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<h1 class="title">Stewart Platform - Simscape Model</h1>
<div id="table-of-contents">
<h2>Table of Contents</h2>
<div id="text-table-of-contents">
<ul>
<li><a href="#orgac25f89">1. <code>initializeFramesPositions</code>: Initialize the positions of frames {A}, {B}, {F} and {M}</a>
<ul>
<li><a href="#org5cdd36d">1.1. Function description</a></li>
<li><a href="#orge837700">1.2. Documentation</a></li>
<li><a href="#org312e9a7">1.3. Optional Parameters</a></li>
<li><a href="#org3622825">1.4. Initialize the Stewart structure</a></li>
<li><a href="#org7d50d54">1.5. Compute the position of each frame</a></li>
</ul>
</li>
<li><a href="#org4310d42">2. Initialize the position of the Joints</a>
<ul>
<li><a href="#org65fc289">2.1. <code>generateCubicConfiguration</code>: Generate a Cubic Configuration</a>
<ul>
<li><a href="#org5a5b987">2.1.1. Function description</a></li>
<li><a href="#org40ea23a">2.1.2. Documentation</a></li>
<li><a href="#org37651aa">2.1.3. Optional Parameters</a></li>
<li><a href="#orge94a885">2.1.4. Position of the Cube</a></li>
<li><a href="#org789a28b">2.1.5. Compute the pose</a></li>
</ul>
</li>
<li><a href="#orgccb31c6">2.2. <code>generateGeneralConfiguration</code>: Generate a Very General Configuration</a>
<ul>
<li><a href="#org0ba3fa4">2.2.1. Function description</a></li>
<li><a href="#org839cae7">2.2.2. Documentation</a></li>
<li><a href="#org2e06fba">2.2.3. Optional Parameters</a></li>
<li><a href="#orgfac23f3">2.2.4. Compute the pose</a></li>
</ul>
</li>
</ul>
</li>
<li><a href="#org9944c04">3. <code>computeJointsPose</code>: Compute the Pose of the Joints</a>
<ul>
<li><a href="#org465ebb2">3.1. Function description</a></li>
<li><a href="#orgc11609b">3.2. Documentation</a></li>
<li><a href="#orge87b302">3.3. Compute the position of the Joints</a></li>
<li><a href="#org3a7e3c5">3.4. Compute the strut length and orientation</a></li>
<li><a href="#org9e1258f">3.5. Compute the orientation of the Joints</a></li>
</ul>
</li>
<li><a href="#orgae8d0dc">4. <code>initializeStrutDynamics</code>: Add Stiffness and Damping properties of each strut</a>
<ul>
<li><a href="#org9af8ca0">4.1. Function description</a></li>
<li><a href="#org335e959">4.2. Optional Parameters</a></li>
<li><a href="#org3c2e550">4.3. Add Stiffness and Damping properties of each strut</a></li>
</ul>
</li>
<li><a href="#org9e8cbfa">5. <code>computeJacobian</code>: Compute the Jacobian Matrix</a>
<ul>
<li><a href="#org64e795c">5.1. Function description</a></li>
<li><a href="#org9bcd9b9">5.2. Compute Jacobian Matrix</a></li>
<li><a href="#orgf08eda6">5.3. Compute Stiffness Matrix</a></li>
<li><a href="#orgd164132">5.4. Compute Compliance Matrix</a></li>
</ul>
</li>
<li><a href="#org53d13cc">6. Initialize the Geometry of the Mechanical Elements</a>
<ul>
<li><a href="#org4674203">6.1. <code>initializeCylindricalPlatforms</code>: Initialize the geometry of the Fixed and Mobile Platforms</a>
<ul>
<li><a href="#org1af6832">6.1.1. Function description</a></li>
<li><a href="#org12a2c2b">6.1.2. Optional Parameters</a></li>
<li><a href="#org2965fe8">6.1.3. Create the <code>platforms</code> struct</a></li>
<li><a href="#org7e1a4d4">6.1.4. Save the <code>platforms</code> struct</a></li>
</ul>
</li>
<li><a href="#org6b4f1ca">6.2. <code>initializeCylindricalStruts</code>: Define the mass and moment of inertia of cylindrical struts</a>
<ul>
<li><a href="#org407cf8c">6.2.1. Function description</a></li>
<li><a href="#org420f14e">6.2.2. Optional Parameters</a></li>
<li><a href="#org3f9f0ef">6.2.3. Create the <code>struts</code> structure</a></li>
</ul>
</li>
</ul>
</li>
<li><a href="#orgb4dc92b">7. Utility Functions</a>
<ul>
<li><a href="#org03168fc">7.1. <code>inverseKinematics</code>: Compute Inverse Kinematics</a>
<ul>
<li><a href="#orgb7853bd">7.1.1. Function description</a></li>
<li><a href="#orge9021eb">7.1.2. Optional Parameters</a></li>
<li><a href="#orgbdc5fb1">7.1.3. Theory</a></li>
<li><a href="#org8b70a76">7.1.4. Compute</a></li>
</ul>
</li>
<li><a href="#orgf4ebfa3">7.2. <code>forwardKinematicsApprox</code>: Compute the Forward Kinematics</a>
<ul>
<li><a href="#org37e6edf">7.2.1. Function description</a></li>
<li><a href="#org6441308">7.2.2. Optional Parameters</a></li>
<li><a href="#orgf17cab9">7.2.3. Computation</a></li>
</ul>
</li>
</ul>
</li>
</ul>
</div>
</div>
<p>
Stewart platforms are generated in multiple steps.
</p>
<p>
We define 4 important <b>frames</b>:
</p>
<ul class="org-ul">
<li>\(\{F\}\): Frame fixed to the <b>Fixed</b> base and located at the center of its bottom surface.
This is used to fix the Stewart platform to some support.</li>
<li>\(\{M\}\): Frame fixed to the <b>Moving</b> platform and located at the center of its top surface.
This is used to place things on top of the Stewart platform.</li>
<li>\(\{A\}\): Frame fixed to the fixed base.
It defined the center of rotation of the moving platform.</li>
<li>\(\{B\}\): Frame fixed to the moving platform.
The motion of the moving platforms and forces applied to it are defined with respect to this frame \(\{B\}\).</li>
</ul>
<p>
Then, we define the <b>location of the spherical joints</b>:
</p>
<ul class="org-ul">
<li>\(\bm{a}_{i}\) are the position of the spherical joints fixed to the fixed base</li>
<li>\(\bm{b}_{i}\) are the position of the spherical joints fixed to the moving platform</li>
</ul>
<p>
We define the <b>rest position</b> of the Stewart platform:
</p>
<ul class="org-ul">
<li>For simplicity, we suppose that the fixed base and the moving platform are parallel and aligned with the vertical axis at their rest position.</li>
<li>Thus, to define the rest position of the Stewart platform, we just have to defined its total height \(H\).
\(H\) corresponds to the distance from the bottom of the fixed base to the top of the moving platform.</li>
</ul>
<p>
From \(\bm{a}_{i}\) and \(\bm{b}_{i}\), we can determine the <b>length and orientation of each strut</b>:
</p>
<ul class="org-ul">
<li>\(l_{i}\) is the length of the strut</li>
<li>\({}^{A}\hat{\bm{s}}_{i}\) is the unit vector align with the strut</li>
</ul>
<p>
The position of the Spherical joints can be computed using various methods:
</p>
<ul class="org-ul">
<li>Cubic configuration</li>
<li>Circular configuration</li>
<li>Arbitrary position</li>
<li>These methods should be easily scriptable and corresponds to specific functions that returns \({}^{F}\bm{a}_{i}\) and \({}^{M}\bm{b}_{i}\).
