
@@ -9,6 +9,11 @@ rocket.inertiaNoMotor = []; % [kg*m^
rocket.xCgNoMotor = []; % [m] OVERRIDE xCg without motor
rocket.lengthCenterNoMot = []; % [m] OVERRIDE Center length - no nose, no motor
+% 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
+
%% 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 b2ca5cb545dec731f15e540e33c3f05711f8e027..2939db0ce6550575817cdd355d8b2f6ca2e68943 100644
--- a/missions/2024_Lyra_Roccaraso_September/config/rocketConfig.m
+++ b/missions/2024_Lyra_Roccaraso_September/config/rocketConfig.m
@@ -15,6 +15,11 @@ rocket.lengthCenterNoMot = []; % [m]
% rocket.xCgNoMotor = 1.28; % [m] OVERRIDE xCg without motor
% rocket.lengthCenterNoMot = 1.778; % [m] OVERRIDE Center length - no nose, no motor
+% 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
+
%% 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 c8791602b6261e955857793796d59d896bd004bc..6a13ec2512f1ba80b938af94064c3038be076bfd 100644
--- a/missions/2025_Orion_Portugal_October/config/rocketConfig.m
+++ b/missions/2025_Orion_Portugal_October/config/rocketConfig.m
@@ -3,12 +3,17 @@
%% ROCKET - OVERRIDES BAYS CONFIG
rocket = Rocket();
-rocket.diameter = 0.15; % [m] Rocket diameter
+rocket.diameter = 0.15; % [m] Rocket diameter
% rocket.massNoMotor = []; % [kg] OVERRIDE mass without motor
% rocket.inertiaNoMotor = []; % [kg*m^2] OVERRIDE inertia without motor - body axes reference
% rocket.xcgNoMotor = []; % [m] OVERRIDE xCg without motor
% rocket.lengthCenterNoMot = []; % [m] OVERRIDE Center length - no nose, no motor
+% 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
+
%% PRF - Includes Parafoil + Nose
parafoil = Parafoil();
@@ -69,7 +74,7 @@ airbrakes.servoTau = 0.0374588;
%% MOTOR
motor = Motor();
-motor.name = 'HRE_ARM_OPT_3_Update';
+motor.name = 'HRE_ARM_EuRoC_2024';
motor.cutoffTime = []; % [s] OVERRIDE Cutoff time
motor.ignitionTransient = 0.3; % [s] Ignition transient
diff --git a/missions/2025_Orion_Roccaraso_September/config/rocketConfig.m b/missions/2025_Orion_Roccaraso_September/config/rocketConfig.m
index dfc372f3e3e1f47af69fd4b9e1dc3d80f730052a..c4e1ffcee38a736e09fe06543010f7699fe3a553 100644
--- a/missions/2025_Orion_Roccaraso_September/config/rocketConfig.m
+++ b/missions/2025_Orion_Roccaraso_September/config/rocketConfig.m
@@ -15,6 +15,11 @@ rocket.lengthCenterNoMot = []; % [m]
% rocket.xCgNoMotor = 1.28; % [m] OVERRIDE xCg without motor
% rocket.lengthCenterNoMot = 1.778; % [m] OVERRIDE Center length - no nose, no motor
+% 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
+
%% PLD - Includes Parafoil + Nose
parafoil = Parafoil();