diff --git a/classes/Bay.m b/classes/Bay.m
index a364fa039a1d2e0b6f973afe495df7e12d087eb9..180b279dc12e0ba8893ec5292ddcfd79c5743121 100644
--- a/classes/Bay.m
+++ b/classes/Bay.m
@@ -1,7 +1,6 @@
 classdef Bay < Component & matlab.mixin.Heterogeneous
-    % An abstraction class that enables a standardized management of data
-    %   Properties and methods implemented in the Component class will 
-    %   impact every physical component of the rocket (e.g. motor, elc ...)
+% Bay: Represents an abstraction layer for all bays
+%   Arrays of bay subclasses will be represented as [mxn Bay] arrays
 
     properties(Abstract)
         position    % [m] Absolute position, relative to previous component
diff --git a/classes/Component.m b/classes/Component.m
index ea0b56b8b09563254e94f9eed4769998b602892f..6bb051022216469a0c2694bb7c81fa022cf87833 100644
--- a/classes/Component.m
+++ b/classes/Component.m
@@ -1,7 +1,7 @@
 classdef Component < Config
-    %COMPONENT Summary of this class goes here
-    %   Detailed explanation goes here
-    
+% Component: Represents an abstraction layer for all components
+%   Components standardize object construction, config and data loading
+
     properties(Abstract, Access = protected) 
         % Insert dependencies here
         mission Mission
diff --git a/classes/Config.m b/classes/Config.m
index 0042af3dc0e9111361e7ad3b691a94062a824a69..7995125bce9b18b34df494e5632f85b25498acb6 100644
--- a/classes/Config.m
+++ b/classes/Config.m
@@ -1,7 +1,7 @@
 classdef(Abstract) Config < handle
-    % An abstraction class that enables a standardized management of data
-    %   Properties and methods implemented in the Config class will impact
-    %   every data class in the framework (e.g. Component and its subclasses)
+% Config: Represents an abstraction layer for all config-dependent Classes
+%   Config standardizes property management and declares fundemental
+%   properties (see doc for more info)
 
     properties(Abstract, Access = protected)
         configName {mustBeTextScalar}
diff --git a/classes/Mission.m b/classes/Mission.m
index c18fd9f8109a02db9e083921dae67977a25cb52a..d3b25085793431c12d3b85341275e127c818f321 100644
--- a/classes/Mission.m
+++ b/classes/Mission.m
@@ -1,11 +1,10 @@
 classdef Mission < Config
-    % Class containing names and paths to access mission files
-    %   This should be the first class to be created, 
-    %   when running a tool.
-    %
-    % To get an empty Mission, run "Mission()", or "Mission(false)"
-    % To get an initialized Mission, run "Mission(true)"
-    %   Where the argument specifies whether to read config files or not
+% Config: Contains names and paths needed to access mission-dependent config files
+%
+% To get an empty Mission, run "Mission()", or "Mission(false)"
+% To get an initialized Mission, run "Mission(true)"
+%   Where the argument specifies whether to read config files or not
+
 
     properties
         name % Mission name, used to access <mission> folder
diff --git a/classes/Rocket.m b/classes/Rocket.m
index 99affd78dd25488291ff9826706095af581b6c05..b56e56ee22edec5378da9cc95245061581d835cd 100644
--- a/classes/Rocket.m
+++ b/classes/Rocket.m
@@ -1,7 +1,15 @@
 classdef Rocket < Component
-    %ROCKET Summary of this class goes here
-    %   Detailed explanation goes here
-    
+% Rocket: Contains and manages all bays
+%
+%   Constructor:
+%       - Rocket: Creates an instance of the Rocket class.
+%           Loaded config: rocketConfig.m > rocket (for overrides)
+%           Loaded data: -
+%           Arguments:
+%               - mission: Mission, mission object
+%               - varIn: (optional) config source. Alternative to config.m
+%               file
+
     properties
         nose        Nose        = Nose()
         payload     Payload     = Payload()
@@ -10,8 +18,6 @@ classdef Rocket < Component
         airbrakes   Airbrakes   = Airbrakes()
         motor       Motor       = Motor()
         rear        Rear        = Rear()
-        % fincan      Fincan      = Fincan()
-        % boat        Boat        = Boat()
 
         pitot       Pitot       = Pitot()
 
diff --git a/classes/Settings.m b/classes/Settings.m
index 7255fa5b849593134a85f7c8b88d865e2bf8e04e..e7a9e8d96f183838cec19f1badc9804ff4dc18fb 100644
--- a/classes/Settings.m
+++ b/classes/Settings.m
@@ -1,5 +1,16 @@
 classdef Settings < Config & dynamicprops
-        
+% Settings: Provides standardized way of loading config files
+%   Looks for files in missions > settings for global settings
+%   Looks for files in caller's folder otherwise
+%
+%   Constructor:
+%       - Settings: Creates an instance of the Settings class.
