649 lines
25 KiB
Org Mode
649 lines
25 KiB
Org Mode
#+TITLE: Identification of the disturbances
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:DRAWER:
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#+STARTUP: overview
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#+LANGUAGE: en
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#+EMAIL: dehaeze.thomas@gmail.com
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#+AUTHOR: Dehaeze Thomas
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#+HTML_LINK_HOME: ./index.html
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#+HTML_LINK_UP: ./index.html
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#+HTML_HEAD: <link rel="stylesheet" type="text/css" href="./css/htmlize.css"/>
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#+HTML_HEAD: <link rel="stylesheet" type="text/css" href="./css/readtheorg.css"/>
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#+HTML_HEAD: <link rel="stylesheet" type="text/css" href="./css/zenburn.css"/>
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#+HTML_HEAD: <script type="text/javascript" src="./js/jquery.min.js"></script>
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#+HTML_HEAD: <script type="text/javascript" src="./js/readtheorg.js"></script>
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#+HTML_MATHJAX: align: center tagside: right font: TeX
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#+PROPERTY: header-args:matlab :session *MATLAB*
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#+PROPERTY: header-args:matlab+ :comments org
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#+PROPERTY: header-args:matlab+ :results none
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#+PROPERTY: header-args:matlab+ :exports both
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#+PROPERTY: header-args:matlab+ :eval no-export
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#+PROPERTY: header-args:matlab+ :output-dir figs
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#+PROPERTY: header-args:matlab+ :tangle no
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#+PROPERTY: header-args:matlab+ :mkdirp yes
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#+PROPERTY: header-args:shell :eval no-export
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#+PROPERTY: header-args:latex :headers '("\\usepackage{tikz}" "\\usepackage{import}" "\\import{$HOME/Cloud/thesis/latex/org/}{config.tex}")
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#+PROPERTY: header-args:latex+ :imagemagick t :fit yes
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#+PROPERTY: header-args:latex+ :iminoptions -scale 100% -density 150
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#+PROPERTY: header-args:latex+ :imoutoptions -quality 100
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#+PROPERTY: header-args:latex+ :results raw replace :buffer no
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#+PROPERTY: header-args:latex+ :eval no-export
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#+PROPERTY: header-args:latex+ :exports both
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#+PROPERTY: header-args:latex+ :mkdirp yes
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#+PROPERTY: header-args:latex+ :output-dir figs
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:END:
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* Introduction :ignore:
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:PROPERTIES:
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:CUSTOM_ID: Introduction
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:END:
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The goal here is to extract the Power Spectral Density of the sources of perturbation.
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The sources of perturbations are (schematically shown in figure [[fig:uniaxial-model-micro-station]]):
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- $D_w$: Ground Motion
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- Parasitic forces applied in the system when scanning with the Translation Stage and the Spindle ($F_{rz}$ and $F_{ty}$).
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These forces can be due to imperfect guiding for instance.
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Because we cannot measure directly the perturbation forces, we have the measure the effect of those perturbations on the system (in terms of velocity for instance using geophones, $D$ on figure [[fig:uniaxial-model-micro-station]]) and then, using a model, compute the forces that induced such velocity.