The input of these functions are the parameters corresponding to the wanted geometry.</li>
</ul>
<p>
For Simscape, we need:
</p>
<ul class="org-ul">
<li>The position and orientation of each spherical joint fixed to the fixed base: \({}^{F}\bm{a}_{i}\) and \({}^{F}\bm{R}_{a_{i}}\)</li>
<li>The position and orientation of each spherical joint fixed to the moving platform: \({}^{M}\bm{b}_{i}\) and \({}^{M}\bm{R}_{b_{i}}\)</li>
<li>The rest length of each strut: \(l_{i}\)</li>
<li>The stiffness and damping of each actuator: \(k_{i}\) and \(c_{i}\)</li>
<li>The position of the frame \(\{A\}\) with respect to the frame \(\{F\}\): \({}^{F}\bm{O}_{A}\)</li>
<li>The position of the frame \(\{B\}\) with respect to the frame \(\{M\}\): \({}^{M}\bm{O}_{B}\)</li>
</ul>
<div id="outline-container-orgac25f89" class="outline-2">
<h2 id="orgac25f89"><span class="section-number-2">1</span> <code>initializeFramesPositions</code>: Initialize the positions of frames {A}, {B}, {F} and {M}</h2>
<div class="outline-text-2" id="text-1">
<p>
<a id="orga56a5c6"></a>
</p>
<p>
This Matlab function is accessible <a href="src/initializeFramesPositions.m">here</a>.
</p>
</div>
<div id="outline-container-org5cdd36d" class="outline-3">
<h3 id="org5cdd36d"><span class="section-number-3">1.1</span> Function description</h3>
<div class="outline-text-3" id="text-1-1">
<div class="org-src-container">
<pre class="src src-matlab"><span class="org-keyword">function</span> <span class="org-variable-name">[stewart]</span> = <span class="org-function-name">initializeFramesPositions</span>(<span class="org-variable-name">args</span>)
<span class="org-comment">% initializeFramesPositions - Initialize the positions of frames {A}, {B}, {F} and {M}</span>
<span class="org-comment">%</span>
<span class="org-comment">% Syntax: [stewart] = initializeFramesPositions(args)</span>
<span class="org-comment">%</span>
<span class="org-comment">% Inputs:</span>
<span class="org-comment">% - args - Can have the following fields:</span>
<span class="org-comment">% - H [1x1] - Total Height of the Stewart Platform (height from {F} to {M}) [m]</span>
<span class="org-comment">% - MO_B [1x1] - Height of the frame {B} with respect to {M} [m]</span>
<span class="org-comment">%</span>
<span class="org-comment">% Outputs:</span>
<span class="org-comment">% - stewart - A structure with the following fields:</span>
<span class="org-comment">% - H [1x1] - Total Height of the Stewart Platform [m]</span>
<span class="org-comment">% - FO_M [3x1] - Position of {M} with respect to {F} [m]</span>
<span class="org-comment">% - MO_B [3x1] - Position of {B} with respect to {M} [m]</span>
<span class="org-comment">% - FO_A [3x1] - Position of {A} with respect to {F} [m]</span>
</pre>
</div>
</div>
</div>
<div id="outline-container-orge837700" class="outline-3">
<h3 id="orge837700"><span class="section-number-3">1.2</span> Documentation</h3>
<div class="outline-text-3" id="text-1-2">
<div id="orgebd0f49" class="figure">
<p><img src="figs/stewart-frames-position.png" alt="stewart-frames-position.png" />
</p>
<p><span class="figure-number">Figure 1: </span>Definition of the position of the frames</p>
</div>
</div>
</div>
<div id="outline-container-org312e9a7" class="outline-3">
<h3 id="org312e9a7"><span class="section-number-3">1.3</span> Optional Parameters</h3>
<div class="outline-text-3" id="text-1-3">
<div class="org-src-container">
<pre class="src src-matlab">arguments
args.H (1,1) double {mustBeNumeric, mustBePositive} = 90e<span class="org-type">-</span>3
args.MO_B (1,1) double {mustBeNumeric} = 50e<span class="org-type">-</span>3
<span class="org-keyword">end</span>
</pre>
</div>
</div>
</div>
<div id="outline-container-org3622825" class="outline-3">
<h3 id="org3622825"><span class="section-number-3">1.4</span> Initialize the Stewart structure</h3>
<div class="outline-text-3" id="text-1-4">
<div class="org-src-container">
<pre class="src src-matlab">stewart = struct();
</pre>
</div>
</div>
</div>
<div id="outline-container-org7d50d54" class="outline-3">
<h3 id="org7d50d54"><span class="section-number-3">1.5</span> Compute the position of each frame</h3>
<div class="outline-text-3" id="text-1-5">
<div class="org-src-container">
<pre class="src src-matlab">stewart.H = args.H; <span class="org-comment">% Total Height of the Stewart Platform [m]</span>
stewart.FO_M = [0; 0; stewart.H]; <span class="org-comment">% Position of {M} with respect to {F} [m]</span>
stewart.MO_B = [0; 0; args.MO_B]; <span class="org-comment">% Position of {B} with respect to {M} [m]</span>
stewart.FO_A = stewart.MO_B <span class="org-type">+</span> stewart.FO_M; <span class="org-comment">% Position of {A} with respect to {F} [m]</span>
</pre>
</div>
</div>
</div>
</div>
<div id="outline-container-org4310d42" class="outline-2">
<h2 id="org4310d42"><span class="section-number-2">2</span> Initialize the position of the Joints</h2>
<div class="outline-text-2" id="text-2">
</div>
<div id="outline-container-org65fc289" class="outline-3">
<h3 id="org65fc289"><span class="section-number-3">2.1</span> <code>generateCubicConfiguration</code>: Generate a Cubic Configuration</h3>
<div class="outline-text-3" id="text-2-1">
<p>
<a id="org677ea95"></a>
</p>
<p>
This Matlab function is accessible <a href="src/generateCubicConfiguration.m">here</a>.
</p>
</div>
<div id="outline-container-org5a5b987" class="outline-4">
<h4 id="org5a5b987"><span class="section-number-4">2.1.1</span> Function description</h4>
<div class="outline-text-4" id="text-2-1-1">
<div class="org-src-container">
<pre class="src src-matlab"><span class="org-keyword">function</span> <span class="org-variable-name">[stewart]</span> = <span class="org-function-name">generateCubicConfiguration</span>(<span class="org-variable-name">stewart</span>, <span class="org-variable-name">args</span>)
<span class="org-comment">% generateCubicConfiguration - Generate a Cubic Configuration</span>
<span class="org-comment">%</span>
<span class="org-comment">% Syntax: [stewart] = generateCubicConfiguration(stewart, args)</span>
<span class="org-comment">%</span>
<span class="org-comment">% Inputs:</span>
<span class="org-comment">% - stewart - A structure with the following fields</span>
<span class="org-comment">% - H [1x1] - Total height of the platform [m]</span>
<span class="org-comment">% - args - Can have the following fields:</span>
<span class="org-comment">% - Hc [1x1] - Height of the "useful" part of the cube [m]</span>
<span class="org-comment">% - FOc [1x1] - Height of the center of the cube with respect to {F} [m]</span>
<span class="org-comment">% - FHa [1x1] - Height of the plane joining the points ai with respect to the frame {F} [m]</span>
<span class="org-comment">% - MHb [1x1] - Height of the plane joining the points bi with respect to the frame {M} [m]</span>
<span class="org-comment">%</span>
<span class="org-comment">% Outputs:</span>
<span class="org-comment">% - stewart - updated Stewart structure with the added fields:</span>
<span class="org-comment">% - Fa [3x6] - Its i'th column is the position vector of joint ai with respect to {F}</span>
<span class="org-comment">% - Mb [3x6] - Its i'th column is the position vector of joint bi with respect to {M}</span>
</pre>
</div>
</div>
</div>
<div id="outline-container-org40ea23a" class="outline-4">
<h4 id="org40ea23a"><span class="section-number-4">2.1.2</span> Documentation</h4>
<div class="outline-text-4" id="text-2-1-2">
<div id="org70070f0" class="figure">
<p><img src="figs/cubic-configuration-definition.png" alt="cubic-configuration-definition.png" />
</p>
<p><span class="figure-number">Figure 2: </span>Cubic Configuration</p>
</div>
</div>
</div>
<div id="outline-container-org37651aa" class="outline-4">
<h4 id="org37651aa"><span class="section-number-4">2.1.3</span> Optional Parameters</h4>
<div class="outline-text-4" id="text-2-1-3">
<div class="org-src-container">
<pre class="src src-matlab">arguments
stewart
args.Hc (1,1) double {mustBeNumeric, mustBePositive} = 60e<span class="org-type">-</span>3
args.FOc (1,1) double {mustBeNumeric} = 50e<span class="org-type">-</span>3
args.FHa (1,1) double {mustBeNumeric, mustBePositive} = 15e<span class="org-type">-</span>3
args.MHb (1,1) double {mustBeNumeric, mustBePositive} = 15e<span class="org-type">-</span>3
<span class="org-keyword">end</span>
</pre>
</div>
</div>
</div>
<div id="outline-container-orge94a885" class="outline-4">
<h4 id="orge94a885"><span class="section-number-4">2.1.4</span> Position of the Cube</h4>
<div class="outline-text-4" id="text-2-1-4">
<p>
We define the useful points of the cube with respect to the Cube&rsquo;s center.
