#+TITLE: Stewart Platform - Definition of the Architecture
:DRAWER:
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#+PROPERTY: header-args:matlab  :session *MATLAB*
#+PROPERTY: header-args:matlab+ :comments org
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* Introduction                                                          :ignore:
In this document is explained how the Stewart Platform architecture is defined.

Some efforts has been made such that the procedure for the definition of the Stewart Platform architecture is as logical and clear as possible.

When possible, the notations are compatible with the one used in cite:taghirad13_paral.

The definition of the Stewart platform is done in three main parts:
- First, the geometry if defined (Section [[sec:definition_geometry]])
- Then, the inertia of the mechanical elements are defined (Section [[sec:definition_inertia]])
- Finally, the Stiffness and Damping characteristics of the elements are defined (Section [[sec:definition_dynamics]])

In section [[sec:summary_initialization]], the procedure the initialize the Stewart platform is summarize and the associated Matlab code is shown.

Finally, all the Matlab function used to initialize the Stewart platform are described in section [[sec:functions]].

* Definition of the Stewart Platform Geometry
<<sec:definition_geometry>>
** Introduction                                                      :ignore:
Stewart platforms are generated in multiple steps:
- Definition of the frames
- Definition of the location of the joints
- Computation of the length and orientation of the struts
- Choice of the rest position of the mobile platform

This steps are detailed below.

** Frames Definition
We define 4 important *frames* (see Figure [[fig:frame_definition]]):
- $\{F\}$: Frame fixed to the *Fixed* base and located at the center of its bottom surface.
  This is used to fix the Stewart platform to some support.
- $\{M\}$: Frame fixed to the *Moving* platform and located at the center of its top surface.
  This is used to place things on top of the Stewart platform.
- $\{A\}$: Frame fixed to the fixed base.
- $\{B\}$: Frame fixed to the moving platform.

Even though frames $\{A\}$ and $\{B\}$ don't usually correspond to physical elements, they are of primary importance.
Firstly, they are used for the definition of the motion of the Mobile platform with respect to the fixed frame:
- In position: ${}^A\bm{P}_{B}$ (read: Position of frame $\{B\}$ expressed in frame $\{A\}$)
- In rotation: ${}^A\bm{R}_{B}$ (read: The rotation matrix that express the orientation of frame $\{B\}$ expressed in frame $\{A\}$)
The frames $\{A\}$ and $\{B\}$ are used for all the kinematic analysis (Jacobian, Stiffness matrix, ...).

Typical choice of $\{A\}$ and $\{B\}$ are:
- Center of mass of the payload
- Location where external forces are applied to the mobile platform (for instance when the mobile platform is in contact with a stiff environment)
- Center of the cube for the cubic configuration

The definition of the frames is done with the =initializeFramesPositions= function ([[sec:initializeFramesPositions][link]]);

#+name: fig:frame_definition
#+caption: Definition of the Frames for the Stewart Platform
#+attr_html: :width 500px
[[file:figs/frame_definition.png]]

** Location of the Spherical Joints
Then, we define the *location of the spherical joints* (see Figure [[fig:joint_location]]):
- $\bm{a}_{i}$ are the position of the spherical joints fixed to the fixed base
- $\bm{b}_{i}$ are the position of the spherical joints fixed to the moving platform

The location of the joints will define the Geometry of the Stewart platform.
Many characteristics of the platform depend on the location of the joints.

The location of the joints can be set to arbitrary positions or it can be computed to obtain specific configurations such as:
- A cubic configuration: function =generateCubicConfiguration= (described in [[file:cubic-configuration.org][this]] file)
- A symmetrical configuration

A function (=generateGeneralConfiguration=) to set the position of the joints on a circle is described [[sec:generateGeneralConfiguration][here]].

The location of the spherical joints are then given by ${}^{F}\bm{a}_{i}$ and ${}^{M}\bm{b}_{i}$.

#+name: fig:joint_location
#+caption: Position of the Spherical/Universal joints for the Stewart Platform
#+attr_html: :width 500px
[[file:figs/joint_location.png]]

** Length and orientation of the struts
From the location of the joints (${}^{F}\bm{a}_{i}$ and ${}^{M}\bm{b}_{i}$), we compute the length $l_i$ and orientation of each strut $\hat{\bm{s}}_i$ (unit vector aligned with the strut).
The length and orientation of each strut is represented in figure [[fig:length_orientation_struts]].

This is done with the =computeJointsPose= function ([[sec:computeJointsPose][link]]).

#+name: fig:length_orientation_struts
#+caption: Length $l_i$ and orientation $\hat{\bm{s}}_i$ of the Stewart platform struts
#+attr_html: :width 500px
[[file:figs/length_orientation_struts.png]]

** Rest Position of the Stewart platform
We may want to initialize the Stewart platform in some position and orientation that corresponds to its rest position.

To do so, we choose:
- the position of $\bm{O}_B$ expressed in $\{A\}$ using ${}^A\bm{P}$
- the orientation of $\{B\}$ expressed in $\{A\}$ using a rotation matrix ${}^{A}\bm{R}_{B}$

Then, the function =initializeStewartPose= ([[sec:initializeStewartPose][link]]) compute the corresponding initial and rest position of each of the strut.

* Definition of the Inertia and geometry of the Fixed base, Mobile platform and Struts
<<sec:definition_inertia>>
** Introduction                                                      :ignore:
Now that the geometry of the Stewart platform has been defined, we have to choose the inertia of:
- The Fixed base
- The Mobile platform
- The two parts of the struts

The inertia of these elements will modify the dynamics of the systems.
It is thus important to set them properly.

** Inertia and Geometry of the Fixed and Mobile platforms
In order to set the inertia of the fixed and mobile platforms, we can use the following function that assume that both platforms are cylindrical:
- =initializeCylindricalPlatforms= ([[sec:initializeCylindricalPlatforms][link]]): by choosing the height, radius and mass of the platforms, it computes the inertia matrix that will be used for simulation

** Inertia and Geometry of the struts
Similarly for the struts, we suppose here that they have a cylindrical shape.
They are initialize with the following function:
- =initializeCylindricalStruts= ([[sec:initializeCylindricalStruts][link]]): the two parts of each strut are supposed to by cylindrical. We can set the mass and geometry of both strut parts.