+%           Loaded config: -
+%           Loaded data: -
+%           Arguments:
+%               - configNames: config file names. Accepts shortened version
+%                   e.g: ode -> odeConfig.m
+
     properties(Access = protected)
         configPath = ''
         configName = ''
diff --git a/classes/bays/Airbrakes.m b/classes/bays/Airbrakes.m
index c4d67b5ca8a8766a60976ef8d1572df3a2bdf803..34a5405e7276dcfb13021215c93fd1dab8c6347f 100644
--- a/classes/bays/Airbrakes.m
+++ b/classes/bays/Airbrakes.m
@@ -1,25 +1,33 @@
 classdef Airbrakes < Bay
-    %AIRBRAKES Summary of this class goes here
-    %   Detailed explanation goes here
+% Airbrakes: Represents airbrakes configuration for a rocket.
+%
+%   Constructor:
+%       - Airbrakes: Creates an instance of the Airbrakes class.
+%           Loaded config: rocketConfig.m > airbrakes
+%           Loaded data: -
+%           Arguments:
+%               - mission: Mission, mission object
+%               - varIn: (optional) config source. Alternative to config.m
+%               file
     
     properties
-        n               double         % [-] number of brakes
-        thickness       double         % [m] brakes thickness        
-        width           double         % [m] brakes width
-        xDistance       double         % [m] axial position from nosecone base
-        multipleAB      {islogical}    % If true, multiple and smooth airbrakes opening will be simulated
-        opening         double         % aerobrakes, 1-2-3 for 0%, 50% or 100% opened
-        deltaTime       double         % aerobrakes, configurations usage time
-        minTime         double         % [s] time after which the airbrakes can be used
-        maxMach         double         % [-] Maximum Mach at which airbrakes can be used
-        servoOmega      double         % [rad/s] Servo-motor angular velocity
-        height          double         % [m] Block airbrakes opening coordinate ( First entry must be 0! )
-        position    % [m] Offset with respect to other bays (negative -> shift forward)
-        length      % [m] Total bay length
-        diameter    % [m] Diameter of the bay
-        mass        % [kg] Total bay mass
-        inertia     % [kg*m^2] Total bay inertia (Body reference)
-        xCg         % [m] Cg relative to bay upper side
+        n               double          % [-] number of brakes
+        thickness       double          % [m] brakes thickness
+        width           double          % [m] brakes width
+        xDistance       double          % [m] axial position from nosecone base
+        multipleAB      {islogical}     % If true, multiple and smooth airbrakes opening will be simulated
+        opening         double          % aerobrakes, 1-2-3 for 0%, 50% or 100% opened
+        deltaTime       double          % aerobrakes, configurations usage time
+        minTime         double          % [s] time after which the airbrakes can be used
+        maxMach         double          % [-] Maximum Mach at which airbrakes can be used
+        servoOmega      double          % [rad/s] Servo-motor angular velocity
+        height          double          % [m] Block airbrakes opening coordinate ( First entry must be 0! )
+        position                        % [m] Offset with respect to other bays (negative -> shift forward)
+        length                          % [m] Total bay length
+        diameter                        % [m] Diameter of the bay
+        mass                            % [kg] Total bay mass
+        inertia                         % [kg*m^2] Total bay inertia (Body reference)
+        xCg                             % [m] Cg relative to bay upper side
     end
     
     properties(Access = protected)
diff --git a/classes/bays/Boat.m b/classes/bays/Boat.m
deleted file mode 100644
index 068eff1933677704dbbfd29321fb2f3512d09ca7..0000000000000000000000000000000000000000
--- a/classes/bays/Boat.m
+++ /dev/null
@@ -1,29 +0,0 @@
-classdef Boat < Bay
-    %GEOMETRY Summary of this class goes here
-    %   Detailed explanation goes here
-    properties
-        type        {mustBeMember(type, {'', 'CONE', 'OGIVE'})} = ''    % [] Boat type 
-        position    % [m] Absolute position, relative to nose base