\({}^{C}C\) are the 6 vertices of the cubes expressed in a frame {C} which is
located at the center of the cube and aligned with {F} and {M}.
</p>
<div class="org-src-container">
<pre class="src src-matlab">sx = [ 2; <span class="org-type">-</span>1; <span class="org-type">-</span>1];
sy = [ 0; 1; <span class="org-type">-</span>1];
sz = [ 1; 1; 1];
R = [sx, sy, sz]<span class="org-type">./</span>vecnorm([sx, sy, sz]);
L = args.Hc<span class="org-type">*</span>sqrt(3);
Cc = R<span class="org-type">'*</span>[[0;0;L],[L;0;L],[L;0;0],[L;L;0],[0;L;0],[0;L;L]] <span class="org-type">-</span> [0;0;1.5<span class="org-type">*</span>args.Hc];
CCf = [Cc(<span class="org-type">:</span>,1), Cc(<span class="org-type">:</span>,3), Cc(<span class="org-type">:</span>,3), Cc(<span class="org-type">:</span>,5), Cc(<span class="org-type">:</span>,5), Cc(<span class="org-type">:</span>,1)]; <span class="org-comment">% CCf(:,i) corresponds to the bottom cube's vertice corresponding to the i'th leg</span>
CCm = [Cc(<span class="org-type">:</span>,2), Cc(<span class="org-type">:</span>,2), Cc(<span class="org-type">:</span>,4), Cc(<span class="org-type">:</span>,4), Cc(<span class="org-type">:</span>,6), Cc(<span class="org-type">:</span>,6)]; <span class="org-comment">% CCm(:,i) corresponds to the top cube's vertice corresponding to the i'th leg</span>
</pre>
</div>
</div>
</div>
<div id="outline-container-org789a28b" class="outline-4">
<h4 id="org789a28b"><span class="section-number-4">2.1.5</span> Compute the pose</h4>
<div class="outline-text-4" id="text-2-1-5">
<p>
We can compute the vector of each leg \({}^{C}\hat{\bm{s}}_{i}\) (unit vector from \({}^{C}C_{f}\) to \({}^{C}C_{m}\)).
</p>
<div class="org-src-container">
<pre class="src src-matlab">CSi = (CCm <span class="org-type">-</span> CCf)<span class="org-type">./</span>vecnorm(CCm <span class="org-type">-</span> CCf);
</pre>
</div>
<p>
We now which to compute the position of the joints \(a_{i}\) and \(b_{i}\).
</p>
<div class="org-src-container">
<pre class="src src-matlab">stewart.Fa = CCf <span class="org-type">+</span> [0; 0; args.FOc] <span class="org-type">+</span> ((args.FHa<span class="org-type">-</span>(args.FOc<span class="org-type">-</span>args.Hc<span class="org-type">/</span>2))<span class="org-type">./</span>CSi(3,<span class="org-type">:</span>))<span class="org-type">.*</span>CSi;
stewart.Mb = CCf <span class="org-type">+</span> [0; 0; args.FOc<span class="org-type">-</span>stewart.H] <span class="org-type">+</span> ((stewart.H<span class="org-type">-</span>args.MHb<span class="org-type">-</span>(args.FOc<span class="org-type">-</span>args.Hc<span class="org-type">/</span>2))<span class="org-type">./</span>CSi(3,<span class="org-type">:</span>))<span class="org-type">.*</span>CSi;
</pre>
</div>
</div>
</div>
</div>
<div id="outline-container-orgccb31c6" class="outline-3">
<h3 id="orgccb31c6"><span class="section-number-3">2.2</span> <code>generateGeneralConfiguration</code>: Generate a Very General Configuration</h3>
<div class="outline-text-3" id="text-2-2">
<p>
<a id="org32105b0"></a>
</p>
<p>
This Matlab function is accessible <a href="src/generateGeneralConfiguration.m">here</a>.
</p>
</div>
<div id="outline-container-org0ba3fa4" class="outline-4">
<h4 id="org0ba3fa4"><span class="section-number-4">2.2.1</span> Function description</h4>
<div class="outline-text-4" id="text-2-2-1">
<div class="org-src-container">
<pre class="src src-matlab"><span class="org-keyword">function</span> <span class="org-variable-name">[stewart]</span> = <span class="org-function-name">generateGeneralConfiguration</span>(<span class="org-variable-name">stewart</span>, <span class="org-variable-name">args</span>)
<span class="org-comment">% generateGeneralConfiguration - Generate a Very General Configuration</span>
<span class="org-comment">%</span>
<span class="org-comment">% Syntax: [stewart] = generateGeneralConfiguration(stewart, args)</span>
<span class="org-comment">%</span>
<span class="org-comment">% Inputs:</span>
<span class="org-comment">% - args - Can have the following fields:</span>
<span class="org-comment">% - FH [1x1] - Height of the position of the fixed joints with respect to the frame {F} [m]</span>
<span class="org-comment">% - FR [1x1] - Radius of the position of the fixed joints in the X-Y [m]</span>
<span class="org-comment">% - FTh [6x1] - Angles of the fixed joints in the X-Y plane with respect to the X axis [rad]</span>
<span class="org-comment">% - MH [1x1] - Height of the position of the mobile joints with respect to the frame {M} [m]</span>
<span class="org-comment">% - FR [1x1] - Radius of the position of the mobile joints in the X-Y [m]</span>
<span class="org-comment">% - MTh [6x1] - Angles of the mobile joints in the X-Y plane with respect to the X axis [rad]</span>
<span class="org-comment">%</span>
<span class="org-comment">% Outputs:</span>
<span class="org-comment">% - stewart - updated Stewart structure with the added fields:</span>
<span class="org-comment">% - Fa [3x6] - Its i'th column is the position vector of joint ai with respect to {F}</span>
<span class="org-comment">% - Mb [3x6] - Its i'th column is the position vector of joint bi with respect to {M}</span>
</pre>
</div>
</div>
</div>
<div id="outline-container-org839cae7" class="outline-4">
<h4 id="org839cae7"><span class="section-number-4">2.2.2</span> Documentation</h4>
<div class="outline-text-4" id="text-2-2-2">
<p>
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.
</p>
</div>
</div>
<div id="outline-container-org2e06fba" class="outline-4">
<h4 id="org2e06fba"><span class="section-number-4">2.2.3</span> Optional Parameters</h4>
<div class="outline-text-4" id="text-2-2-3">
<div class="org-src-container">
<pre class="src src-matlab">arguments
stewart
args.FH (1,1) double {mustBeNumeric, mustBePositive} = 15e<span class="org-type">-</span>3
args.FR (1,1) double {mustBeNumeric, mustBePositive} = 90e<span class="org-type">-</span>3;
args.FTh (6,1) double {mustBeNumeric} = [<span class="org-type">-</span>10, 10, 120<span class="org-type">-</span>10, 120<span class="org-type">+</span>10, 240<span class="org-type">-</span>10, 240<span class="org-type">+</span>10]<span class="org-type">*</span>(<span class="org-constant">pi</span><span class="org-type">/</span>180);
args.MH (1,1) double {mustBeNumeric, mustBePositive} = 15e<span class="org-type">-</span>3
args.MR (1,1) double {mustBeNumeric, mustBePositive} = 70e<span class="org-type">-</span>3;
args.MTh (6,1) double {mustBeNumeric} = [<span class="org-type">-</span>60<span class="org-type">+</span>10, 60<span class="org-type">-</span>10, 60<span class="org-type">+</span>10, 180<span class="org-type">-</span>10, 180<span class="org-type">+</span>10, <span class="org-type">-</span>60<span class="org-type">-</span>10]<span class="org-type">*</span>(<span class="org-constant">pi</span><span class="org-type">/</span>180);
<span class="org-keyword">end</span>
</pre>
</div>
</div>
</div>
<div id="outline-container-orgfac23f3" class="outline-4">
<h4 id="orgfac23f3"><span class="section-number-4">2.2.4</span> Compute the pose</h4>
<div class="outline-text-4" id="text-2-2-4">
<div class="org-src-container">
<pre class="src src-matlab">stewart.Fa = zeros(3,6);
stewart.Mb = zeros(3,6);
</pre>
</div>
<div class="org-src-container">
<pre class="src src-matlab"><span class="org-keyword">for</span> <span class="org-variable-name"><span class="org-constant">i</span></span> = <span class="org-constant">1:6</span>
stewart.Fa(<span class="org-type">:</span>,<span class="org-constant">i</span>) = [args.FR<span class="org-type">*</span>cos(args.FTh(<span class="org-constant">i</span>)); args.FR<span class="org-type">*</span>sin(args.FTh(<span class="org-constant">i</span>)); args.FH];
stewart.Mb(<span class="org-type">:</span>,<span class="org-constant">i</span>) = [args.MR<span class="org-type">*</span>cos(args.MTh(<span class="org-constant">i</span>)); args.MR<span class="org-type">*</span>sin(args.MTh(<span class="org-constant">i</span>)); <span class="org-type">-</span>args.MH];
<span class="org-keyword">end</span>
</pre>
</div>
</div>
</div>
</div>
</div>
<div id="outline-container-org9944c04" class="outline-2">
<h2 id="org9944c04"><span class="section-number-2">3</span> <code>computeJointsPose</code>: Compute the Pose of the Joints</h2>
<div class="outline-text-2" id="text-3">
<p>
<a id="orgd0bee51"></a>
</p>
<p>
This Matlab function is accessible <a href="src/computeJointsPose.m">here</a>.