* Definition of the stiffness and damping of the joints
<<sec:definition_dynamics>>

** Introduction                                                      :ignore:
The global stiffness and damping of the Stewart platform depends on its geometry but also on the stiffness and damping of:
- the actuator because of the finite stiffness of the actuator / linear guide
- the spherical joints

** Stiffness and Damping of the Actuator
Each Actuator is modeled by 3 elements in parallel (Figure [[fig:stewart_platform_actuator]]):
- A spring with a stiffness $k_{i}$
- A dashpot with a damping $c_{i}$
- An ideal force actuator generating a force $\tau_i$

#+name: fig:stewart_platform_actuator
#+caption: Model of the Stewart platform actuator
[[file:figs/stewart_platform_actuator.png]]

The initialization of the stiffness and damping properties of the actuators is done with the =initializeStrutDynamics= ([[sec:initializeStrutDynamics][link]]).

** Stiffness and Damping of the Spherical Joints
Even though we often suppose that the spherical joint are perfect in the sense that we neglect its stiffness and damping, we can set some rotation stiffness and damping of each of the spherical/universal joints.

This is done with the =initializeJointDynamics= function ([[sec:initializeJointDynamics][link]]).

* Summary of the Initialization Procedure and Matlab Example
<<sec:summary_initialization>>
** Introduction                                                      :ignore:
The procedure to define the Stewart platform is the following:
1. Define the initial position of frames $\{A\}$, $\{B\}$, $\{F\}$ and $\{M\}$.
   We do that using the =initializeFramesPositions= function.
   We have to specify the total height of the Stewart platform $H$ and the position ${}^{M}\bm{O}_{B}$ of $\{B\}$ with respect to $\{M\}$.
2. Compute the positions of joints ${}^{F}\bm{a}_{i}$ and ${}^{M}\bm{b}_{i}$.
   We can do that using various methods depending on the wanted architecture:
   - =generateCubicConfiguration= permits to generate a cubic configuration
3. Compute the position and orientation of the joints with respect to the fixed base and the moving platform.
   This is done with the =computeJointsPose= function.
   If wanted, compute the rest position of each strut to have the wanted pose of the mobile platform with the function =initializeStewartPose=.
4. Define the mass and inertia of each element of the Stewart platform with the =initializeCylindricalPlatforms= and =initializeCylindricalStruts=
5. Define the dynamical properties of the Stewart platform by setting the stiffness and damping of the actuators and joints.

By following this procedure, we obtain a Matlab structure =stewart= that contains all the information for the Simscape model and for further analysis.

** Matlab Init                                              :noexport:ignore:
#+begin_src matlab :tangle no :exports none :results silent :noweb yes :var current_dir=(file-name-directory buffer-file-name)
  <<matlab-dir>>
#+end_src

#+begin_src matlab :exports none :results silent :noweb yes
  <<matlab-init>>
#+end_src

#+begin_src matlab
  simulinkproject('./');
#+end_src

** Example of the initialization of a Stewart Platform
Let's first define the Stewart Platform Geometry.
#+begin_src matlab
  stewart = initializeFramesPositions('H', 90e-3, 'MO_B', 45e-3);
  stewart = generateGeneralConfiguration(stewart);
  stewart = computeJointsPose(stewart);
  stewart = initializeStewartPose(stewart, 'AP', [0;0;0.01], 'ARB', eye(3));
#+end_src

Then, define the inertia and geometry of the fixed base, mobile platform and struts.
#+begin_src matlab
  stewart = initializeCylindricalPlatforms(stewart);
  stewart = initializeCylindricalStruts(stewart);
#+end_src

Finally, initialize the strut stiffness and damping properties.
#+begin_src matlab
  stewart = initializeStrutDynamics(stewart, 'Ki', 1e6*ones(6,1), 'Ci', 1e2*ones(6,1));
  stewart = initializeJointDynamics(stewart);
#+end_src

The obtained =stewart= Matlab structure contains all the information for analysis of the Stewart platform and for simulations using Simscape.

The function =displayArchitecture= can be used to display the current Stewart configuration:
#+begin_src matlab
  displayArchitecture(stewart);
#+end_src

#+header: :tangle no :exports results :results none :noweb yes
#+begin_src matlab :var filepath="figs/stewart_architecture_example.pdf" :var figsize="wide-tall" :post pdf2svg(file=*this*, ext="png")
<<plt-matlab>>
#+end_src

#+name: fig:stewart_architecture_example
#+caption: Display of the current Stewart platform architecture ([[./figs/stewart_architecture_example.png][png]], [[./figs/stewart_architecture_example.pdf][pdf]])
[[file:figs/stewart_architecture_example.png]]

There are many options to show or hides elements such as labels and frames.
The documentation of the function is available [[sec:displayArchitecture][here]].

Let's now move a little bit the top platform and re-display the configuration:
#+begin_src matlab
  tx = 0.1; % [rad]
  ty = 0.2; % [rad]
  tz = 0.05; % [rad]

  Rx = [1 0        0;
        0 cos(tx) -sin(tx);
        0 sin(tx)  cos(tx)];

  Ry = [ cos(ty) 0 sin(ty);
        0        1 0;
        -sin(ty) 0 cos(ty)];

  Rz = [cos(tz) -sin(tz) 0;
        sin(tz)  cos(tz) 0;
        0        0       1];

  ARB = Rz*Ry*Rx;
  AP = [0.08; 0; 0]; % [m]

  displayArchitecture(stewart, 'AP', AP, 'ARB', ARB);
  view([0 -1 0]);
#+end_src

#+header: :tangle no :exports results :results none :noweb yes
#+begin_src matlab :var filepath="figs/stewart_architecture_example_pose.pdf" :var figsize="wide-tall" :post pdf2svg(file=*this*, ext="png")
<<plt-matlab>>
#+end_src

#+name: fig:stewart_architecture_example_pose
#+caption: Display of the Stewart platform architecture at some defined pose ([[./figs/stewart_architecture_example_pose.png][png]], [[./figs/stewart_architecture_example_pose.pdf][pdf]])
[[file:figs/stewart_architecture_example_pose.png]]

* Functions
<<sec:functions>>
** =initializeFramesPositions=: Initialize the positions of frames {A}, {B}, {F} and {M}
:PROPERTIES:
:header-args:matlab+: :tangle src/initializeFramesPositions.m
:header-args:matlab+: :comments none :mkdirp yes :eval no
:END:
<<sec:initializeFramesPositions>>

This Matlab function is accessible [[file:src/initializeFramesPositions.m][here]].