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#+begin_src latex :file uniaxial-model-micro-station.pdf :post pdf2svg(file=*this*, ext="png") :exports results
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\begin{tikzpicture}
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% ====================
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% Parameters
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% ====================
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\def\massw{2.2} % Width of the masses
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\def\massh{0.8} % Height of the masses
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\def\spaceh{1.2} % Height of the springs/dampers
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\def\dispw{0.4} % Width of the dashed line for the displacement
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\def\disph{0.3} % Height of the arrow for the displacements
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\def\bracs{0.05} % Brace spacing vertically
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\def\brach{-12pt} % Brace shift horizontaly
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\def\fsensh{0.2} % Height of the force sensor
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\def\velsize{0.2} % Size of the velocity sensor
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% ====================
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% ====================
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% Ground
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% ====================
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\draw (-0.5*\massw, 0) -- (0.5*\massw, 0);
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\draw[dashed] (0.5*\massw, 0) -- ++(1, 0);
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\draw[->, dasehd] (0.5*\massw+0.8, 0) -- ++(0, 0.5) node[right]{$D_{w}$};
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% ====================
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% ====================
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% Marble
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\begin{scope}[shift={(0, 0)}]
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% Mass
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\draw[fill=white] (-0.5*\massw, \spaceh) rectangle (0.5*\massw, \spaceh+\massh) node[pos=0.5]{$m_{m}$};
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% Spring, Damper, and Actuator
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\draw[spring] (-0.4*\massw, 0) -- (-0.4*\massw, \spaceh) node[midway, left=0.1]{$k_{m}$};
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\draw[damper] (0, 0) -- ( 0, \spaceh) node[midway, left=0.2]{$c_{m}$};
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% Legend
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\draw[decorate, decoration={brace, amplitude=8pt}, xshift=\brach] %
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(-0.5*\massw, \bracs) -- (-0.5*\massw, \spaceh+\massh-\bracs) node[midway,rotate=90,anchor=south,yshift=10pt]{Marble};
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% Displacements
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\draw[dashed] (0.5*\massw, \spaceh+\massh) -- ++(2*\dispw, 0) coordinate(xm) -- ++(2.2*\dispw, 0) coordinate(dbot);
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\end{scope}
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% ====================
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% ====================
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% Ty
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\begin{scope}[shift={(0, \spaceh+\massh)}]
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% Mass
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\draw[fill=white] (-0.5*\massw, \spaceh) rectangle (0.5*\massw, \spaceh+\massh) node[pos=0.5]{$m_{t}$};
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% Spring, Damper, and Actuator
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\draw[spring] (-0.4*\massw, 0) -- (-0.4*\massw, \spaceh) node[midway, left=0.1]{$k_{t}$};
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\draw[damper] (0, 0) -- ( 0, \spaceh) node[midway, left=0.2]{$c_{t}$};
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\draw[actuator={0.45}{0.2}] ( 0.4*\massw, 0) -- ( 0.4*\massw, \spaceh) node[midway, right=0.1](ft){$F_{ty}$};
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% Legend
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\draw[decorate, decoration={brace, amplitude=8pt}, xshift=\brach] %
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(-0.5*\massw, \bracs) -- (-0.5*\massw, \spaceh+\massh-\bracs) node[midway,rotate=90,anchor=south,yshift=10pt]{Ty};
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\end{scope}
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% ====================
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% ====================
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% Rz
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\begin{scope}[shift={(0, 2*(\spaceh+\massh))}]
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% Mass
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\draw[fill=white] (-0.5*\massw, \spaceh) rectangle (0.5*\massw, \spaceh+\massh) node[pos=0.5]{$m_{z}$};
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% Spring, Damper, and Actuator
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\draw[spring] (-0.4*\massw, 0) -- (-0.4*\massw, \spaceh) node[midway, left=0.1]{$k_{z}$};
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\draw[damper] (0, 0) -- ( 0, \spaceh) node[midway, left=0.2]{$c_{z}$};
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\draw[actuator] ( 0.4*\massw, 0) -- ( 0.4*\massw, \spaceh) node[midway, right=0.1](F){$F_{rz}$};
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% Legend
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\draw[decorate, decoration={brace, amplitude=8pt}, xshift=\brach] %
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(-0.5*\massw, \bracs) -- (-0.5*\massw, \spaceh+\massh-\bracs) node[midway,rotate=90,anchor=south,yshift=10pt]{Rz};
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\end{scope}
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% ====================
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% ====================
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% Hexapod
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\begin{scope}[shift={(0, 3*(\spaceh+\massh))}]
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% Mass
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\draw[fill=white] (-0.5*\massw, \spaceh) rectangle (0.5*\massw, \spaceh+\massh) node[pos=0.5]{$m_{h}$};
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% Spring, Damper, and Actuator