</p>
</div>
<div id="outline-container-org465ebb2" class="outline-3">
<h3 id="org465ebb2"><span class="section-number-3">3.1</span> Function description</h3>
<div class="outline-text-3" id="text-3-1">
<div class="org-src-container">
<pre class="src src-matlab"><span class="org-keyword">function</span> <span class="org-variable-name">[stewart]</span> = <span class="org-function-name">computeJointsPose</span>(<span class="org-variable-name">stewart</span>)
<span class="org-comment">% computeJointsPose -</span>
<span class="org-comment">%</span>
<span class="org-comment">% Syntax: [stewart] = computeJointsPose(stewart)</span>
<span class="org-comment">%</span>
<span class="org-comment">% Inputs:</span>
<span class="org-comment">% - stewart - A structure with the following fields</span>
<span class="org-comment">% - Fa [3x6] - Its i'th column is the position vector of joint ai with respect to {F}</span>
<span class="org-comment">% - Mb [3x6] - Its i'th column is the position vector of joint bi with respect to {M}</span>
<span class="org-comment">% - FO_A [3x1] - Position of {A} with respect to {F}</span>
<span class="org-comment">% - MO_B [3x1] - Position of {B} with respect to {M}</span>
<span class="org-comment">% - FO_M [3x1] - Position of {M} with respect to {F}</span>
<span class="org-comment">%</span>
<span class="org-comment">% Outputs:</span>
<span class="org-comment">% - stewart - A structure with the following added fields</span>
<span class="org-comment">% - Aa [3x6] - The i'th column is the position of ai with respect to {A}</span>
<span class="org-comment">% - Ab [3x6] - The i'th column is the position of bi with respect to {A}</span>
<span class="org-comment">% - Ba [3x6] - The i'th column is the position of ai with respect to {B}</span>
<span class="org-comment">% - Bb [3x6] - The i'th column is the position of bi with respect to {B}</span>
<span class="org-comment">% - l [6x1] - The i'th element is the initial length of strut i</span>
<span class="org-comment">% - As [3x6] - The i'th column is the unit vector of strut i expressed in {A}</span>
<span class="org-comment">% - Bs [3x6] - The i'th column is the unit vector of strut i expressed in {B}</span>
<span class="org-comment">% - FRa [3x3x6] - The i'th 3x3 array is the rotation matrix to orientate the bottom of the i'th strut from {F}</span>
<span class="org-comment">% - MRb [3x3x6] - The i'th 3x3 array is the rotation matrix to orientate the top of the i'th strut from {M}</span>
</pre>
</div>
</div>
</div>
<div id="outline-container-orgc11609b" class="outline-3">
<h3 id="orgc11609b"><span class="section-number-3">3.2</span> Documentation</h3>
<div class="outline-text-3" id="text-3-2">
<div id="org20f7106" class="figure">
<p><img src="figs/stewart-struts.png" alt="stewart-struts.png" />
</p>
<p><span class="figure-number">Figure 3: </span>Position and orientation of the struts</p>
</div>
</div>
</div>
<div id="outline-container-orge87b302" class="outline-3">
<h3 id="orge87b302"><span class="section-number-3">3.3</span> Compute the position of the Joints</h3>
<div class="outline-text-3" id="text-3-3">
<div class="org-src-container">
<pre class="src src-matlab">stewart.Aa = stewart.Fa <span class="org-type">-</span> repmat(stewart.FO_A, [1, 6]);
stewart.Bb = stewart.Mb <span class="org-type">-</span> repmat(stewart.MO_B, [1, 6]);
stewart.Ab = stewart.Bb <span class="org-type">-</span> repmat(<span class="org-type">-</span>stewart.MO_B<span class="org-type">-</span>stewart.FO_M<span class="org-type">+</span>stewart.FO_A, [1, 6]);
stewart.Ba = stewart.Aa <span class="org-type">-</span> repmat( stewart.MO_B<span class="org-type">+</span>stewart.FO_M<span class="org-type">-</span>stewart.FO_A, [1, 6]);
</pre>
</div>
</div>
</div>
<div id="outline-container-org3a7e3c5" class="outline-3">
<h3 id="org3a7e3c5"><span class="section-number-3">3.4</span> Compute the strut length and orientation</h3>
<div class="outline-text-3" id="text-3-4">
<div class="org-src-container">
<pre class="src src-matlab">stewart.As = (stewart.Ab <span class="org-type">-</span> stewart.Aa)<span class="org-type">./</span>vecnorm(stewart.Ab <span class="org-type">-</span> stewart.Aa); <span class="org-comment">% As_i is the i'th vector of As</span>
stewart.l = vecnorm(stewart.Ab <span class="org-type">-</span> stewart.Aa)<span class="org-type">'</span>;
</pre>
</div>
<div class="org-src-container">
<pre class="src src-matlab">stewart.Bs = (stewart.Bb <span class="org-type">-</span> stewart.Ba)<span class="org-type">./</span>vecnorm(stewart.Bb <span class="org-type">-</span> stewart.Ba);
</pre>
</div>
</div>
</div>
<div id="outline-container-org9e1258f" class="outline-3">
<h3 id="org9e1258f"><span class="section-number-3">3.5</span> Compute the orientation of the Joints</h3>
<div class="outline-text-3" id="text-3-5">
<div class="org-src-container">
<pre class="src src-matlab">stewart.FRa = zeros(3,3,6);
stewart.MRb = zeros(3,3,6);
<span class="org-keyword">for</span> <span class="org-variable-name"><span class="org-constant">i</span></span> = <span class="org-constant">1:6</span>
stewart.FRa(<span class="org-type">:</span>,<span class="org-type">:</span>,<span class="org-constant">i</span>) = [cross([0;1;0], stewart.As(<span class="org-type">:</span>,<span class="org-constant">i</span>)) , cross(stewart.As(<span class="org-type">:</span>,<span class="org-constant">i</span>), cross([0;1;0], stewart.As(<span class="org-type">:</span>,<span class="org-constant">i</span>))) , stewart.As(<span class="org-type">:</span>,<span class="org-constant">i</span>)];
stewart.FRa(<span class="org-type">:</span>,<span class="org-type">:</span>,<span class="org-constant">i</span>) = stewart.FRa(<span class="org-type">:</span>,<span class="org-type">:</span>,<span class="org-constant">i</span>)<span class="org-type">./</span>vecnorm(stewart.FRa(<span class="org-type">:</span>,<span class="org-type">:</span>,<span class="org-constant">i</span>));
stewart.MRb(<span class="org-type">:</span>,<span class="org-type">:</span>,<span class="org-constant">i</span>) = [cross([0;1;0], stewart.Bs(<span class="org-type">:</span>,<span class="org-constant">i</span>)) , cross(stewart.Bs(<span class="org-type">:</span>,<span class="org-constant">i</span>), cross([0;1;0], stewart.Bs(<span class="org-type">:</span>,<span class="org-constant">i</span>))) , stewart.Bs(<span class="org-type">:</span>,<span class="org-constant">i</span>)];
stewart.MRb(<span class="org-type">:</span>,<span class="org-type">:</span>,<span class="org-constant">i</span>) = stewart.MRb(<span class="org-type">:</span>,<span class="org-type">:</span>,<span class="org-constant">i</span>)<span class="org-type">./</span>vecnorm(stewart.MRb(<span class="org-type">:</span>,<span class="org-type">:</span>,<span class="org-constant">i</span>));
<span class="org-keyword">end</span>
</pre>
</div>
</div>
</div>
</div>
<div id="outline-container-orgae8d0dc" class="outline-2">
<h2 id="orgae8d0dc"><span class="section-number-2">4</span> <code>initializeStrutDynamics</code>: Add Stiffness and Damping properties of each strut</h2>
<div class="outline-text-2" id="text-4">
<p>
<a id="orgd55e892"></a>
</p>
<p>
This Matlab function is accessible <a href="src/initializeStrutDynamics.m">here</a>.
