[code-refactoring][missions] created aerodynamicsConfig and updated engineConfig, settingsConfig

- wip for flags
- {settingsConfig} changed features struct into settings

missions/2024_Lyra_Roccaraso_September/config/aerodynamicsConfig.m

+% CONFIG - This script sets up control parameters
+
+%% AERODYNAMICS DETAILS
+% These coefficients are obtained using MISSILE DATCOM, check simulator/README.md for further details.
+
+features = loadConfig("settingsConfig.m");
+
+if not(isfield(aerodynamics,'autoMatProt_flag')) || features.flags.autoMatProt
+    
+    % Coefficients
+    Coeffs = load(filename_coeffs);
+    aerodynamics.Coeffs = Coeffs.CoeffsTot;
+
+    % Geometry
+    aerodynamics.Geometry = Coeffs.Geometry;
+    aerodynamics.Geometry.xcg = Coeffs.Geometry.xcg';
+
+    % State
+    aerodynamics.State.Alphas = Coeffs.State.Alphas';
+    aerodynamics.State.Betas = Coeffs.State.Betas';
+    aerodynamics.State.Altitudes = Coeffs.State.Altitudes';
+    aerodynamics.State.Machs = Coeffs.State.Machs';
+    aerodynamics.State.Controls = Coeffs.State.hprot';
+    aerodynamics.State.xcgTime = Coeffs.State.xcgTime';
+    clear('Coeffs');
+
+    CoeffHighAOA = load('HighAOA.mat'); 
+    aerodynamics.highAOA.Coeffs = CoeffHighAOA.CoeffsTot; 
+    aerodynamics.highAOA.State.Alphas = CoeffHighAOA.State.Alphas';
+    aerodynamics.highAOA.State.Betas = CoeffHighAOA.State.Betas'; 
+    aerodynamics.highAOA.State.Altitudes = CoeffHighAOA.State.Altitudes'; 
+    aerodynamics.highAOA.State.Machs = CoeffHighAOA.State.Machs';
+    aerodynamics.highAOA.State.Controls = CoeffHighAOA.State.hprot';
+    aerodynamics.highAOA.State.xcgTime = CoeffHighAOA.State.xcgTime';
+    clear('CoeffHighAOA');
+
+    aerodynamics.highAOA.tb = aerodynamics.tb; 
+    aerodynamics.highAOA.timeEngineCut = aerodynamics.timeEngineCut; 
+end
\ No newline at end of file

missions/2024_Lyra_Roccaraso_September/config/engineConfig.m

@@ -4,3 +4,5 @@ engine.name = 'HRE_FURIA-Rv2-T04T03';
 engine.burnTime = inf;                                 % [s] Burn duration
 engine.ignitionTime = 000; %0.4;                       % [s] Ignition transient
 engine.cutOffTime = 000; %0.3;                         % [s] Cut-off transient
+
+filename_coeffs = strcat(engine.name, '.mat');
\ No newline at end of file

missions/2024_Lyra_Roccaraso_September/config/settingsConfig.m

@@ -4,4 +4,6 @@
 % mission (e.g. whether a specific algorithm is used, the engine type, 
 % flags...)
 
-features.engineType = 'hybrid';      % [-] choices are: solid, hybrid
+settings.engineType = 'hybrid';      % [-] choices are: solid, hybrid
\ No newline at end of file
+
+settings.flags.autoMatProt = false;
\ No newline at end of file