nass-micro-station-measurem.../modal-analysis/index.org

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#+TITLE: Modal Analysis of the ID31 Micro-Station
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:DRAWER:
#+STARTUP: overview
#+LANGUAGE: en
#+EMAIL: dehaeze.thomas@gmail.com
#+AUTHOR: Dehaeze Thomas
#+HTML_LINK_HOME: ../index.html
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#+HTML_LINK_UP: ../index.html
#+HTML_HEAD: <link rel="stylesheet" type="text/css" href="https://research.tdehaeze.xyz/css/style.css"/>
#+HTML_HEAD: <script type="text/javascript" src="https://research.tdehaeze.xyz/js/script.js"></script>
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#+HTML_MATHJAX: align: center tagside: right font: TeX
:END:
The goal is to experimentally extract a *Spatial Model* (mass, damping, stiffness) of the structure (shown on figure [[fig:nass_picture]]) in order to tune the Multi-Body model.
#+name: fig:nass_picture
#+caption: Picture of the ID31 Micro-Station. (1) Granite (2) Translation Stage (3) Tilt Stage (4) Hexapod (5) Dummy Mass
#+attr_html: :width 500px
[[file:img/nass_picture.png]]
The procedure is represented on figure [[fig:vibration_analysis_procedure]] where we go from left to right.
#+name: fig:vibration_analysis_procedure
#+caption: Vibration Analysis Procedure
#+attr_html: :width 400px
[[file:img/vibration_analysis_procedure.png]]
The steps are:
- we obtain a *Response Model* (Frequency Response Functions) from measurements (described [[file:measurement.org][here]])
- the response model is further converted into a *Modal Model* (Natural Frequencies and Mode Shapes) (described [[file:modal_extraction.org][here]])
- this is converted into a *Spatial Model* with the Mass/Damping/Stiffness matrices (described [[file:mathematical_model.org][here]])
Theses matrices will be used to tune the Simscape (multi-body) model.
The modes we want to identify are those in the frequency range between 0Hz and 150Hz.
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#+name: tab:terminology_numbers
#+caption: Terminology for further analysis
| <c> | <l> | <c> |
| Symbol | Meaning | Value |
|--------+---------------------------------+-------|
| $p$ | Number of solid body considered | 6 |
| $m$ | Number of accelerometers | 23 |
| $n$ | Number of identified modes | 21 |
| $q$ | Number of frequency points | 801 |
| $s$ | Number of excitation | 3 |
#+name: tab:terminology_elements
#+caption: Terminology for further analysis
| <c> | <l> |
| Symbol | Meaning |
|-----------------+--------------------------------------|
| $[\Lambda]$ | Complex eigen value matrix |
| $[\Psi]$ | Complex eigen vector matrix |
| $\omega_r$ | Eigen frequency of mode $r$ [rad/s] |
| $\xi_r$ | Modal damping for mode $r$ |
| $\{\psi\}_r$ | Complex mode shape of mode $r$ |
| $[M], [C], [K]$ | Mass, damping and stiffness matrices |
| $a_r$ | "Modal A" for mode $r$ |
The modal analysis of the ID31 Micro-station thus consists of several parts:
- [[file:measurement.org][Frequency Response Measurements]]
- [[file:frf_processing.org][Frequency Response Analysis and Processing]]
- [[file:modal_extraction.org][Modal Parameter Extraction]]
- [[file:mathematical_model.org][Derivation of Mathematical Model]]
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#+name: fig:modal_test_procedure_vertical
#+caption: Modal Anslysis Procedure
#+attr_html: :width 600px
[[file:figs/modal_test_procedure_vertical.png]]