</p>
</div>
<div id="outline-container-org9af8ca0" class="outline-3">
<h3 id="org9af8ca0"><span class="section-number-3">4.1</span> Function description</h3>
<div class="outline-text-3" id="text-4-1">
<div class="org-src-container">
<pre class="src src-matlab"><span class="org-keyword">function</span> <span class="org-variable-name">[stewart]</span> = <span class="org-function-name">initializeStrutDynamics</span>(<span class="org-variable-name">stewart</span>, <span class="org-variable-name">args</span>)
<span class="org-comment">% initializeStrutDynamics - Add Stiffness and Damping properties of each strut</span>
<span class="org-comment">%</span>
<span class="org-comment">% Syntax: [stewart] = initializeStrutDynamics(args)</span>
<span class="org-comment">%</span>
<span class="org-comment">% Inputs:</span>
<span class="org-comment">% - args - Structure with the following fields:</span>
<span class="org-comment">% - Ki [6x1] - Stiffness of each strut [N/m]</span>
<span class="org-comment">% - Ci [6x1] - Damping of each strut [N/(m/s)]</span>
<span class="org-comment">%</span>
<span class="org-comment">% Outputs:</span>
<span class="org-comment">% - stewart - updated Stewart structure with the added fields:</span>
<span class="org-comment">% - Ki [6x1] - Stiffness of each strut [N/m]</span>
<span class="org-comment">% - Ci [6x1] - Damping of each strut [N/(m/s)]</span>
</pre>
</div>
</div>
</div>
<div id="outline-container-org335e959" class="outline-3">
<h3 id="org335e959"><span class="section-number-3">4.2</span> Optional Parameters</h3>
<div class="outline-text-3" id="text-4-2">
<div class="org-src-container">
<pre class="src src-matlab">arguments
stewart
args.Ki (6,1) double {mustBeNumeric, mustBePositive} = 1e6<span class="org-type">*</span>ones(6,1)
args.Ci (6,1) double {mustBeNumeric, mustBePositive} = 1e3<span class="org-type">*</span>ones(6,1)
<span class="org-keyword">end</span>
</pre>
</div>
</div>
</div>
<div id="outline-container-org3c2e550" class="outline-3">
<h3 id="org3c2e550"><span class="section-number-3">4.3</span> Add Stiffness and Damping properties of each strut</h3>
<div class="outline-text-3" id="text-4-3">
<div class="org-src-container">
<pre class="src src-matlab">stewart.Ki = args.Ki;
stewart.Ci = args.Ci;
</pre>
</div>
</div>
</div>
</div>
<div id="outline-container-org9e8cbfa" class="outline-2">
<h2 id="org9e8cbfa"><span class="section-number-2">5</span> <code>computeJacobian</code>: Compute the Jacobian Matrix</h2>
<div class="outline-text-2" id="text-5">
<p>
<a id="orgfb113f5"></a>
</p>
<p>
This Matlab function is accessible <a href="src/computeJacobian.m">here</a>.
</p>
</div>
<div id="outline-container-org64e795c" class="outline-3">
<h3 id="org64e795c"><span class="section-number-3">5.1</span> Function description</h3>
<div class="outline-text-3" id="text-5-1">
<div class="org-src-container">
<pre class="src src-matlab"><span class="org-keyword">function</span> <span class="org-variable-name">[stewart]</span> = <span class="org-function-name">computeJacobian</span>(<span class="org-variable-name">stewart</span>)
<span class="org-comment">% computeJacobian -</span>
<span class="org-comment">%</span>
<span class="org-comment">% Syntax: [stewart] = computeJacobian(stewart)</span>
<span class="org-comment">%</span>
<span class="org-comment">% Inputs:</span>
<span class="org-comment">% - stewart - With at least the following fields:</span>
<span class="org-comment">% - As [3x6] - The 6 unit vectors for each strut expressed in {A}</span>
<span class="org-comment">% - Ab [3x6] - The 6 position of the joints bi expressed in {A}</span>
<span class="org-comment">%</span>
<span class="org-comment">% Outputs:</span>
<span class="org-comment">% - stewart - With the 3 added field:</span>
<span class="org-comment">% - J [6x6] - The Jacobian Matrix</span>
<span class="org-comment">% - K [6x6] - The Stiffness Matrix</span>
<span class="org-comment">% - C [6x6] - The Compliance Matrix</span>
</pre>
</div>
</div>
</div>
<div id="outline-container-org9bcd9b9" class="outline-3">
<h3 id="org9bcd9b9"><span class="section-number-3">5.2</span> Compute Jacobian Matrix</h3>
<div class="outline-text-3" id="text-5-2">
<div class="org-src-container">
<pre class="src src-matlab">stewart.J = [stewart.As<span class="org-type">'</span> , cross(stewart.Ab, stewart.As)<span class="org-type">'</span>];
</pre>
</div>
</div>
</div>
<div id="outline-container-orgf08eda6" class="outline-3">
<h3 id="orgf08eda6"><span class="section-number-3">5.3</span> Compute Stiffness Matrix</h3>
<div class="outline-text-3" id="text-5-3">
<div class="org-src-container">
<pre class="src src-matlab">stewart.K = stewart.J<span class="org-type">'*</span>diag(stewart.Ki)<span class="org-type">*</span>stewart.J;
</pre>
</div>
</div>
</div>
<div id="outline-container-orgd164132" class="outline-3">
<h3 id="orgd164132"><span class="section-number-3">5.4</span> Compute Compliance Matrix</h3>
<div class="outline-text-3" id="text-5-4">
<div class="org-src-container">
<pre class="src src-matlab">stewart.C = inv(stewart.K);
</pre>
</div>
</div>
</div>
</div>
<div id="outline-container-org53d13cc" class="outline-2">
<h2 id="org53d13cc"><span class="section-number-2">6</span> Initialize the Geometry of the Mechanical Elements</h2>
<div class="outline-text-2" id="text-6">
</div>
<div id="outline-container-org4674203" class="outline-3">
<h3 id="org4674203"><span class="section-number-3">6.1</span> <code>initializeCylindricalPlatforms</code>: Initialize the geometry of the Fixed and Mobile Platforms</h3>
<div class="outline-text-3" id="text-6-1">
<p>
<a id="orgac77ed6"></a>
</p>
<p>
This Matlab function is accessible <a href="src/initializeCylindricalPlatforms.m">here</a>.