*** Function description
:PROPERTIES:
:UNNUMBERED: t
:END:
#+begin_src matlab
  function [stewart] = initializeFramesPositions(args)
  % initializeFramesPositions - Initialize the positions of frames {A}, {B}, {F} and {M}
  %
  % Syntax: [stewart] = initializeFramesPositions(args)
  %
  % Inputs:
  %    - args - Can have the following fields:
  %        - H    [1x1] - Total Height of the Stewart Platform (height from {F} to {M}) [m]
  %        - MO_B [1x1] - Height of the frame {B} with respect to {M} [m]
  %
  % Outputs:
  %    - stewart - A structure with the following fields:
  %        - H    [1x1] - Total Height of the Stewart Platform [m]
  %        - FO_M [3x1] - Position of {M} with respect to {F} [m]
  %        - MO_B [3x1] - Position of {B} with respect to {M} [m]
  %        - FO_A [3x1] - Position of {A} with respect to {F} [m]
#+end_src

*** Documentation
:PROPERTIES:
:UNNUMBERED: t
:END:

#+name: fig:stewart-frames-position
#+caption: Definition of the position of the frames
[[file:figs/stewart-frames-position.png]]

*** Optional Parameters
:PROPERTIES:
:UNNUMBERED: t
:END:
#+begin_src matlab
  arguments
      args.H    (1,1) double {mustBeNumeric, mustBePositive} = 90e-3
      args.MO_B (1,1) double {mustBeNumeric} = 50e-3
  end
#+end_src

*** Initialize the Stewart structure
:PROPERTIES:
:UNNUMBERED: t
:END:
#+begin_src matlab
  stewart = struct();
#+end_src

*** Compute the position of each frame
:PROPERTIES:
:UNNUMBERED: t
:END:
#+begin_src matlab
  stewart.H = args.H; % Total Height of the Stewart Platform [m]

  stewart.FO_M = [0; 0; stewart.H]; % Position of {M} with respect to {F} [m]

  stewart.MO_B = [0; 0; args.MO_B]; % Position of {B} with respect to {M} [m]

  stewart.FO_A = stewart.MO_B + stewart.FO_M; % Position of {A} with respect to {F} [m]
#+end_src

** =generateGeneralConfiguration=: Generate a Very General Configuration
:PROPERTIES:
:header-args:matlab+: :tangle src/generateGeneralConfiguration.m
:header-args:matlab+: :comments none :mkdirp yes :eval no
:END:
<<sec:generateGeneralConfiguration>>

This Matlab function is accessible [[file:src/generateGeneralConfiguration.m][here]].

*** Function description
:PROPERTIES:
:UNNUMBERED: t
:END:
#+begin_src matlab
  function [stewart] = generateGeneralConfiguration(stewart, args)
  % generateGeneralConfiguration - Generate a Very General Configuration
  %
  % Syntax: [stewart] = generateGeneralConfiguration(stewart, args)
  %
  % Inputs:
  %    - args - Can have the following fields:
  %        - FH  [1x1] - Height of the position of the fixed joints with respect to the frame {F} [m]
  %        - FR  [1x1] - Radius of the position of the fixed joints in the X-Y [m]
  %        - FTh [6x1] - Angles of the fixed joints in the X-Y plane with respect to the X axis [rad]
  %        - MH  [1x1] - Height of the position of the mobile joints with respect to the frame {M} [m]
  %        - FR  [1x1] - Radius of the position of the mobile joints in the X-Y [m]
  %        - MTh [6x1] - Angles of the mobile joints in the X-Y plane with respect to the X axis [rad]
  %
  % Outputs:
  %    - stewart - updated Stewart structure with the added fields:
  %        - Fa  [3x6] - Its i'th column is the position vector of joint ai with respect to {F}
  %        - Mb  [3x6] - Its i'th column is the position vector of joint bi with respect to {M}
#+end_src

*** Documentation
:PROPERTIES:
:UNNUMBERED: t
:END:
Joints are positions on a circle centered with the Z axis of {F} and {M} and at a chosen distance from {F} and {M}.
The radius of the circles can be chosen as well as the angles where the joints are located (see Figure [[fig:joint_position_general]]).

#+begin_src latex :file stewart_bottom_plate.pdf :exports results
  \begin{tikzpicture}
    % Internal and external limit
    \draw[fill=white!80!black] (0, 0) circle [radius=3];
    % Circle where the joints are located
    \draw[dashed] (0, 0) circle [radius=2.5];

    % Bullets for the positions of the joints
    \node[] (J1) at ( 80:2.5){$\bullet$};
    \node[] (J2) at (100:2.5){$\bullet$};
    \node[] (J3) at (200:2.5){$\bullet$};
    \node[] (J4) at (220:2.5){$\bullet$};
    \node[] (J5) at (320:2.5){$\bullet$};
    \node[] (J6) at (340:2.5){$\bullet$};

    % Name of the points
    \node[above right] at (J1) {$a_{1}$};
    \node[above left]  at (J2) {$a_{2}$};
    \node[above left]  at (J3) {$a_{3}$};
    \node[right     ]  at (J4) {$a_{4}$};
    \node[left      ]  at (J5) {$a_{5}$};
    \node[above right] at (J6) {$a_{6}$};

    % First 2 angles
    \draw[dashed, ->] (0:1)   arc [start angle=0, end angle=80, radius=1]    node[below right]{$\theta_{1}$};
    \draw[dashed, ->] (0:1.5) arc [start angle=0, end angle=100, radius=1.5] node[left       ]{$\theta_{2}$};

    % Division of 360 degrees by 3
    \draw[dashed] (0, 0) -- ( 80:3.2);
    \draw[dashed] (0, 0) -- (100:3.2);
    \draw[dashed] (0, 0) -- (200:3.2);
    \draw[dashed] (0, 0) -- (220:3.2);
    \draw[dashed] (0, 0) -- (320:3.2);
    \draw[dashed] (0, 0) -- (340:3.2);

    % Radius for the position of the joints
    \draw[<->] (0, 0) --node[near end, above]{$R$} (180:2.5);

    \draw[->] (0, 0) -- ++(3.4, 0) node[above]{$x$};
    \draw[->] (0, 0) -- ++(0, 3.4) node[left]{$y$};
  \end{tikzpicture}
#+end_src