-        length                                                          % [m] Total bay length
-        diameter                                                        % [m] Final diameter of the bay
-        mass                                                            % [kg] Total bay mass
-        inertia                                                         % [kg*m^2] Total bay inertia (Body reference)
-        xCg                                                             % [m] Cg relative to bay upper side
-    end
-
-    properties(Access = protected)
-        configName = 'rocketConfig.m'
-        variableName = 'boat'
-        mission Mission = Mission()
-    end
-
-    methods
-        function obj = Boat(mission, varIn)
-            arguments(Input)
-                mission Mission = Mission()
-                varIn = []
-            end
-            obj@Bay(mission, varIn);
-        end
-    end
-end
\ No newline at end of file
diff --git a/classes/bays/Electronics.m b/classes/bays/Electronics.m
index 3da511198d51ad5214082d982712d382c883fa9b..c7b419e29cb564fb49e7229cd8e1af6ea6d60c23 100644
--- a/classes/bays/Electronics.m
+++ b/classes/bays/Electronics.m
@@ -1,7 +1,14 @@
 classdef Electronics < Bay
-    % An abstraction class that enables a standardized management of data
-    %   Properties and methods implemented in the Component class will 
-    %   impact every physical component of the rocket (e.g. motor, elc ...)
+% Electronics: Represents electronics configuration for a rocket.
+%
+%   Constructor:
+%       - Electronics: Creates an instance of the Electronics class.
+%           Loaded config: rocketConfig.m > electronics
+%           Loaded data: -
+%           Arguments:
+%               - mission: Mission, mission object
+%               - varIn: (optional) config source. Alternative to config.m
+%               file
     properties
         offset = 0
         position    % [m] Absolute position, relative to nose base
diff --git a/classes/bays/Fincan.m b/classes/bays/Fincan.m
deleted file mode 100644
index fba4ea2c371793b6fea071ec0636576ff0e621eb..0000000000000000000000000000000000000000
--- a/classes/bays/Fincan.m
+++ /dev/null
@@ -1,38 +0,0 @@
-classdef Fincan < Bay
-    %FINS Summary of this class goes here
-    %   Detailed explanation goes here
-
-    properties
-        mass                                % [kg] Fins mass 
-        position                            % [m] Absolute position, relative to nose base
-        length 
-        diameter 
-        inertia
-        xCg                                 % [m] Cg from fins root chord tip
-        rootChord               double      % [m] attached chord length
-        freeChord               double      % [m] free chord length
-        height                  double      % [m] fin heigth
-        deltaXFreeChord         double      % [m] start of Chord 2 measured from start of Chord 1
-        nPanel                  double      % [m] number of fins
-        leadingEdgeRadius       double      % [deg] Leading edge radius at each span station
-        axialDistance           double      % [m] distance between end of root chord and end of center body
-        semiThickness           double      % [m] fin semi-thickness
-        maxThicknessPosition    double      % [m] Fraction of chord from leading edge to max thickness
-    end
-
-    properties(Access = protected)
-        configName = 'rocketConfig.m'
-        variableName = 'fincan'
-        mission Mission = Mission()
-    end
-
-    methods
-        function obj = Fincan(mission, varIn)
-            arguments(Input)
-                mission Mission = Mission()
-                varIn = []
-            end
-            obj@Bay(mission, varIn);
-        end
-    end
-end
\ No newline at end of file
diff --git a/classes/bays/Motor.m b/classes/bays/Motor.m
index 41dfde0c3fcb586844f6503c8c83a16669adfd50..d58b4e135b0f90239dfd8eefb1e9d9a8623ff47b 100644
--- a/classes/bays/Motor.m
+++ b/classes/bays/Motor.m
@@ -1,7 +1,14 @@
 classdef Motor < Bay
-    %MOTOR Summary of this class goes here
-    %   Detailed explanation goes here
-
+% Motor: Represents the motor configuration for a rocket.
+%
+%   Constructor:
+%       - Motor: Creates an instance of the Motor class.