</p>
</div>
<div id="outline-container-org1af6832" class="outline-4">
<h4 id="org1af6832"><span class="section-number-4">6.1.1</span> Function description</h4>
<div class="outline-text-4" id="text-6-1-1">
<div class="org-src-container">
<pre class="src src-matlab"><span class="org-keyword">function</span> <span class="org-variable-name">[stewart]</span> = <span class="org-function-name">initializeCylindricalPlatforms</span>(<span class="org-variable-name">stewart</span>, <span class="org-variable-name">args</span>)
<span class="org-comment">% initializeCylindricalPlatforms - Initialize the geometry of the Fixed and Mobile Platforms</span>
<span class="org-comment">%</span>
<span class="org-comment">% Syntax: [stewart] = initializeCylindricalPlatforms(args)</span>
<span class="org-comment">%</span>
<span class="org-comment">% Inputs:</span>
<span class="org-comment">% - args - Structure with the following fields:</span>
<span class="org-comment">% - Fpm [1x1] - Fixed Platform Mass [kg]</span>
<span class="org-comment">% - Fph [1x1] - Fixed Platform Height [m]</span>
<span class="org-comment">% - Fpr [1x1] - Fixed Platform Radius [m]</span>
<span class="org-comment">% - Mpm [1x1] - Mobile Platform Mass [kg]</span>
<span class="org-comment">% - Mph [1x1] - Mobile Platform Height [m]</span>
<span class="org-comment">% - Mpr [1x1] - Mobile Platform Radius [m]</span>
<span class="org-comment">%</span>
<span class="org-comment">% Outputs:</span>
<span class="org-comment">% - stewart - updated Stewart structure with the added fields:</span>
<span class="org-comment">% - platforms [struct] - structure with the following fields:</span>
<span class="org-comment">% - Fpm [1x1] - Fixed Platform Mass [kg]</span>
<span class="org-comment">% - Msi [3x3] - Mobile Platform Inertia matrix [kg*m^2]</span>
<span class="org-comment">% - Fph [1x1] - Fixed Platform Height [m]</span>
<span class="org-comment">% - Fpr [1x1] - Fixed Platform Radius [m]</span>
<span class="org-comment">% - Mpm [1x1] - Mobile Platform Mass [kg]</span>
<span class="org-comment">% - Fsi [3x3] - Fixed Platform Inertia matrix [kg*m^2]</span>
<span class="org-comment">% - Mph [1x1] - Mobile Platform Height [m]</span>
<span class="org-comment">% - Mpr [1x1] - Mobile Platform Radius [m]</span>
</pre>
</div>
</div>
</div>
<div id="outline-container-org12a2c2b" class="outline-4">
<h4 id="org12a2c2b"><span class="section-number-4">6.1.2</span> Optional Parameters</h4>
<div class="outline-text-4" id="text-6-1-2">
<div class="org-src-container">
<pre class="src src-matlab">arguments
stewart
args.Fpm (1,1) double {mustBeNumeric, mustBePositive} = 1
args.Fph (1,1) double {mustBeNumeric, mustBePositive} = 10e<span class="org-type">-</span>3
args.Fpr (1,1) double {mustBeNumeric, mustBePositive} = 125e<span class="org-type">-</span>3
args.Mpm (1,1) double {mustBeNumeric, mustBePositive} = 1
args.Mph (1,1) double {mustBeNumeric, mustBePositive} = 10e<span class="org-type">-</span>3
args.Mpr (1,1) double {mustBeNumeric, mustBePositive} = 100e<span class="org-type">-</span>3
<span class="org-keyword">end</span>
</pre>
</div>
</div>
</div>
<div id="outline-container-org2965fe8" class="outline-4">
<h4 id="org2965fe8"><span class="section-number-4">6.1.3</span> Create the <code>platforms</code> struct</h4>
<div class="outline-text-4" id="text-6-1-3">
<div class="org-src-container">
<pre class="src src-matlab">platforms = struct();
platforms.Fpm = args.Fpm;
platforms.Fph = args.Fph;
platforms.Fpr = args.Fpr;
platforms.Fpi = diag([1<span class="org-type">/</span>12 <span class="org-type">*</span> platforms.Fpm <span class="org-type">*</span> (3<span class="org-type">*</span>platforms.Fpr<span class="org-type">^</span>2 <span class="org-type">+</span> platforms.Fph<span class="org-type">^</span>2), ...
1<span class="org-type">/</span>12 <span class="org-type">*</span> platforms.Fpm <span class="org-type">*</span> (3<span class="org-type">*</span>platforms.Fpr<span class="org-type">^</span>2 <span class="org-type">+</span> platforms.Fph<span class="org-type">^</span>2), ...
1<span class="org-type">/</span>2 <span class="org-type">*</span> platforms.Fpm <span class="org-type">*</span> platforms.Fpr<span class="org-type">^</span>2]);
platforms.Mpm = args.Mpm;
platforms.Mph = args.Mph;
platforms.Mpr = args.Mpr;
platforms.Mpi = diag([1<span class="org-type">/</span>12 <span class="org-type">*</span> platforms.Mpm <span class="org-type">*</span> (3<span class="org-type">*</span>platforms.Mpr<span class="org-type">^</span>2 <span class="org-type">+</span> platforms.Mph<span class="org-type">^</span>2), ...
1<span class="org-type">/</span>12 <span class="org-type">*</span> platforms.Mpm <span class="org-type">*</span> (3<span class="org-type">*</span>platforms.Mpr<span class="org-type">^</span>2 <span class="org-type">+</span> platforms.Mph<span class="org-type">^</span>2), ...
1<span class="org-type">/</span>2 <span class="org-type">*</span> platforms.Mpm <span class="org-type">*</span> platforms.Mpr<span class="org-type">^</span>2]);
</pre>
</div>
</div>
</div>
<div id="outline-container-org7e1a4d4" class="outline-4">
<h4 id="org7e1a4d4"><span class="section-number-4">6.1.4</span> Save the <code>platforms</code> struct</h4>
<div class="outline-text-4" id="text-6-1-4">
<div class="org-src-container">
<pre class="src src-matlab">stewart.platforms = platforms;
</pre>
</div>
</div>
</div>
</div>
<div id="outline-container-org6b4f1ca" class="outline-3">
<h3 id="org6b4f1ca"><span class="section-number-3">6.2</span> <code>initializeCylindricalStruts</code>: Define the mass and moment of inertia of cylindrical struts</h3>
<div class="outline-text-3" id="text-6-2">
<p>
<a id="orgfd38bf8"></a>
</p>
<p>
This Matlab function is accessible <a href="src/initializeCylindricalStruts.m">here</a>.
</p>
</div>
<div id="outline-container-org407cf8c" class="outline-4">
<h4 id="org407cf8c"><span class="section-number-4">6.2.1</span> Function description</h4>
<div class="outline-text-4" id="text-6-2-1">
<div class="org-src-container">
<pre class="src src-matlab"><span class="org-keyword">function</span> <span class="org-variable-name">[stewart]</span> = <span class="org-function-name">initializeCylindricalStruts</span>(<span class="org-variable-name">stewart</span>, <span class="org-variable-name">args</span>)
<span class="org-comment">% initializeCylindricalStruts - Define the mass and moment of inertia of cylindrical struts</span>
<span class="org-comment">%</span>
<span class="org-comment">% Syntax: [stewart] = initializeCylindricalStruts(args)</span>
<span class="org-comment">%</span>
<span class="org-comment">% Inputs:</span>
<span class="org-comment">% - args - Structure with the following fields:</span>
<span class="org-comment">% - Fsm [1x1] - Mass of the Fixed part of the struts [kg]</span>
<span class="org-comment">% - Fsh [1x1] - Height of cylinder for the Fixed part of the struts [m]</span>
<span class="org-comment">% - Fsr [1x1] - Radius of cylinder for the Fixed part of the struts [m]</span>
<span class="org-comment">% - Msm [1x1] - Mass of the Mobile part of the struts [kg]</span>
<span class="org-comment">% - Msh [1x1] - Height of cylinder for the Mobile part of the struts [m]</span>
<span class="org-comment">% - Msr [1x1] - Radius of cylinder for the Mobile part of the struts [m]</span>
<span class="org-comment">%</span>
<span class="org-comment">% Outputs:</span>
<span class="org-comment">% - stewart - updated Stewart structure with the added fields:</span>
<span class="org-comment">% - struts [struct] - structure with the following fields:</span>
<span class="org-comment">% - Fsm [6x1] - Mass of the Fixed part of the struts [kg]</span>
<span class="org-comment">% - Fsi [3x3x6] - Moment of Inertia for the Fixed part of the struts [kg*m^2]</span>