#+name: fig:joint_position_general
#+caption: Position of the joints
#+RESULTS:
[[file:figs/stewart_bottom_plate.png]]

*** Optional Parameters
:PROPERTIES:
:UNNUMBERED: t
:END:
#+begin_src matlab
  arguments
      stewart
      args.FH  (1,1) double {mustBeNumeric, mustBePositive} = 15e-3
      args.FR  (1,1) double {mustBeNumeric, mustBePositive} = 115e-3;
      args.FTh (6,1) double {mustBeNumeric} = [-10, 10, 120-10, 120+10, 240-10, 240+10]*(pi/180);
      args.MH  (1,1) double {mustBeNumeric, mustBePositive} = 15e-3
      args.MR  (1,1) double {mustBeNumeric, mustBePositive} = 90e-3;
      args.MTh (6,1) double {mustBeNumeric} = [-60+10, 60-10, 60+10, 180-10, 180+10, -60-10]*(pi/180);
  end
#+end_src

*** Compute the pose
:PROPERTIES:
:UNNUMBERED: t
:END:
#+begin_src matlab
  stewart.Fa = zeros(3,6);
  stewart.Mb = zeros(3,6);
#+end_src

#+begin_src matlab
  for i = 1:6
    stewart.Fa(:,i) = [args.FR*cos(args.FTh(i)); args.FR*sin(args.FTh(i)); args.FH];
    stewart.Mb(:,i) = [args.MR*cos(args.MTh(i)); args.MR*sin(args.MTh(i)); -args.MH];
  end
#+end_src

** =computeJointsPose=: Compute the Pose of the Joints
:PROPERTIES:
:header-args:matlab+: :tangle src/computeJointsPose.m
:header-args:matlab+: :comments none :mkdirp yes :eval no
:END:
<<sec:computeJointsPose>>

This Matlab function is accessible [[file:src/computeJointsPose.m][here]].

*** Function description
:PROPERTIES:
:UNNUMBERED: t
:END:
#+begin_src matlab
  function [stewart] = computeJointsPose(stewart)
  % computeJointsPose -
  %
  % Syntax: [stewart] = computeJointsPose(stewart)
  %
  % Inputs:
  %    - stewart - A structure with the following fields
  %        - Fa   [3x6] - Its i'th column is the position vector of joint ai with respect to {F}
  %        - Mb   [3x6] - Its i'th column is the position vector of joint bi with respect to {M}
  %        - FO_A [3x1] - Position of {A} with respect to {F}
  %        - MO_B [3x1] - Position of {B} with respect to {M}
  %        - FO_M [3x1] - Position of {M} with respect to {F}
  %
  % Outputs:
  %    - stewart - A structure with the following added fields
  %        - Aa  [3x6]   - The i'th column is the position of ai with respect to {A}
  %        - Ab  [3x6]   - The i'th column is the position of bi with respect to {A}
  %        - Ba  [3x6]   - The i'th column is the position of ai with respect to {B}
  %        - Bb  [3x6]   - The i'th column is the position of bi with respect to {B}
  %        - l   [6x1]   - The i'th element is the initial length of strut i
  %        - As  [3x6]   - The i'th column is the unit vector of strut i expressed in {A}
  %        - Bs  [3x6]   - The i'th column is the unit vector of strut i expressed in {B}
  %        - FRa [3x3x6] - The i'th 3x3 array is the rotation matrix to orientate the bottom of the i'th strut from {F}
  %        - MRb [3x3x6] - The i'th 3x3 array is the rotation matrix to orientate the top of the i'th strut from {M}
#+end_src

*** Documentation
:PROPERTIES:
:UNNUMBERED: t
:END:

#+name: fig:stewart-struts
#+caption: Position and orientation of the struts
[[file:figs/stewart-struts.png]]

*** Compute the position of the Joints
:PROPERTIES:
:UNNUMBERED: t
:END:
#+begin_src matlab
  stewart.Aa = stewart.Fa - repmat(stewart.FO_A, [1, 6]);
  stewart.Bb = stewart.Mb - repmat(stewart.MO_B, [1, 6]);

  stewart.Ab = stewart.Bb - repmat(-stewart.MO_B-stewart.FO_M+stewart.FO_A, [1, 6]);
  stewart.Ba = stewart.Aa - repmat( stewart.MO_B+stewart.FO_M-stewart.FO_A, [1, 6]);
#+end_src

*** Compute the strut length and orientation
:PROPERTIES:
:UNNUMBERED: t
:END:
#+begin_src matlab
  stewart.As = (stewart.Ab - stewart.Aa)./vecnorm(stewart.Ab - stewart.Aa); % As_i is the i'th vector of As

  stewart.l = vecnorm(stewart.Ab - stewart.Aa)';
#+end_src

#+begin_src matlab
  stewart.Bs = (stewart.Bb - stewart.Ba)./vecnorm(stewart.Bb - stewart.Ba);
#+end_src

*** Compute the orientation of the Joints
:PROPERTIES:
:UNNUMBERED: t
:END:
#+begin_src matlab
  stewart.FRa = zeros(3,3,6);
  stewart.MRb = zeros(3,3,6);

  for i = 1:6
    stewart.FRa(:,:,i) = [cross([0;1;0], stewart.As(:,i)) , cross(stewart.As(:,i), cross([0;1;0], stewart.As(:,i))) , stewart.As(:,i)];
    stewart.FRa(:,:,i) = stewart.FRa(:,:,i)./vecnorm(stewart.FRa(:,:,i));

    stewart.MRb(:,:,i) = [cross([0;1;0], stewart.Bs(:,i)) , cross(stewart.Bs(:,i), cross([0;1;0], stewart.Bs(:,i))) , stewart.Bs(:,i)];
    stewart.MRb(:,:,i) = stewart.MRb(:,:,i)./vecnorm(stewart.MRb(:,:,i));
  end
#+end_src

** =initializeStewartPose=: Determine the initial stroke in each leg to have the wanted pose
:PROPERTIES:
:header-args:matlab+: :tangle src/initializeStewartPose.m
:header-args:matlab+: :comments none :mkdirp yes :eval no
:END:
<<sec:initializeStewartPose>>

This Matlab function is accessible [[file:src/initializeStewartPose.m][here]].

