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modal-analysis/frf_processing.org
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#+PROPERTY: header-args:shell :eval no-export
#+PROPERTY: header-args:latex :headers '("\\usepackage{tikz}" "\\usepackage{import}" "\\import{$HOME/MEGA/These/LaTeX/}{config.tex}")
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@@ -772,3 +772,6 @@ Then, as we know the positions of the accelerometers on each solid body, and we
#+begin_src matlab
save('mat/frf_com.mat', 'FRFs_CoM');
#+end_src
* Bibliography :ignore:
bibliographystyle:unsrt
bibliography:ref.bib

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<!-- 2019-07-03 mer. 13:53 -->
<!-- 2019-10-08 mar. 10:48 -->
<meta http-equiv="Content-Type" content="text/html;charset=utf-8" />
<meta name="viewport" content="width=device-width, initial-scale=1" />
<title>Modal Analysis - Derivation of Mathematical Models</title>
@@ -246,18 +246,261 @@ for the JavaScript code in this tag.
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<div id="org-div-home-and-up">
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</div><div id="content">
<h1 class="title">Modal Analysis - Derivation of Mathematical Models</h1>
<div id="table-of-contents">
<h2>Table of Contents</h2>
<div id="text-table-of-contents">
<ul>
<li><a href="#org93dde66">1. Type of Model</a></li>
<li><a href="#orgfd7d140">2. <span class="todo TODO">TODO</span> Extract Physical Matrices</a></li>
<li><a href="#orgdaaea25">3. Some notes about constraining the number of degrees of freedom</a></li>
</ul>
</div>
</div>
<div id="outline-container-org93dde66" class="outline-2">
<h2 id="org93dde66"><span class="section-number-2">1</span> Type of Model</h2>
<div class="outline-text-2" id="text-1">
<p>
The model that we want to obtain is a <b>multi-body model</b>.
It is composed of several <b>solid bodies connected with springs and dampers</b>.
The solid bodies are represented with different colors on figure <a href="#org4703119">1</a>.
</p>
<p>
In the simscape model, the solid bodies are:
</p>
<ul class="org-ul">
<li>the granite (1 or 2 solids)</li>
<li>the translation stage</li>
<li>the tilt stage</li>
<li>the spindle and slip-ring</li>
<li>the hexapod</li>
</ul>
<div id="org4703119" class="figure">
<p><img src="img/nass_solidworks.png" alt="nass_solidworks.png" width="800px" />
</p>
<p><span class="figure-number">Figure 1: </span>CAD view of the ID31 Micro-Station</p>
</div>
<p>
However, each of the DOF of the system may not be relevant for the modes present in the frequency band of interest.
For instance, the translation stage may not vibrate in the Z direction for all the modes identified. Then, we can block this DOF and this simplifies the model.
</p>
<p>
The modal identification done here will thus permit us to determine <b>which DOF can be neglected</b>.
</p>
</div>
</div>
<div id="outline-container-orgfd7d140" class="outline-2">
<h2 id="orgfd7d140"><span class="section-number-2">2</span> <span class="todo TODO">TODO</span> Extract Physical Matrices</h2>
<div class="outline-text-2" id="text-2">
<p>
<a class='org-ref-reference' href="#wang11_extrac_real_modes_physic_matric">wang11_extrac_real_modes_physic_matric</a>
</p>
<p>
Let's recall that:
\[ \Lambda = \begin{bmatrix}
s_1 & & 0 \\
& \ddots & \\
0 & & s_N
\end{bmatrix}_{N \times N}; \quad \Psi = \begin{bmatrix}
& & \\
\{\psi_1\} & \dots & \{\psi_N\} \\
& &
\end{bmatrix}_{M \times N} ; \quad A = \begin{bmatrix}
a_1 & & 0 \\
& \ddots & \\
0 & & a_N
\end{bmatrix}_{N \times N}; \]
</p>
\begin{align}
M &= \frac{1}{2} \left[ \text{Re}(\Psi A^{-1} \Lambda \Psi^T ) \right]^{-1} \\
C &= -2 M \text{Re}(\Psi A^{-1} \Lambda^2 A^{-1} \Psi^T ) M \\
K &= -\frac{1}{2} \left[ \text{Re}(\Psi \Lambda^{-1} A^{-1} \Psi^T) \right]^{-1}
\end{align}
<div class="org-src-container">
<pre class="src src-matlab">psi = eigen_vec_CoM;
a = modal_a_M;
lambda = eigen_val_M;
M = <span class="org-highlight-numbers-number">0</span>.<span class="org-highlight-numbers-number">5</span><span class="org-type">*</span>inv<span class="org-rainbow-delimiters-depth-1">(</span>real<span class="org-rainbow-delimiters-depth-2">(</span>psi<span class="org-type">*</span>inv<span class="org-rainbow-delimiters-depth-3">(</span>a<span class="org-rainbow-delimiters-depth-3">)</span><span class="org-type">*</span>lambda<span class="org-type">*</span>psi'<span class="org-rainbow-delimiters-depth-2">)</span><span class="org-rainbow-delimiters-depth-1">)</span>;
C = <span class="org-type">-</span><span class="org-highlight-numbers-number">2</span><span class="org-type">*</span>M<span class="org-type">*</span>real<span class="org-rainbow-delimiters-depth-1">(</span>psi<span class="org-type">*</span>inv<span class="org-rainbow-delimiters-depth-2">(</span>a<span class="org-rainbow-delimiters-depth-2">)</span><span class="org-type">*</span>lambda<span class="org-type">^</span><span class="org-highlight-numbers-number">2</span><span class="org-type">*</span>inv<span class="org-rainbow-delimiters-depth-2">(</span>a<span class="org-rainbow-delimiters-depth-2">)</span><span class="org-type">*</span>psi'<span class="org-rainbow-delimiters-depth-1">)</span><span class="org-type">*</span>M;
K = <span class="org-type">-</span><span class="org-highlight-numbers-number">0</span>.<span class="org-highlight-numbers-number">5</span><span class="org-type">*</span>inv<span class="org-rainbow-delimiters-depth-1">(</span>real<span class="org-rainbow-delimiters-depth-2">(</span>psi<span class="org-type">*</span>inv<span class="org-rainbow-delimiters-depth-3">(</span>lambda<span class="org-rainbow-delimiters-depth-3">)</span><span class="org-type">*</span>inv<span class="org-rainbow-delimiters-depth-3">(</span>a<span class="org-rainbow-delimiters-depth-3">)</span><span class="org-type">*</span>psi'<span class="org-rainbow-delimiters-depth-2">)</span><span class="org-rainbow-delimiters-depth-1">)</span>;
</pre>
</div>
<p>
From <a class='org-ref-reference' href="#ewins00_modal">ewins00_modal</a>
</p>
\begin{align}
[M] &= [\Phi]^{-T} [I] [\Phi]^{-1} \\
[K] &= [\Phi]^{-T} [\lambda_r^2] [\Phi]^{-1}
\end{align}
</div>
</div>
<div id="outline-container-orgdaaea25" class="outline-2">
<h2 id="orgdaaea25"><span class="section-number-2">3</span> Some notes about constraining the number of degrees of freedom</h2>
<div class="outline-text-2" id="text-3">
<p>
We want to have the two eigen matrices.