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\draw[spring] (-0.4*\massw, 0) -- (-0.4*\massw, \spaceh) node[midway, left=0.1]{$k_{h}$};
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\draw[damper] (0, 0) -- ( 0, \spaceh) node[midway, left=0.2]{$c_{h}$};
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% Displacements
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\draw[dashed] (0.5*\massw, \spaceh+\massh) -- ++(2*\dispw, 0) coordinate(xs) -- ++(2.2*\dispw, 0) coordinate(dtop);
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% Legend
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\draw[decorate, decoration={brace, amplitude=8pt}, xshift=\brach] %
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(-0.5*\massw, \bracs) -- (-0.5*\massw, \spaceh+\massh-\bracs) node[midway,rotate=90,anchor=south,yshift=10pt]{Hexapod};
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\end{scope}
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% ====================
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\draw[<->] ($(dbot)+(-0.3,0)$) --node[midway, right]{$D$} ($(dtop)+(-0.3,0)$);
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\end{tikzpicture}
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#+end_src
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#+name: fig:uniaxial-model-micro-station
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#+caption: Schematic of the Micro Station and the sources of disturbance
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#+RESULTS:
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[[file:figs/uniaxial-model-micro-station.png]]
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This file is divided in the following sections:
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- Section [[sec:simscape_model]]: the simscape model used here is presented
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- Section [[sec:identification]]: transfer functions from the disturbance forces to the relative velocity of the hexapod with respect to the granite are computed using the Simscape Model representing the experimental setup
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- Section [[sec:sensitivity_disturbances]]: the bode plot of those transfer functions are shown
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- Section [[sec:psd_dist]]: the measured PSD of the effect of the disturbances are shown
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- Section [[sec:psd_force_dist]]: from the model and the measured PSD, the PSD of the disturbance forces are computed
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- Section [[sec:noise_budget]]: with the computed PSD, the noise budget of the system is done
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* Matlab Init :noexport:ignore:
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:PROPERTIES:
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:CUSTOM_ID: Matlab-Init
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:END:
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#+begin_src matlab :tangle no :exports none :results silent :noweb yes :var current_dir=(file-name-directory buffer-file-name)
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<<matlab-dir>>
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#+end_src
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#+begin_src matlab :exports none :results silent :noweb yes
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<<matlab-init>>
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#+end_src
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#+begin_src matlab :tangle no
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simulinkproject('../');
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#+end_src
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#+begin_src matlab
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open('nass_model.slx')
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#+end_src
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* Simscape Model
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:PROPERTIES:
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:CUSTOM_ID: Simscape-Model
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:END:
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<<sec:simscape_model>>
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The following Simscape model of the micro-station is the same model used for the dynamical analysis.
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However, we here constrain all the stage to only move in the vertical direction.
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We add disturbances forces in the vertical direction for the Translation Stage and the Spindle.
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Also, we measure the absolute displacement of the granite and of the top platform of the Hexapod.
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We load the configuration and we set a small =StopTime=.
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#+begin_src matlab
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load('mat/conf_simulink.mat');
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set_param(conf_simulink, 'StopTime', '0.5');
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#+end_src
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We initialize all the stages.
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#+begin_src matlab
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initializeGround();
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initializeGranite('type', 'modal-analysis');
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initializeTy();
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initializeRy();
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initializeRz();
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initializeMicroHexapod('type', 'modal-analysis');
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initializeAxisc('type', 'none');
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initializeMirror('type', 'none');
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initializeNanoHexapod('type', 'none');
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initializeSample('type', 'none');
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#+end_src
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* Identification
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:PROPERTIES:
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:CUSTOM_ID: Identification
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:END:
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<<sec:identification>>
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The transfer functions from the disturbance forces to the relative velocity of the hexapod with respect to the granite are computed using the Simscape Model representing the experimental setup with the code below.