*** Function description
:PROPERTIES:
:UNNUMBERED: t
:END:
#+begin_src matlab
  function [stewart] = initializeStewartPose(stewart, args)
  % initializeStewartPose - Determine the initial stroke in each leg to have the wanted pose
  %                         It uses the inverse kinematic
  %
  % Syntax: [stewart] = initializeStewartPose(stewart, args)
  %
  % Inputs:
  %    - stewart - A structure with the following fields
  %        - Aa   [3x6] - The positions ai expressed in {A}
  %        - Bb   [3x6] - The positions bi expressed in {B}
  %    - args - Can have the following fields:
  %        - AP   [3x1] - The wanted position of {B} with respect to {A}
  %        - ARB  [3x3] - The rotation matrix that gives the wanted orientation of {B} with respect to {A}
  %
  % Outputs:
  %    - stewart - updated Stewart structure with the added fields:
  %      - dLi[6x1] - The 6 needed displacement of the struts from the initial position in [m] to have the wanted pose of {B} w.r.t. {A}
#+end_src

*** Optional Parameters
:PROPERTIES:
:UNNUMBERED: t
:END:
#+begin_src matlab
  arguments
      stewart
      args.AP  (3,1) double {mustBeNumeric} = zeros(3,1)
      args.ARB (3,3) double {mustBeNumeric} = eye(3)
  end
#+end_src

*** Use the Inverse Kinematic function
:PROPERTIES:
:UNNUMBERED: t
:END:
#+begin_src matlab
  [Li, dLi] = inverseKinematics(stewart, 'AP', args.AP, 'ARB', args.ARB);

  stewart.dLi = dLi;
#+end_src

** =initializeCylindricalPlatforms=: Initialize the geometry of the Fixed and Mobile Platforms
:PROPERTIES:
:header-args:matlab+: :tangle src/initializeCylindricalPlatforms.m
:header-args:matlab+: :comments none :mkdirp yes :eval no
:END:
<<sec:initializeCylindricalPlatforms>>

This Matlab function is accessible [[file:src/initializeCylindricalPlatforms.m][here]].

*** Function description
:PROPERTIES:
:UNNUMBERED: t
:END:
#+begin_src matlab
  function [stewart] = initializeCylindricalPlatforms(stewart, args)
  % initializeCylindricalPlatforms - Initialize the geometry of the Fixed and Mobile Platforms
  %
  % Syntax: [stewart] = initializeCylindricalPlatforms(args)
  %
  % Inputs:
  %    - args - Structure with the following fields:
  %        - Fpm [1x1] - Fixed Platform Mass [kg]
  %        - Fph [1x1] - Fixed Platform Height [m]
  %        - Fpr [1x1] - Fixed Platform Radius [m]
  %        - Mpm [1x1] - Mobile Platform Mass [kg]
  %        - Mph [1x1] - Mobile Platform Height [m]
  %        - Mpr [1x1] - Mobile Platform Radius [m]
  %
  % Outputs:
  %    - stewart - updated Stewart structure with the added fields:
  %      - platforms [struct] - structure with the following fields:
  %        - Fpm [1x1] - Fixed Platform Mass [kg]
  %        - Msi [3x3] - Mobile Platform Inertia matrix [kg*m^2]
  %        - Fph [1x1] - Fixed Platform Height [m]
  %        - Fpr [1x1] - Fixed Platform Radius [m]
  %        - Mpm [1x1] - Mobile Platform Mass [kg]
  %        - Fsi [3x3] - Fixed Platform Inertia matrix [kg*m^2]
  %        - Mph [1x1] - Mobile Platform Height [m]
  %        - Mpr [1x1] - Mobile Platform Radius [m]
#+end_src

*** Optional Parameters
:PROPERTIES:
:UNNUMBERED: t
:END:
#+begin_src matlab
  arguments
      stewart
      args.Fpm (1,1) double {mustBeNumeric, mustBePositive} = 1
      args.Fph (1,1) double {mustBeNumeric, mustBePositive} = 10e-3
      args.Fpr (1,1) double {mustBeNumeric, mustBePositive} = 125e-3
      args.Mpm (1,1) double {mustBeNumeric, mustBePositive} = 1
      args.Mph (1,1) double {mustBeNumeric, mustBePositive} = 10e-3
      args.Mpr (1,1) double {mustBeNumeric, mustBePositive} = 100e-3
  end
#+end_src

*** Create the =platforms= struct
:PROPERTIES:
:UNNUMBERED: t
:END:
#+begin_src matlab
  platforms = struct();

  platforms.Fpm = args.Fpm;
  platforms.Fph = args.Fph;
  platforms.Fpr = args.Fpr;
  platforms.Fpi = diag([1/12 * platforms.Fpm * (3*platforms.Fpr^2 + platforms.Fph^2), ...
                        1/12 * platforms.Fpm * (3*platforms.Fpr^2 + platforms.Fph^2), ...
                        1/2  * platforms.Fpm * platforms.Fpr^2]);

  platforms.Mpm = args.Mpm;
  platforms.Mph = args.Mph;
  platforms.Mpr = args.Mpr;
  platforms.Mpi = diag([1/12 * platforms.Mpm * (3*platforms.Mpr^2 + platforms.Mph^2), ...
                        1/12 * platforms.Mpm * (3*platforms.Mpr^2 + platforms.Mph^2), ...
                        1/2  * platforms.Mpm * platforms.Mpr^2]);
#+end_src

*** Save the =platforms= struct
:PROPERTIES:
:UNNUMBERED: t
:END:
#+begin_src matlab
  stewart.platforms = platforms;
#+end_src

** =initializeCylindricalStruts=: Define the inertia of cylindrical struts
:PROPERTIES:
:header-args:matlab+: :tangle src/initializeCylindricalStruts.m
:header-args:matlab+: :comments none :mkdirp yes :eval no
:END:
<<sec:initializeCylindricalStruts>>

This Matlab function is accessible [[file:src/initializeCylindricalStruts.m][here]].