+%           Loaded config: rocketConfig.m > motor
+%           Loaded data: motors.mat
+%           Arguments:
+%               - mission: Mission, mission object
+%               - varIn: (optional) config source. Alternative to config.m file
+  
     properties
         name                {mustBeTextScalar} = '' % [-]  Motor name
         position    % [m] Absolute position, relative to nose base
@@ -51,7 +58,7 @@ classdef Motor < Bay
 
         function mass = get.mass(obj)
             mass = obj.propellantMass + ... 
-                obj.structureMass; %+ obj.fuselageMass;
+                obj.structureMass + obj.fuselageMass;
         end
 
         function fuselageXCg = get.fuselageXCg(obj)
diff --git a/classes/bays/Nose.m b/classes/bays/Nose.m
index 8906d68f53beef1dc904aa47bcfe918e018268a6..1bdc032e84ecf968568a8a5f963d8c74e7ff7f50 100644
--- a/classes/bays/Nose.m
+++ b/classes/bays/Nose.m
@@ -1,6 +1,14 @@
 classdef Nose < Bay
-    %NOSE Summary of this class goes here
-    %   Detailed explanation goes here
+% Nose: Represents nose configuration for a rocket.
+%
+%   Constructor:
+%       - Nose: Creates an instance of the Nose class.
+%           Loaded config: rocketConfig.m > nose
+%           Loaded data: -
+%           Arguments:
+%               - mission: Mission, mission object
+%               - varIn: (optional) config source. Alternative to config.m
+%               file
 
     properties
         ogiveType   {mustBeMember(ogiveType, {'', 'CONE', 'OGIVE', ...
diff --git a/classes/bays/Payload.m b/classes/bays/Payload.m
index 3db6c22d3f7ea066a821ff49dde1e2553b644c2d..1c94ad74993995d77424fa70636ca75d5d58edfc 100644
--- a/classes/bays/Payload.m
+++ b/classes/bays/Payload.m
@@ -1,6 +1,15 @@
 classdef Payload < Bay
-    %GEOMETRY Summary of this class goes here
-    %   Detailed explanation goes here
+% Payload: Represents payload configuration for a rocket.
+%
+%   Constructor:
+%       - Payload: Creates an instance of the Payload class.
+%           Loaded config: rocketConfig.m > payload
+%           Loaded data: -
+%           Arguments:
+%               - mission: Mission, mission object
+%               - varIn: (optional) config source. Alternative to config.m
+%               file
+
     properties
         position    % [m] Absolute position, relative to nose base
         length      % [m] Total bay length
diff --git a/classes/bays/Rear.m b/classes/bays/Rear.m
index cd0b66d1ebab0a4a7fd00f28cc3469fad2446df2..33f1b9e10d9f7cb077ee6c437ece03de876788af 100644
--- a/classes/bays/Rear.m
+++ b/classes/bays/Rear.m
@@ -1,7 +1,15 @@
 classdef Rear < Bay
-    %REAR Summary of this class goes here
-    %   Detailed explanation goes here
-    
+% Rear: Represents fincan + boat configuration for a rocket.
+%
+%   Constructor:
+%       - Rear: Creates an instance of the Rear class.
+%           Loaded config: rocketConfig.m > rear
+%           Loaded data: -
+%           Arguments:
+%               - mission: Mission, mission object
+%               - varIn: (optional) config source. Alternative to config.m
+%               file
+
     properties
         position                                                        % [m] Absolute position, relative to nose base
         length                                                          % [m] Total bay length
diff --git a/classes/bays/Recovery.m b/classes/bays/Recovery.m
index 2c34c587a52d9c87df7713923c5c598acfa1a45a..1947b29244b270e1dc496960b9239c064d961e73 100644
--- a/classes/bays/Recovery.m
+++ b/classes/bays/Recovery.m
@@ -1,6 +1,15 @@
 classdef Recovery < Bay
-    %GEOMETRY Summary of this class goes here
-    %   Detailed explanation goes here
+% Recovery: Represents recovery configuration for a rocket.
+%
+%   Constructor:
+%       - Recovery: Creates an instance of the Recovery class.