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#+begin_src matlab
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%% Options for Linearized
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options = linearizeOptions;
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options.SampleTime = 0;
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%% Name of the Simulink File
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mdl = 'nass_model';
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#+end_src
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#+begin_src matlab
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%% Micro-Hexapod
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clear io; io_i = 1;
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io(io_i) = linio([mdl, '/Disturbances'], 1, 'openinput', [], 'Dwz'); io_i = io_i + 1; % Vertical Ground Motion
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io(io_i) = linio([mdl, '/Disturbances'], 1, 'openinput', [], 'Fty_z'); io_i = io_i + 1; % Parasitic force Ty
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io(io_i) = linio([mdl, '/Disturbances'], 1, 'openinput', [], 'Frz_z'); io_i = io_i + 1; % Parasitic force Rz
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io(io_i) = linio([mdl, '/Micro-Station/Granite/Modal Analysis/accelerometer'], 1, 'openoutput'); io_i = io_i + 1; % Absolute motion - Granite
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io(io_i) = linio([mdl, '/Micro-Station/Micro Hexapod/Modal Analysis/accelerometer'], 1, 'openoutput'); io_i = io_i + 1; % Absolute Motion - Hexapod
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% io(io_i) = linio([mdl, '/Vm'], 1, 'openoutput'); io_i = io_i + 1; % Relative Velocity hexapod/granite
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#+end_src
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#+begin_src matlab
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% Run the linearization
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G = linearize(mdl, io, 0);
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% We Take only the outputs corresponding to the vertical acceleration
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G = G([3,9], :);
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% Input/Output names
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G.InputName = {'Dw', 'Fty', 'Frz'};
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G.OutputName = {'Agm', 'Ahm'};
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% We integrate 1 time the output to have the velocity and we
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% substract the absolute velocities to have the relative velocity
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G = (1/s)*tf([-1, 1])*G;
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% Input/Output names
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G.InputName = {'Dw', 'Fty', 'Frz'};
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G.OutputName = {'Vm'};
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#+end_src
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* Sensitivity to Disturbances
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:PROPERTIES:
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:CUSTOM_ID: Sensitivity-to-Disturbances
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:END:
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<<sec:sensitivity_disturbances>>
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#+begin_src matlab :exports none
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freqs = logspace(0, 3, 1000);
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figure;
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title('$D_w$ to $D$');
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hold on;
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plot(freqs, abs(squeeze(freqresp(G('Vm', 'Dw')/s, freqs, 'Hz'))), 'k-');
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hold off;
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set(gca, 'XScale', 'log'); set(gca, 'YScale', 'log');
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ylabel('Amplitude [m/m]'); xlabel('Frequency [Hz]');
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#+end_src
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#+HEADER: :tangle no :exports results :results none :noweb yes
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#+begin_src matlab :var filepath="figs/sensitivity_dist_gm.pdf" :var figsize="wide-normal" :post pdf2svg(file=*this*, ext="png")
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<<plt-matlab>>
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#+end_src
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#+NAME: fig:sensitivity_dist_gm
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#+CAPTION: Sensitivity to Ground Motion ([[./figs/sensitivity_dist_gm.png][png]], [[./figs/sensitivity_dist_gm.pdf][pdf]])
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[[file:figs/sensitivity_dist_gm.png]]
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#+begin_src matlab :exports none
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freqs = logspace(0, 3, 1000);
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figure;
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title('$F_{ty}$ to $D$');
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hold on;
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plot(freqs, abs(squeeze(freqresp(G('Vm', 'Fty')/s, freqs, 'Hz'))), 'k-');
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hold off;
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set(gca, 'XScale', 'log'); set(gca, 'YScale', 'log');