*** Function description
:PROPERTIES:
:UNNUMBERED: t
:END:
#+begin_src matlab
  function [stewart] = initializeCylindricalStruts(stewart, args)
  % initializeCylindricalStruts - Define the mass and moment of inertia of cylindrical struts
  %
  % Syntax: [stewart] = initializeCylindricalStruts(args)
  %
  % Inputs:
  %    - args - Structure with the following fields:
  %        - Fsm [1x1] - Mass of the Fixed part of the struts [kg]
  %        - Fsh [1x1] - Height of cylinder for the Fixed part of the struts [m]
  %        - Fsr [1x1] - Radius of cylinder for the Fixed part of the struts [m]
  %        - Msm [1x1] - Mass of the Mobile part of the struts [kg]
  %        - Msh [1x1] - Height of cylinder for the Mobile part of the struts [m]
  %        - Msr [1x1] - Radius of cylinder for the Mobile part of the struts [m]
  %
  % Outputs:
  %    - stewart - updated Stewart structure with the added fields:
  %      - struts [struct] - structure with the following fields:
  %        - Fsm [6x1]   - Mass of the Fixed part of the struts [kg]
  %        - Fsi [3x3x6] - Moment of Inertia for the Fixed part of the struts [kg*m^2]
  %        - Msm [6x1]   - Mass of the Mobile part of the struts [kg]
  %        - Msi [3x3x6] - Moment of Inertia for the Mobile part of the struts [kg*m^2]
  %        - Fsh [6x1]   - Height of cylinder for the Fixed part of the struts [m]
  %        - Fsr [6x1]   - Radius of cylinder for the Fixed part of the struts [m]
  %        - Msh [6x1]   - Height of cylinder for the Mobile part of the struts [m]
  %        - Msr [6x1]   - Radius of cylinder for the Mobile part of the struts [m]
#+end_src

*** Optional Parameters
:PROPERTIES:
:UNNUMBERED: t
:END:
#+begin_src matlab
  arguments
      stewart
      args.Fsm (1,1) double {mustBeNumeric, mustBePositive} = 0.1
      args.Fsh (1,1) double {mustBeNumeric, mustBePositive} = 50e-3
      args.Fsr (1,1) double {mustBeNumeric, mustBePositive} = 5e-3
      args.Msm (1,1) double {mustBeNumeric, mustBePositive} = 0.1
      args.Msh (1,1) double {mustBeNumeric, mustBePositive} = 50e-3
      args.Msr (1,1) double {mustBeNumeric, mustBePositive} = 5e-3
  end
#+end_src

*** Create the =struts= structure
:PROPERTIES:
:UNNUMBERED: t
:END:
#+begin_src matlab
  struts = struct();

  struts.Fsm = ones(6,1).*args.Fsm;
  struts.Msm = ones(6,1).*args.Msm;

  struts.Fsh = ones(6,1).*args.Fsh;
  struts.Fsr = ones(6,1).*args.Fsr;
  struts.Msh = ones(6,1).*args.Msh;
  struts.Msr = ones(6,1).*args.Msr;

  struts.Fsi = zeros(3, 3, 6);
  struts.Msi = zeros(3, 3, 6);
  for i = 1:6
    struts.Fsi(:,:,i) = diag([1/12 * struts.Fsm(i) * (3*struts.Fsr(i)^2 + struts.Fsh(i)^2), ...
                              1/12 * struts.Fsm(i) * (3*struts.Fsr(i)^2 + struts.Fsh(i)^2), ...
                              1/2  * struts.Fsm(i) * struts.Fsr(i)^2]);
    struts.Msi(:,:,i) = diag([1/12 * struts.Msm(i) * (3*struts.Msr(i)^2 + struts.Msh(i)^2), ...
                              1/12 * struts.Msm(i) * (3*struts.Msr(i)^2 + struts.Msh(i)^2), ...
                              1/2  * struts.Msm(i) * struts.Msr(i)^2]);
  end
#+end_src

#+begin_src matlab
  stewart.struts = struts;
#+end_src

** =initializeStrutDynamics=: Add Stiffness and Damping properties of each strut
:PROPERTIES:
:header-args:matlab+: :tangle src/initializeStrutDynamics.m
:header-args:matlab+: :comments none :mkdirp yes :eval no
:END:
<<sec:initializeStrutDynamics>>

This Matlab function is accessible [[file:src/initializeStrutDynamics.m][here]].

*** Function description
:PROPERTIES:
:UNNUMBERED: t
:END:
#+begin_src matlab
  function [stewart] = initializeStrutDynamics(stewart, args)
  % initializeStrutDynamics - Add Stiffness and Damping properties of each strut
  %
  % Syntax: [stewart] = initializeStrutDynamics(args)
  %
  % Inputs:
  %    - args - Structure with the following fields:
  %        - Ki [6x1] - Stiffness of each strut [N/m]
  %        - Ci [6x1] - Damping of each strut [N/(m/s)]
  %
  % Outputs:
  %    - stewart - updated Stewart structure with the added fields:
  %        - Ki [6x1] - Stiffness of each strut [N/m]
  %        - Ci [6x1] - Damping of each strut [N/(m/s)]
#+end_src

*** Optional Parameters
:PROPERTIES:
:UNNUMBERED: t
:END:
#+begin_src matlab
  arguments
      stewart
      args.Ki (6,1) double {mustBeNumeric, mustBeNonnegative} = 1e6*ones(6,1)
      args.Ci (6,1) double {mustBeNumeric, mustBeNonnegative} = 1e1*ones(6,1)
  end
#+end_src

*** Add Stiffness and Damping properties of each strut
:PROPERTIES:
:UNNUMBERED: t
:END:
#+begin_src matlab
  stewart.Ki = args.Ki;
  stewart.Ci = args.Ci;
#+end_src

** =initializeJointDynamics=: Add Stiffness and Damping properties for spherical joints
:PROPERTIES:
:header-args:matlab+: :tangle src/initializeJointDynamics.m
:header-args:matlab+: :comments none :mkdirp yes :eval no
:END:
<<sec:initializeJointDynamics>>

This Matlab function is accessible [[file:src/initializeJointDynamics.m][here]].

