[refactoring-ode][classes] Improved object constructor

classes/Component.m

@@ -28,48 +28,12 @@ classdef Component < Config
                 varName = strtok(fileName, 'C');
             end
 
-            [m, n] = size(varsIn.(varName));
-            objMatrix(m,n) = obj;
-
-            for i = 1:m
-                for j = 1:n
-                    varIn.(varName) = varsIn.(varName)(i,j);
-                    objMatrix(i,j).loadConfig(varIn);
-                end
-            end
-            obj = objMatrix;
+            [varsIn.(varName).mission] = deal(mission);
+            obj = varsIn.(varName);
         end
     end
     
     methods(Access = protected)
-        function loadConfig(obj, varargin)
-            % This method loads desired configs into calling component.
-            % The component can chose between:
-            %   - Only specifying the configName (name of the config file):
-            %       The loader will look for a variable named like the
-            %       config file.
-            %   - Specifying both the configName and the variableName:
-            %       Useful for when you want to group multiple small
-            %       objects into a larger config file
-            %
-            % Syntax:
-            %   obj.loadConfig()        - To load from a config file
-            %   obj.loadConfig(vars)    - To load from given variables
-
-            fileName = obj.configName;
-            varName = obj.variableName;
-            if isempty(varName), varName = strtok(fileName, 'C'); end
-
-            if nargin == 2, configObj = varargin{end}.(varName);
-            else, configObj = obj.getConfig(); end
-
-            fields = obj.getProperties('writable');
-            for j = 1:size(fields, 2)
-                if isempty(configObj.(fields{j})), continue; end
-                obj.(fields{j}) = configObj.(fields{j}); 
-            end
-        end
-
         function outputVariables = getConfig(obj)
             fileName = obj.configName;
             filePath = obj.mission.configPath;

classes/Rocket.m

@@ -229,12 +229,13 @@ classdef Rocket < Component
                 options.checkGeometry       logical = true
             end
             obj@Component(mission, varIn);
-            obj.mission = mission;
 
             %% Loading data
             if nargin == 0
                 return;
             end
+            obj.mission = mission;
+
             vars             = obj.getConfig(); % Load config once and apply to other bays
             obj.payload      = Payload(mission, vars);
             obj.recovery     = Recovery(mission, vars);

classes/bays/Motor.m

@@ -30,7 +30,7 @@ classdef Motor < Bay
         ae                  double                  % [Pa] Eflux Area
     end
 
-    properties(Dependent)
+    properties
         mass                                        % [kg] Total Motor mass
         fuselageXCg         double                  % [m]  xcg of the engine fuselage only from tank tip
     end
@@ -53,20 +53,19 @@ classdef Motor < Bay
             end
             obj@Bay(mission, varIn);
             obj.loadData();
+            obj.updateAll();
         end
 
         function set.name(obj, name)
             obj.name = name;
             obj.loadData();
+            obj.updateAll();
         end
 
-        function mass = get.mass(obj)
-            mass = obj.propellantMass + obj.structureMass;
-        end
-
-        function fuselageXCg = get.fuselageXCg(obj)
-            fuselageXCg = (obj.length - ...
+        function updateAll(obj)
+            obj.fuselageXCg = (obj.length - ...
                 obj.tankLength)/2 + obj.tankLength;
+            obj.mass = obj.propellantMass + obj.structureMass;
         end
     end
 

classes/components/Environment.m

@@ -56,15 +56,19 @@ classdef Environment < Component
             obj.omega = deg2rad(obj.omega);
             obj.phi = deg2rad(obj.phi);
 
+            obj.updateAll();
+        end
+    end
+    
+    % Updaters
+    methods
+        function updateAll(obj)
             obj.updateG0;
             obj.updatePinDistance;
             obj.updateRamp;
             obj.updateLocal;
         end
-    end
 
-    % Updaters
-    methods
         function obj = updateG0(obj)
             obj.g0 = gravitywgs84(obj.z0, obj.lat0);
         end

classes/components/WindCustom.m

@@ -38,7 +38,7 @@ classdef WindCustom < Component
                 varIn = []
             end
             obj@Component(mission, varIn);
-            obj.setData();
+            obj.updateAll();
         end
 
         function [uw, vw, ww] = getVels(obj, z)
@@ -57,7 +57,7 @@ classdef WindCustom < Component
             end
         end
 
-        function obj = setData(obj)
+        function updateAll(obj)
             s = length(obj.altitudes);
             magVector = nan(1,s);
             azVector = nan(1,s);

functions/eventFunctions/eventLanding.m

-function [value, isterminal, direction] = eventLanding(~, Y, ~, ~, ~, ~)
+function [value, isterminal, direction] = eventLanding(~, Y, varargin)
 %{
 eventLanding - Event function to stop simulation at landing checking when a
                value tends to zero; the value taken is to account is the