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ylabel('Amplitude [m/N]'); xlabel('Frequency [Hz]');
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#+end_src
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#+HEADER: :tangle no :exports results :results none :noweb yes
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#+begin_src matlab :var filepath="figs/sensitivity_dist_fty.pdf" :var figsize="wide-normal" :post pdf2svg(file=*this*, ext="png")
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<<plt-matlab>>
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#+end_src
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#+NAME: fig:sensitivity_dist_fty
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#+CAPTION: Sensitivity to vertical forces applied by the Ty stage ([[./figs/sensitivity_dist_fty.png][png]], [[./figs/sensitivity_dist_fty.pdf][pdf]])
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[[file:figs/sensitivity_dist_fty.png]]
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#+begin_src matlab :exports none
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freqs = logspace(0, 3, 1000);
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figure;
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title('$F_{rz}$ to $D$');
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hold on;
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plot(freqs, abs(squeeze(freqresp(G('Vm', 'Frz')/s, freqs, 'Hz'))), 'k-');
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hold off;
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set(gca, 'XScale', 'log'); set(gca, 'YScale', 'log');
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ylabel('Amplitude [m/N]'); xlabel('Frequency [Hz]');
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#+end_src
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#+HEADER: :tangle no :exports results :results none :noweb yes
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#+begin_src matlab :var filepath="figs/sensitivity_dist_frz.pdf" :var figsize="wide-normal" :post pdf2svg(file=*this*, ext="png")
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<<plt-matlab>>
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#+end_src
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#+NAME: fig:sensitivity_dist_frz
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#+CAPTION: Sensitivity to vertical forces applied by the Rz stage ([[./figs/sensitivity_dist_frz.png][png]], [[./figs/sensitivity_dist_frz.pdf][pdf]])
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[[file:figs/sensitivity_dist_frz.png]]
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* Power Spectral Density of the effect of the disturbances
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:PROPERTIES:
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:CUSTOM_ID: Power-Spectral-Density-of-the-effect-of-the-disturbances
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:END:
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<<sec:psd_dist>>
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The PSD of the relative velocity between the hexapod and the marble in $[(m/s)^2/Hz]$ are loaded for the following sources of disturbance:
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- Slip Ring Rotation
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- Scan of the translation stage (effect in the vertical direction and in the horizontal direction)
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Also, the Ground Motion is measured.
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#+begin_src matlab
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gm = load('./mat/psd_gm.mat', 'f', 'psd_gm');
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rz = load('./mat/pxsp_r.mat', 'f', 'pxsp_r');
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tyz = load('./mat/pxz_ty_r.mat', 'f', 'pxz_ty_r');
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tyx = load('./mat/pxe_ty_r.mat', 'f', 'pxe_ty_r');
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#+end_src
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#+begin_src matlab :exports none
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gm.f = gm.f(2:end);
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rz.f = rz.f(2:end);
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tyz.f = tyz.f(2:end);
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tyx.f = tyx.f(2:end);
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gm.psd_gm = gm.psd_gm(2:end); % PSD of Ground Motion [m^2/Hz]
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gm.psd_gv = gm.psd_gv(2:end); % PSD of Ground Velocity [(m/s)^2/Hz]
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rz.pxsp_r = rz.pxsp_r(2:end); % PSD of Relative Velocity [(m/s)^2/Hz]
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tyz.pxz_ty_r = tyz.pxz_ty_r(2:end); % PSD of Relative Velocity [(m/s)^2/Hz]
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tyx.pxe_ty_r = tyx.pxe_ty_r(2:end); % PSD of Relative Velocity [(m/s)^2/Hz]
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#+end_src
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We now compute the relative velocity between the hexapod and the granite due to ground motion.
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#+begin_src matlab
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gm.psd_rv = gm.psd_gm.*abs(squeeze(freqresp(G('Vm', 'Dw'), gm.f, 'Hz'))).^2;
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#+end_src
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The Power Spectral Density of the relative motion/velocity of the hexapod with respect to the granite are shown in figures [[fig:dist_effect_relative_velocity]] and [[fig:dist_effect_relative_motion]].