</p>
<p>
They should have the same size \(n \times n\) where \(n\) is the number of modes as well as the number of degrees of freedom.
Thus, if we consider 21 modes, we should restrict our system to have only 21 DOFs.
</p>
<p>
Actually, we are measured 6 DOFs of 6 solids, thus we have 36 DOFs.
</p>
<p>
From the mode shapes animations, it seems that in the frequency range of interest, the two marbles can be considered as one solid.
We thus have 5 solids and 30 DOFs.
</p>
<p>
In order to determine which DOF can be neglected, two solutions seems possible:
</p>
<ul class="org-ul">
<li>compare the mode shapes</li>
<li>compare the FRFs</li>
</ul>
<p>
The question is: in which base (frame) should be express the modes shapes and FRFs?
Is it meaningful to compare mode shapes as they give no information about the amplitudes of vibration?
</p>
<table border="2" cellspacing="0" cellpadding="6" rules="groups" frame="hsides">
<colgroup>
<col class="org-left" />
<col class="org-right" />
<col class="org-right" />
<col class="org-right" />
<col class="org-left" />
</colgroup>
<thead>
<tr>
<th scope="col" class="org-left">Stage</th>
<th scope="col" class="org-right">Motion DOFs</th>
<th scope="col" class="org-right">Parasitic DOF</th>
<th scope="col" class="org-right">Total DOF</th>
<th scope="col" class="org-left">Description of DOF</th>
</tr>
</thead>
<tbody>
<tr>
<td class="org-left">Granite</td>
<td class="org-right">0</td>
<td class="org-right">3</td>
<td class="org-right">3</td>
<td class="org-left">&#xa0;</td>
</tr>
<tr>
<td class="org-left">Ty</td>
<td class="org-right">1</td>
<td class="org-right">2</td>
<td class="org-right">3</td>
<td class="org-left">Ty, Rz</td>
</tr>
<tr>
<td class="org-left">Ry</td>
<td class="org-right">1</td>
<td class="org-right">2</td>
<td class="org-right">3</td>
<td class="org-left">Ry,</td>
</tr>
<tr>
<td class="org-left">Rz</td>
<td class="org-right">1</td>
<td class="org-right">2</td>
<td class="org-right">3</td>
<td class="org-left">Rz, Rx, Ry</td>
</tr>
<tr>
<td class="org-left">Hexapod</td>
<td class="org-right">6</td>
<td class="org-right">0</td>
<td class="org-right">6</td>
<td class="org-left">Txyz, Rxyz</td>
</tr>
</tbody>
<tbody>
<tr>
<td class="org-left">&#xa0;</td>
<td class="org-right">9</td>
<td class="org-right">9</td>
<td class="org-right">18</td>
<td class="org-left">&#xa0;</td>
</tr>
</tbody>
</table>
</div>
</div>
<p>
<h1 class='org-ref-bib-h1'>Bibliography</h1>
<ul class='org-ref-bib'><li><a id="wang11_extrac_real_modes_physic_matric">[wang11_extrac_real_modes_physic_matric]</a> <a name="wang11_extrac_real_modes_physic_matric"></a>Tong Wang, Lingmi Zhang & Kong Fah Tee, Extraction of Real Modes and Physical Matrices From Modal Testing, <i>Earthquake Engineering and Engineering Vibration</i>, <b>10(2)</b>, 219-227 (2011). <a href="https://doi.org/10.1007/s11803-011-0060-6">link</a>. <a href="http://dx.doi.org/10.1007/s11803-011-0060-6">doi</a>.</li>
<li><a id="ewins00_modal">[ewins00_modal]</a> <a name="ewins00_modal"></a>Ewins, Modal testing: theory, practice and application, Wiley-Blackwell (2000).</li>
</ul>
</p>
</div>
<div id="postamble" class="status">
<p class="author">Author: Dehaeze Thomas</p>
<p class="date">Created: 2019-07-03 mer. 13:53</p>
<p class="date">Created: 2019-10-08 mar. 10:48</p>
<p class="validation"><a href="http://validator.w3.org/check?uri=referer">Validate</a></p>
</div>
</body>

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| | 9 | 9 | 18 | |
#+TBLFM: $4=vsum($2..$3)
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