<span class="org-comment">% - Msm [6x1] - Mass of the Mobile part of the struts [kg]</span>
<span class="org-comment">% - Msi [3x3x6] - Moment of Inertia for the Mobile part of the struts [kg*m^2]</span>
<span class="org-comment">% - Fsh [6x1] - Height of cylinder for the Fixed part of the struts [m]</span>
<span class="org-comment">% - Fsr [6x1] - Radius of cylinder for the Fixed part of the struts [m]</span>
<span class="org-comment">% - Msh [6x1] - Height of cylinder for the Mobile part of the struts [m]</span>
<span class="org-comment">% - Msr [6x1] - Radius of cylinder for the Mobile part of the struts [m]</span>
</pre>
</div>
</div>
</div>
<div id="outline-container-org420f14e" class="outline-4">
<h4 id="org420f14e"><span class="section-number-4">6.2.2</span> Optional Parameters</h4>
<div class="outline-text-4" id="text-6-2-2">
<div class="org-src-container">
<pre class="src src-matlab">arguments
stewart
args.Fsm (1,1) double {mustBeNumeric, mustBePositive} = 0.1
args.Fsh (1,1) double {mustBeNumeric, mustBePositive} = 50e<span class="org-type">-</span>3
args.Fsr (1,1) double {mustBeNumeric, mustBePositive} = 5e<span class="org-type">-</span>3
args.Msm (1,1) double {mustBeNumeric, mustBePositive} = 0.1
args.Msh (1,1) double {mustBeNumeric, mustBePositive} = 50e<span class="org-type">-</span>3
args.Msr (1,1) double {mustBeNumeric, mustBePositive} = 5e<span class="org-type">-</span>3
<span class="org-keyword">end</span>
</pre>
</div>
</div>
</div>
<div id="outline-container-org3f9f0ef" class="outline-4">
<h4 id="org3f9f0ef"><span class="section-number-4">6.2.3</span> Create the <code>struts</code> structure</h4>
<div class="outline-text-4" id="text-6-2-3">
<div class="org-src-container">
<pre class="src src-matlab">struts = struct();
struts.Fsm = ones(6,1)<span class="org-type">.*</span>args.Fsm;
struts.Msm = ones(6,1)<span class="org-type">.*</span>args.Msm;
struts.Fsh = ones(6,1)<span class="org-type">.*</span>args.Fsh;
struts.Fsr = ones(6,1)<span class="org-type">.*</span>args.Fsr;
struts.Msh = ones(6,1)<span class="org-type">.*</span>args.Msh;
struts.Msr = ones(6,1)<span class="org-type">.*</span>args.Msr;
struts.Fsi = zeros(3, 3, 6);
struts.Msi = zeros(3, 3, 6);
<span class="org-keyword">for</span> <span class="org-variable-name"><span class="org-constant">i</span></span> = <span class="org-constant">1:6</span>
struts.Fsi(<span class="org-type">:</span>,<span class="org-type">:</span>,<span class="org-constant">i</span>) = diag([1<span class="org-type">/</span>12 <span class="org-type">*</span> struts.Fsm(<span class="org-constant">i</span>) <span class="org-type">*</span> (3<span class="org-type">*</span>struts.Fsr(<span class="org-constant">i</span>)<span class="org-type">^</span>2 <span class="org-type">+</span> struts.Fsh(<span class="org-constant">i</span>)<span class="org-type">^</span>2), ...
1<span class="org-type">/</span>12 <span class="org-type">*</span> struts.Fsm(<span class="org-constant">i</span>) <span class="org-type">*</span> (3<span class="org-type">*</span>struts.Fsr(<span class="org-constant">i</span>)<span class="org-type">^</span>2 <span class="org-type">+</span> struts.Fsh(<span class="org-constant">i</span>)<span class="org-type">^</span>2), ...
1<span class="org-type">/</span>2 <span class="org-type">*</span> struts.Fsm(<span class="org-constant">i</span>) <span class="org-type">*</span> struts.Fsr(<span class="org-constant">i</span>)<span class="org-type">^</span>2]);
struts.Msi(<span class="org-type">:</span>,<span class="org-type">:</span>,<span class="org-constant">i</span>) = diag([1<span class="org-type">/</span>12 <span class="org-type">*</span> struts.Msm(<span class="org-constant">i</span>) <span class="org-type">*</span> (3<span class="org-type">*</span>struts.Msr(<span class="org-constant">i</span>)<span class="org-type">^</span>2 <span class="org-type">+</span> struts.Msh(<span class="org-constant">i</span>)<span class="org-type">^</span>2), ...
1<span class="org-type">/</span>12 <span class="org-type">*</span> struts.Msm(<span class="org-constant">i</span>) <span class="org-type">*</span> (3<span class="org-type">*</span>struts.Msr(<span class="org-constant">i</span>)<span class="org-type">^</span>2 <span class="org-type">+</span> struts.Msh(<span class="org-constant">i</span>)<span class="org-type">^</span>2), ...
1<span class="org-type">/</span>2 <span class="org-type">*</span> struts.Msm(<span class="org-constant">i</span>) <span class="org-type">*</span> struts.Msr(<span class="org-constant">i</span>)<span class="org-type">^</span>2]);
<span class="org-keyword">end</span>
</pre>
</div>
<div class="org-src-container">
<pre class="src src-matlab">stewart.struts = struts;
</pre>
</div>
</div>
</div>
</div>
</div>
<div id="outline-container-orgb4dc92b" class="outline-2">
<h2 id="orgb4dc92b"><span class="section-number-2">7</span> Utility Functions</h2>
<div class="outline-text-2" id="text-7">
</div>
<div id="outline-container-org03168fc" class="outline-3">
<h3 id="org03168fc"><span class="section-number-3">7.1</span> <code>inverseKinematics</code>: Compute Inverse Kinematics</h3>
<div class="outline-text-3" id="text-7-1">
<p>
<a id="org681bcb5"></a>
</p>
<p>
This Matlab function is accessible <a href="src/inverseKinematics.m">here</a>.
</p>
</div>
<div id="outline-container-orgb7853bd" class="outline-4">
<h4 id="orgb7853bd"><span class="section-number-4">7.1.1</span> Function description</h4>
<div class="outline-text-4" id="text-7-1-1">
<div class="org-src-container">
<pre class="src src-matlab"><span class="org-keyword">function</span> <span class="org-variable-name">[Li, dLi]</span> = <span class="org-function-name">inverseKinematics</span>(<span class="org-variable-name">stewart</span>, <span class="org-variable-name">args</span>)
<span class="org-comment">% inverseKinematics - Compute the needed length of each strut to have the wanted position and orientation of {B} with respect to {A}</span>
<span class="org-comment">%</span>
<span class="org-comment">% Syntax: [stewart] = inverseKinematics(stewart)</span>
<span class="org-comment">%</span>
<span class="org-comment">% Inputs:</span>
<span class="org-comment">% - stewart - A structure with the following fields</span>
<span class="org-comment">% - Aa [3x6] - The positions ai expressed in {A}</span>
<span class="org-comment">% - Bb [3x6] - The positions bi expressed in {B}</span>
<span class="org-comment">% - args - Can have the following fields:</span>
<span class="org-comment">% - AP [3x1] - The wanted position of {B} with respect to {A}</span>
<span class="org-comment">% - ARB [3x3] - The rotation matrix that gives the wanted orientation of {B} with respect to {A}</span>
<span class="org-comment">%</span>
<span class="org-comment">% Outputs:</span>
<span class="org-comment">% - Li [6x1] - The 6 needed length of the struts in [m] to have the wanted pose of {B} w.r.t. {A}</span>
<span class="org-comment">% - 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}</span>
</pre>
</div>
</div>
</div>
<div id="outline-container-orge9021eb" class="outline-4">
<h4 id="orge9021eb"><span class="section-number-4">7.1.2</span> Optional Parameters</h4>
<div class="outline-text-4" id="text-7-1-2">
<div class="org-src-container">
<pre class="src src-matlab">arguments
stewart
args.AP (3,1) double {mustBeNumeric} = zeros(3,1)
args.ARB (3,3) double {mustBeNumeric} = eye(3)
<span class="org-keyword">end</span>
</pre>
</div>
</div>
</div>
<div id="outline-container-orgbdc5fb1" class="outline-4">
<h4 id="orgbdc5fb1"><span class="section-number-4">7.1.3</span> Theory</h4>
<div class="outline-text-4" id="text-7-1-3">
<p>
For inverse kinematic analysis, it is assumed that the position \({}^A\bm{P}\) and orientation of the moving platform \({}^A\bm{R}_B\) are given and the problem is to obtain the joint variables, namely, \(\bm{L} = [l_1, l_2, \dots, l_6]^T\).