*** Function description
:PROPERTIES:
:UNNUMBERED: t
:END:
#+begin_src matlab
  function [stewart] = initializeJointDynamics(stewart, args)
  % initializeJointDynamics - Add Stiffness and Damping properties for the spherical joints
  %
  % Syntax: [stewart] = initializeJointDynamics(args)
  %
  % Inputs:
  %    - args - Structure with the following fields:
  %        - Ksbi [6x1] - Bending (Rx, Ry) Stiffness for each top Spherical joints [N/rad]
  %        - Csbi [6x1] - Bending (Rx, Ry) Damping of each top Spherical joint [N/(rad/s)]
  %        - Ksti [6x1] - Torsion (Rz) Stiffness for each top Spherical joints [N/rad]
  %        - Csti [6x1] - Torsion (Rz) Damping of each top Spherical joint [N/(rad/s)]
  %        - Kubi [6x1] - Bending (Rx, Ry) Stiffness for each bottom Universal joints [N/rad]
  %        - Cubi [6x1] - Bending (Rx, Ry) Damping of each bottom Universal joint [N/(rad/s)]
  %        - disable [true/false] - Sets all the stiffness/damping to zero
  %
  % Outputs:
  %    - stewart - updated Stewart structure with the added fields:
  %        - Ksbi [6x1] - Bending (Rx, Ry) Stiffness for each top Spherical joints [N/rad]
  %        - Csbi [6x1] - Bending (Rx, Ry) Damping of each top Spherical joint [N/(rad/s)]
  %        - Ksti [6x1] - Torsion (Rz) Stiffness for each top Spherical joints [N/rad]
  %        - Csti [6x1] - Torsion (Rz) Damping of each top Spherical joint [N/(rad/s)]
  %        - Kubi [6x1] - Bending (Rx, Ry) Stiffness for each bottom Universal joints [N/rad]
  %        - Cubi [6x1] - Bending (Rx, Ry) Damping of each bottom Universal joint [N/(rad/s)]
#+end_src

*** Optional Parameters
:PROPERTIES:
:UNNUMBERED: t
:END:
#+begin_src matlab
  arguments
      stewart
      args.Ksbi (6,1) double {mustBeNumeric, mustBeNonnegative} = 1e+1*ones(6,1)
      args.Csbi (6,1) double {mustBeNumeric, mustBeNonnegative} = 1e-4*ones(6,1)
      args.Ksti (6,1) double {mustBeNumeric, mustBeNonnegative} = 1e+0*ones(6,1)
      args.Csti (6,1) double {mustBeNumeric, mustBeNonnegative} = 1e-3*ones(6,1)
      args.Kubi (6,1) double {mustBeNumeric, mustBeNonnegative} = 1e+1*ones(6,1)
      args.Cubi (6,1) double {mustBeNumeric, mustBeNonnegative} = 1e-4*ones(6,1)
      args.disable logical {mustBeNumericOrLogical} = false
  end
#+end_src

*** Add Stiffness and Damping properties of each strut
:PROPERTIES:
:UNNUMBERED: t
:END:
#+begin_src matlab
  if args.disable
    stewart.Ksbi = zeros(6,1);
    stewart.Csbi = zeros(6,1);
    stewart.Ksti = zeros(6,1);
    stewart.Csti = zeros(6,1);
    stewart.Kubi = zeros(6,1);
    stewart.Cubi = zeros(6,1);
  else
    stewart.Ksbi = args.Ksbi;
    stewart.Csbi = args.Csbi;
    stewart.Ksti = args.Ksti;
    stewart.Csti = args.Csti;
    stewart.Kubi = args.Kubi;
    stewart.Cubi = args.Cubi;
  end
#+end_src

** =displayArchitecture=: 3D plot of the Stewart platform architecture
:PROPERTIES:
:header-args:matlab+: :tangle src/displayArchitecture.m
:header-args:matlab+: :comments none :mkdirp yes :eval no
:END:
<<sec:displayArchitecture>>

This Matlab function is accessible [[file:src/displayArchitecture.m][here]].

*** Function description
:PROPERTIES:
:UNNUMBERED: t
:END:
#+begin_src matlab
  function [] = displayArchitecture(stewart, args)
  % displayArchitecture - 3D plot of the Stewart platform architecture
  %
  % Syntax: [] = displayArchitecture(args)
  %
  % Inputs:
  %    - stewart
  %    - args - Structure with the following fields:
  %        - AP   [3x1] - The wanted position of {B} with respect to {A}
  %        - ARB  [3x3] - The rotation matrix that gives the wanted orientation of {B} with respect to {A}
  %        - ARB  [3x3] - The rotation matrix that gives the wanted orientation of {B} with respect to {A}
  %        - F_color [color] - Color used for the Fixed elements
  %        - M_color [color] - Color used for the Mobile elements
  %        - L_color [color] - Color used for the Legs elements
  %        - frames    [true/false] - Display the Frames
  %        - legs      [true/false] - Display the Legs
  %        - joints    [true/false] - Display the Joints
  %        - labels    [true/false] - Display the Labels
  %        - platforms [true/false] - Display the Platforms
  %
  % Outputs:
#+end_src

*** Optional Parameters
:PROPERTIES:
:UNNUMBERED: t
:END:
#+begin_src matlab
  arguments
      stewart
      args.AP  (3,1) double {mustBeNumeric} = zeros(3,1)
      args.ARB (3,3) double {mustBeNumeric} = eye(3)
      args.F_color = [0 0.4470 0.7410]
      args.M_color = [0.8500 0.3250 0.0980]
      args.L_color = [0 0 0]
      args.frames logical {mustBeNumericOrLogical} = true
      args.legs logical {mustBeNumericOrLogical} = true
      args.joints logical {mustBeNumericOrLogical} = true
      args.labels logical {mustBeNumericOrLogical} = true
      args.platforms logical {mustBeNumericOrLogical} = true
  end
#+end_src

*** Figure Creation, Frames and Homogeneous transformations
:PROPERTIES:
:UNNUMBERED: t
:END:

The reference frame of the 3d plot corresponds to the frame $\{F\}$.
#+begin_src matlab
  figure;
  hold on;
#+end_src

We first compute homogeneous matrices that will be useful to position elements on the figure where the reference frame is $\{F\}$.
#+begin_src matlab
  FTa = [eye(3), stewart.FO_A; ...
         zeros(1,3), 1];
  ATb = [args.ARB, args.AP; ...
         zeros(1,3), 1];
  BTm = [eye(3), -stewart.MO_B; ...
         zeros(1,3), 1];

  FTm = FTa*ATb*BTm;
#+end_src

Let's define a parameter that define the length of the unit vectors used to display the frames.
#+begin_src matlab
  d_unit_vector = stewart.H/4;
#+end_src

Let's define a parameter used to position the labels with respect to the center of the element.
#+begin_src matlab
  d_label = stewart.H/20;
#+end_src