+%           Loaded config: rocketConfig.m > recovery
+%           Loaded data: -
+%           Arguments:
+%               - mission: Mission, mission object
+%               - varIn: (optional) config source. Alternative to config.m
+%               file
+
     properties
         position    % [m] Absolute position, relative to nose base
         length      % [m] Total bay length
diff --git a/classes/old/Environment.asv b/classes/old/Environment.asv
deleted file mode 100644
index 32e64319ce3e8e789f7d43ca44604a53fdacd777..0000000000000000000000000000000000000000
--- a/classes/old/Environment.asv
+++ /dev/null
@@ -1,54 +0,0 @@
-classdef Environment < Config
-    %ENVIRONMENT Summary of this class goes here
-    %   Detailed explanation goes here
-
-    properties
-        lat0            double       % [deg] Launchpad latitude
-        lon0            double       % [deg] Launchpad longitude
-        z0              double       % [m] Launchpad Altitude
-        pin1Length      double       % [m] Distance from the upper pin to the upper tank cap
-        pin2Length      double       % [m] Distance from the lower pin to the lower tank cap   
-        rampLength      double       % [m] Total launchpad length
-        temperature     double       % [deg] Ground temperature
-        pressure        double       % [Pa] Ground pressure
-        rho             double       % [Kg/m^3] Gorund air density
-    end
-
-    properties(Dependent)
-        g0                      double       % [-] Gravity costant at launch latitude and altitude
-        pinDistance             double       % [m] Distance of the upper pin from the rail base (upper pin-boat + boat-rail base)
-        effectiveRampLength     double       % [m] Total launchpad length
-    end
-
-    properties(Access = protected)
-        configName = 'environmentConfig.m'
-        mission Mission
-        motor Motor
-    end
-
-    methods
-        function obj = Environment(mission, motor)
-            arguments
-                mission Mission = Mission()
-                motor Motor = Mission()
-            end
-            obj.mission = mission;
-            obj.motor = motor;
-            if nargin == 0, return; end
-            obj.loadConfig();
-        end
-
-        function g0 = get.g0(obj)
-            g0 = gravitywgs84(obj.z0, obj.lat0);
-        end
-
-        function pinDistance = get.pinDistance(obj)
-            pinDistance = obj.pin1Length + obj.pin2Length ... 
-                + obj.motor.tankLength;
-        end
-
-        function effectiveRampLength = get.effectiveRampLength(obj)
-            effectiveRampLength = gravitywgs84(obj.z0, obj.lat0);
-        end
-    end
-end
\ No newline at end of file
diff --git a/classes/old/Geometries.m b/classes/old/Geometries.m
deleted file mode 100644
index 1f2706deb20b0e5be5a9faef709cfd48c0ef6174..0000000000000000000000000000000000000000
--- a/classes/old/Geometries.m
+++ /dev/null
@@ -1,57 +0,0 @@
-classdef(InferiorClasses = {?Boat, ?Center, ?Nose, ?Pitot, ?Fins, ?Protuberances}) ...
-    Geometries < Config
-    %GEOMETRY Summary of this class goes here
-    %   Detailed explanation goes here
-
-    properties
-        boat            Boat            = Boat()
-        center          Center          = Center()  % Center (Excluding motor)
-        nose            Nose            = Nose()
-        pitot           Pitot           = Pitot()
-        fins            Fins            = Fins()
-        protuberances   Protuberances   = Protuberances()
-        nXCg            {mustBePositive, mustBeInteger}
-        xCgNoMotor      double
-    end
-
-    properties(Dependent)                           % Center + motor length
-        length          double                      
-        xCg             (1,:) double
-    end
-
-    properties(Access = protected)
-        configName = 'geometryConfig.m'
-        mission         Mission
-        motor           Motor
-        mass            Masses
-    end
-
-    methods
-        function obj = Geometries(mission, motor, mass)
-            %GEOMETRY Construct an instance of this class
-            %   Detailed explanation goes here
-            %obj;
-            arguments (Input)
-                mission Mission = Mission()
-                motor Motor = Motor()
-                mass Masses = Masses()
-            end
-            obj.mission = mission;
-            obj.motor = motor;
-            obj.mass = mass;
-            if nargin == 0, return;  end
-            if nargin ~= 3, error('Wrong input arguments count: only specify 2 arguments'); end
-            obj.loadConfig();
-        end
-        
-        function xCg = get.xCg(obj)
-            xCg = (obj.motor.totalMass.*(obj.center.length + obj.motor.xCg) + ...
-                obj.mass.noMotor*obj.xCgNoMotor)./(obj.motor.totalMass + obj.mass.noMotor);
-        end
-
-        function length = get.length(obj)
-            length = obj.center.length + ...
