Draft: Alpha phi

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