*** Fixed Base elements
:PROPERTIES:
:UNNUMBERED: t
:END:
Let's first plot the frame $\{F\}$.
#+begin_src matlab
  Ff = [0, 0, 0];
  if args.frames
    quiver3(Ff(1)*ones(1,3), Ff(2)*ones(1,3), Ff(3)*ones(1,3), ...
            [d_unit_vector 0 0], [0 d_unit_vector 0], [0 0 d_unit_vector], '-', 'Color', args.F_color)

    if args.labels
      text(Ff(1) + d_label, ...
          Ff(2) + d_label, ...
          Ff(3) + d_label, '$\{F\}$', 'Color', args.F_color);
    end
  end
#+end_src

Now plot the frame $\{A\}$ fixed to the Base.
#+begin_src matlab
  Fa = stewart.FO_A;

  if args.frames
    quiver3(Fa(1)*ones(1,3), Fa(2)*ones(1,3), Fa(3)*ones(1,3), ...
            [d_unit_vector 0 0], [0 d_unit_vector 0], [0 0 d_unit_vector], '-', 'Color', args.F_color)

    if args.labels
      text(Fa(1) + d_label, ...
           Fa(2) + d_label, ...
           Fa(3) + d_label, '$\{A\}$', 'Color', args.F_color);
    end
  end
#+end_src

Let's then plot the circle corresponding to the shape of the Fixed base.
#+begin_src matlab
  if args.platforms && isfield(stewart, 'platforms') && isfield(stewart.platforms, 'Fpr')
    theta = [0:0.01:2*pi+0.01]; % Angles [rad]
    v = null([0; 0; 1]'); % Two vectors that are perpendicular to the circle normal
    center = [0; 0; 0]; % Center of the circle
    radius = stewart.platforms.Fpr; % Radius of the circle [m]

    points = center*ones(1, length(theta)) + radius*(v(:,1)*cos(theta) + v(:,2)*sin(theta));

    plot3(points(1,:), ...
          points(2,:), ...
          points(3,:), '-', 'Color', args.F_color);
  end
#+end_src

Let's now plot the position and labels of the Fixed Joints
#+begin_src matlab
  if args.joints
    scatter3(stewart.Fa(1,:), ...
             stewart.Fa(2,:), ...
             stewart.Fa(3,:), 'MarkerEdgeColor', args.F_color);
    if args.labels
      for i = 1:size(stewart.Fa,2)
        text(stewart.Fa(1,i) + d_label, ...
             stewart.Fa(2,i), ...
             stewart.Fa(3,i), sprintf('$a_{%i}$', i), 'Color', args.F_color);
      end
    end
  end
#+end_src

*** Mobile Platform elements
:PROPERTIES:
:UNNUMBERED: t
:END:

Plot the frame $\{M\}$.
#+begin_src matlab
  Fm = FTm*[0; 0; 0; 1]; % Get the position of frame {M} w.r.t. {F}

  if args.frames
    FM_uv = FTm*[d_unit_vector*eye(3); zeros(1,3)]; % Rotated Unit vectors
    quiver3(Fm(1)*ones(1,3), Fm(2)*ones(1,3), Fm(3)*ones(1,3), ...
            FM_uv(1,1:3), FM_uv(2,1:3), FM_uv(3,1:3), '-', 'Color', args.M_color)

    if args.labels
      text(Fm(1) + d_label, ...
           Fm(2) + d_label, ...
           Fm(3) + d_label, '$\{M\}$', 'Color', args.M_color);
    end
  end
#+end_src

Plot the frame $\{B\}$.
#+begin_src matlab
  FB = stewart.FO_A + args.AP;

  if args.frames
    FB_uv = FTm*[d_unit_vector*eye(3); zeros(1,3)]; % Rotated Unit vectors
    quiver3(FB(1)*ones(1,3), FB(2)*ones(1,3), FB(3)*ones(1,3), ...
            FB_uv(1,1:3), FB_uv(2,1:3), FB_uv(3,1:3), '-', 'Color', args.M_color)

    if args.labels
      text(FB(1) - d_label, ...
           FB(2) + d_label, ...
           FB(3) + d_label, '$\{B\}$', 'Color', args.M_color);
    end
  end
#+end_src

Let's then plot the circle corresponding to the shape of the Mobile platform.
#+begin_src matlab
  if args.platforms && isfield(stewart, 'platforms') && isfield(stewart.platforms, 'Mpr')
    theta = [0:0.01:2*pi+0.01]; % Angles [rad]
    v = null((FTm(1:3,1:3)*[0;0;1])'); % Two vectors that are perpendicular to the circle normal
    center = Fm(1:3); % Center of the circle
    radius = stewart.platforms.Mpr; % Radius of the circle [m]

    points = center*ones(1, length(theta)) + radius*(v(:,1)*cos(theta) + v(:,2)*sin(theta));

    plot3(points(1,:), ...
          points(2,:), ...
          points(3,:), '-', 'Color', args.M_color);
  end
#+end_src

Plot the position and labels of the rotation joints fixed to the mobile platform.
#+begin_src matlab
  if args.joints
    Fb = FTm*[stewart.Mb;ones(1,6)];

    scatter3(Fb(1,:), ...
             Fb(2,:), ...
             Fb(3,:), 'MarkerEdgeColor', args.M_color);

    if args.labels
      for i = 1:size(Fb,2)
        text(Fb(1,i) + d_label, ...
             Fb(2,i), ...
             Fb(3,i), sprintf('$b_{%i}$', i), 'Color', args.M_color);
      end
    end
  end
#+end_src

*** Legs
:PROPERTIES:
:UNNUMBERED: t
:END:
Plot the legs connecting the joints of the fixed base to the joints of the mobile platform.
#+begin_src matlab
  if args.legs
    for i = 1:6
      plot3([stewart.Fa(1,i), Fb(1,i)], ...
            [stewart.Fa(2,i), Fb(2,i)], ...
            [stewart.Fa(3,i), Fb(3,i)], '-', 'Color', args.L_color);

      if args.labels
        text((stewart.Fa(1,i)+Fb(1,i))/2 + d_label, ...
             (stewart.Fa(2,i)+Fb(2,i))/2, ...
             (stewart.Fa(3,i)+Fb(3,i))/2, sprintf('$%i$', i), 'Color', args.L_color);
      end
    end
  end
#+end_src

*** Figure parameters
#+begin_src matlab
  view([1 -0.6 0.4]);
  axis equal;
  axis off;
#+end_src

* Bibliography                                                        :ignore:
bibliographystyle:unsrt
bibliography:ref.bib