-                obj.motor.totalLength;
-        end
-    end
-end
\ No newline at end of file
diff --git a/classes/old/Masses.m b/classes/old/Masses.m
deleted file mode 100644
index 5114576a4c86d8e6c19bdd7390daf99d2dd55c2a..0000000000000000000000000000000000000000
--- a/classes/old/Masses.m
+++ /dev/null
@@ -1,52 +0,0 @@
-classdef Masses < Config
-    %MASS Summary of this class goes here
-    %   Detailed explanation goes here
-
-    properties
-        boat            % [kg] BoatTail Mass
-        center          % [kg] Center Mass (no motor)
-        nose            % [kg] Nosecone Mass
-        fins            % [kg] Finset Mass
-    end
-
-    properties(Dependent)
-        noMotor         % [kg] Total mass (no motor)
-        structure       % [kg] Total structural Mass
-        total           % [kg] Total mass (in time)
-    end
-
-    properties(Access = protected)
-        configName = 'massConfig.m'
-        mission Mission
-        motor Motor
-    end
-
-    methods
-        function obj = Masses(mission, motor)
-            arguments (Input)
-                mission Mission = Mission()
-                motor Motor = Motor()
-            end
-            obj.mission = mission;
-            obj.motor = motor;
-            if nargin == 0, return;  end
-            if nargin ~= 2, error('Wrong input arguments count: only specify 2 arguments'); end
-            obj.loadConfig();
-        end
-
-        function noMotor = get.noMotor(obj)
-            noMotor = obj.boat + obj.center + ...
-                obj.nose + obj.fins;
-        end
-
-        function structure = get.structure(obj)
-            structure = obj.noMotor + ...
-                obj.motor.structureMass;
-        end
-
-        function total = get.total(obj)
-            total = obj.noMotor + ...
-                obj.motor.totalMass;
-        end
-    end
-end
\ No newline at end of file
diff --git a/tests/argValidation.m b/tests/argValidation.m
deleted file mode 100644
index 96633f8ad9a7f00d4c42f0fb1c77b8c65f3dece4..0000000000000000000000000000000000000000
--- a/tests/argValidation.m
+++ /dev/null
@@ -1,11 +0,0 @@
-function test(in)
-    arguments(Input)
-        in Config {mustBeConfig}
-    end
-    disp(in.a);
-end
-
-function mustBeConfig(obj)
-    if ~isa(obj, 'Config'), error('suca');
-    end
-end
\ No newline at end of file
diff --git a/tests/speedBenchmark.asv b/tests/speedBenchmark.asv
deleted file mode 100644
index 1388be0e6f1ef8be1f34f7e9237e143556ce35e9..0000000000000000000000000000000000000000
--- a/tests/speedBenchmark.asv
+++ /dev/null
@@ -1,22 +0,0 @@
-ms = Mission(true);
-
-cl = Motor(ms);
-st = struct(cl);
-
-len = length(st.xCg);
-a = zeros(1, len);
-b = zeros(1, len);
-
-tic  
-    for i = 1:len
-        a(i) = cl.xCg(i);
-    end
-classTime = toc;
-
-tic  
-    for i = 1:len
-        b(i) = st.xCg(i);
-    end
-structTime = toc;
-
-disp(strcat('classTime: ', classTime));
\ No newline at end of file
diff --git a/tests/speedBenchmark.m b/tests/speedBenchmark.m
deleted file mode 100644
index 5c2c39edc619e9584e9787817643767534da0b94..0000000000000000000000000000000000000000
--- a/tests/speedBenchmark.m
+++ /dev/null
@@ -1,32 +0,0 @@
-clear; clc; close all;
-
-ms = Mission(true);
-
-cl = Motor(ms);
-st = struct(cl);
-
-len = length(st.xCg);
-a = zeros(1, len);
-b = zeros(1, len);
-c = zeros(1, len);
-d = zeros(1, len);
-
-tic  
-a = cl.xCg;
-fprintf('stdAssignment, class: %f s\n', toc);
-
-tic  
-c = st.xCg;
-fprintf('stdAssignment, struct: %f s\n', toc);
-
-tic  
-for i = 1:len
-    b(i) = cl.xCg(i);
-end
-fprintf('elementWiseAssignment, class: %f s\n', toc);
-
-tic  
-for i = 1:len
-    d(i) = st.xCg(i);
-end
-fprintf('elementWiseAssignment, struct: %f s\n', toc);
\ No newline at end of file