</p>
<p>
From the geometry of the manipulator, the loop closure for each limb, \(i = 1, 2, \dots, 6\) can be written as
</p>
\begin{align*}
l_i {}^A\hat{\bm{s}}_i &= {}^A\bm{A} + {}^A\bm{b}_i - {}^A\bm{a}_i \\
&= {}^A\bm{A} + {}^A\bm{R}_b {}^B\bm{b}_i - {}^A\bm{a}_i
\end{align*}
<p>
To obtain the length of each actuator and eliminate \(\hat{\bm{s}}_i\), it is sufficient to dot multiply each side by itself:
</p>
\begin{equation}
l_i^2 \left[ {}^A\hat{\bm{s}}_i^T {}^A\hat{\bm{s}}_i \right] = \left[ {}^A\bm{P} + {}^A\bm{R}_B {}^B\bm{b}_i - {}^A\bm{a}_i \right]^T \left[ {}^A\bm{P} + {}^A\bm{R}_B {}^B\bm{b}_i - {}^A\bm{a}_i \right]
\end{equation}
<p>
Hence, for \(i = 1, 2, \dots, 6\), each limb length can be uniquely determined by:
</p>
\begin{equation}
l_i = \sqrt{{}^A\bm{P}^T {}^A\bm{P} + {}^B\bm{b}_i^T {}^B\bm{b}_i + {}^A\bm{a}_i^T {}^A\bm{a}_i - 2 {}^A\bm{P}^T {}^A\bm{a}_i + 2 {}^A\bm{P}^T \left[{}^A\bm{R}_B {}^B\bm{b}_i\right] - 2 \left[{}^A\bm{R}_B {}^B\bm{b}_i\right]^T {}^A\bm{a}_i}
\end{equation}
<p>
If the position and orientation of the moving platform lie in the feasible workspace of the manipulator, one unique solution to the limb length is determined by the above equation.
Otherwise, when the limbs&rsquo; lengths derived yield complex numbers, then the position or orientation of the moving platform is not reachable.
</p>
</div>
</div>
<div id="outline-container-org8b70a76" class="outline-4">
<h4 id="org8b70a76"><span class="section-number-4">7.1.4</span> Compute</h4>
<div class="outline-text-4" id="text-7-1-4">
<div class="org-src-container">
<pre class="src src-matlab">Li = sqrt(args.AP<span class="org-type">'*</span>args.AP <span class="org-type">+</span> diag(stewart.Bb<span class="org-type">'*</span>stewart.Bb) <span class="org-type">+</span> diag(stewart.Aa<span class="org-type">'*</span>stewart.Aa) <span class="org-type">-</span> (2<span class="org-type">*</span>args.AP<span class="org-type">'*</span>stewart.Aa)<span class="org-type">'</span> <span class="org-type">+</span> (2<span class="org-type">*</span>args.AP<span class="org-type">'*</span>(args.ARB<span class="org-type">*</span>stewart.Bb))<span class="org-type">'</span> <span class="org-type">-</span> diag(2<span class="org-type">*</span>(args.ARB<span class="org-type">*</span>stewart.Bb)<span class="org-type">'*</span>stewart.Aa));
</pre>
</div>
<div class="org-src-container">
<pre class="src src-matlab">dLi = Li<span class="org-type">-</span>stewart.l;
</pre>
</div>
</div>
</div>
</div>
<div id="outline-container-orgf4ebfa3" class="outline-3">
<h3 id="orgf4ebfa3"><span class="section-number-3">7.2</span> <code>forwardKinematicsApprox</code>: Compute the Forward Kinematics</h3>
<div class="outline-text-3" id="text-7-2">
<p>
<a id="org5b15db4"></a>
</p>
<p>
This Matlab function is accessible <a href="src/forwardKinematicsApprox.m">here</a>.
</p>
</div>
<div id="outline-container-org37e6edf" class="outline-4">
<h4 id="org37e6edf"><span class="section-number-4">7.2.1</span> Function description</h4>
<div class="outline-text-4" id="text-7-2-1">
<div class="org-src-container">
<pre class="src src-matlab"><span class="org-keyword">function</span> <span class="org-variable-name">[P, R]</span> = <span class="org-function-name">forwardKinematicsApprox</span>(<span class="org-variable-name">stewart</span>, <span class="org-variable-name">args</span>)
<span class="org-comment">% forwardKinematicsApprox - Computed the approximate pose of {B} with respect to {A} from the length of each strut and using</span>
<span class="org-comment">% the Jacobian Matrix</span>
<span class="org-comment">%</span>
<span class="org-comment">% Syntax: [P, R] = forwardKinematicsApprox(stewart, args)</span>
<span class="org-comment">%</span>
<span class="org-comment">% Inputs:</span>
<span class="org-comment">% - stewart - A structure with the following fields</span>
<span class="org-comment">% - J [6x6] - The Jacobian Matrix</span>
<span class="org-comment">% - args - Can have the following fields:</span>
<span class="org-comment">% - dL [6x1] - Displacement of each strut [m]</span>
<span class="org-comment">%</span>
<span class="org-comment">% Outputs:</span>
<span class="org-comment">% - P [3x1] - The estimated position of {B} with respect to {A}</span>
<span class="org-comment">% - R [3x3] - The estimated rotation matrix that gives the orientation of {B} with respect to {A}</span>
</pre>
</div>
</div>
</div>
<div id="outline-container-org6441308" class="outline-4">
<h4 id="org6441308"><span class="section-number-4">7.2.2</span> Optional Parameters</h4>
<div class="outline-text-4" id="text-7-2-2">
<div class="org-src-container">
<pre class="src src-matlab">arguments
stewart
args.dL (6,1) double {mustBeNumeric} = zeros(6,1)
<span class="org-keyword">end</span>
</pre>
</div>
</div>
</div>
<div id="outline-container-orgf17cab9" class="outline-4">
<h4 id="orgf17cab9"><span class="section-number-4">7.2.3</span> Computation</h4>
<div class="outline-text-4" id="text-7-2-3">
<p>
From a small displacement of each strut \(d\bm{\mathcal{L}}\), we can compute the
position and orientation of {B} with respect to {A} using the following formula:
\[ d \bm{\mathcal{X}} = \bm{J}^{-1} d\bm{\mathcal{L}} \]
</p>
<div class="org-src-container">
<pre class="src src-matlab">X = stewart.J<span class="org-type">\</span>args.dL;
</pre>
</div>
<p>
The position vector corresponds to the first 3 elements.
</p>
<div class="org-src-container">
<pre class="src src-matlab">P = X(1<span class="org-type">:</span>3);
</pre>
</div>
<p>
The next 3 elements are the orientation of {B} with respect to {A} expressed
using the screw axis.
</p>
<div class="org-src-container">
<pre class="src src-matlab">theta = norm(X(4<span class="org-type">:</span>6));
s = X(4<span class="org-type">:</span>6)<span class="org-type">/</span>theta;
</pre>
</div>
<p>
We then compute the corresponding rotation matrix.
</p>
<div class="org-src-container">
<pre class="src src-matlab">R = [s(1)<span class="org-type">^</span>2<span class="org-type">*</span>(1<span class="org-type">-</span>cos(theta)) <span class="org-type">+</span> cos(theta) , s(1)<span class="org-type">*</span>s(2)<span class="org-type">*</span>(1<span class="org-type">-</span>cos(theta)) <span class="org-type">-</span> s(3)<span class="org-type">*</span>sin(theta), s(1)<span class="org-type">*</span>s(3)<span class="org-type">*</span>(1<span class="org-type">-</span>cos(theta)) <span class="org-type">+</span> s(2)<span class="org-type">*</span>sin(theta);
s<span class="org-type">(2)*s(1)*(1-cos(theta)) + s(3)*sin(theta), s(2)^2*(1-cos(theta)) + cos(theta), s(2)*s(3)*(1-cos(theta)) - s(1)*sin(theta);</span>
s<span class="org-type">(3)*s(1)*(1-cos(theta)) - s(2)*sin(theta), s(3)*s(2)*(1-cos(theta)) + s(1)*sin(theta), s(3)^2*(1-cos(theta)) + cos(theta)];</span>
</pre>
</div>
</div>
</div>
</div>
</div>
</div>
<div id="postamble" class="status">
<p class="author">Author: Dehaeze Thomas</p>
<p class="date">Created: 2020-04-17 ven. 09:36</p>
</div>
</body>
</html>