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The Cumulative Amplitude Spectrum of the relative motion is shown in figure [[fig:dist_effect_relative_motion_cas]].
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#+begin_src matlab :exports none
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figure;
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hold on;
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plot(gm.f, sqrt(gm.psd_rv), 'DisplayName', 'Ground Motion');
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plot(tyz.f, sqrt(tyz.pxz_ty_r), 'DisplayName', 'Ty');
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plot(rz.f, sqrt(rz.pxsp_r), 'DisplayName', 'Rz');
|
|
hold off;
|
|
set(gca, 'xscale', 'log'); set(gca, 'yscale', 'log');
|
|
xlabel('Frequency [Hz]'); ylabel('ASD of the measured velocity $\left[\frac{m/s}{\sqrt{Hz}}\right]$')
|
|
legend('Location', 'southwest');
|
|
xlim([2, 500]);
|
|
#+end_src
|
|
|
|
#+HEADER: :tangle no :exports results :results none :noweb yes
|
|
#+begin_src matlab :var filepath="figs/dist_effect_relative_velocity.pdf" :var figsize="full-tall" :post pdf2svg(file=*this*, ext="png")
|
|
<<plt-matlab>>
|
|
#+end_src
|
|
|
|
#+NAME: fig:dist_effect_relative_velocity
|
|
#+CAPTION: Amplitude Spectral Density of the relative velocity of the hexapod with respect to the granite due to different sources of perturbation ([[./figs/dist_effect_relative_velocity.png][png]], [[./figs/dist_effect_relative_velocity.pdf][pdf]])
|
|
[[file:figs/dist_effect_relative_velocity.png]]
|
|
|
|
|
|
#+begin_src matlab :exports none
|
|
figure;
|
|
hold on;
|
|
plot(gm.f, sqrt(gm.psd_rv)./(2*pi*gm.f), 'DisplayName', 'Ground Motion');
|
|
plot(tyz.f, sqrt(tyz.pxz_ty_r)./(2*pi*tyz.f), 'DisplayName', 'Ty');
|
|
plot(rz.f, sqrt(rz.pxsp_r)./(2*pi*rz.f), 'DisplayName', 'Rz');
|
|
hold off;
|
|
set(gca, 'xscale', 'log'); set(gca, 'yscale', 'log');
|
|
xlabel('Frequency [Hz]'); ylabel('ASD of the displacement $\left[\frac{m}{\sqrt{Hz}}\right]$')
|
|
legend('Location', 'southwest');
|
|
xlim([2, 500]);
|
|
#+end_src
|
|
|
|
#+HEADER: :tangle no :exports results :results none :noweb yes
|
|
#+begin_src matlab :var filepath="figs/dist_effect_relative_motion.pdf" :var figsize="full-tall" :post pdf2svg(file=*this*, ext="png")
|
|
<<plt-matlab>>
|
|
#+end_src
|
|
|
|
#+NAME: fig:dist_effect_relative_motion
|
|
#+CAPTION: Amplitude Spectral Density of the relative displacement of the hexapod with respect to the granite due to different sources of perturbation ([[./figs/dist_effect_relative_motion.png][png]], [[./figs/dist_effect_relative_motion.pdf][pdf]])
|
|
[[file:figs/dist_effect_relative_motion.png]]
|
|
|
|
#+begin_src matlab :exports none
|
|
figure;
|
|
hold on;
|
|
plot(gm.f, flip(sqrt(-cumtrapz(flip(gm.f), flip(gm.psd_rv./((2*pi*gm.f).^2))))), 'DisplayName', 'Ground Motion');
|
|
plot(tyz.f, flip(sqrt(-cumtrapz(flip(tyz.f), flip(tyz.pxz_ty_r./((2*pi*tyz.f).^2))))), 'DisplayName', 'Ty');
|
|
plot(rz.f, flip(sqrt(-cumtrapz(flip(rz.f), flip(rz.pxsp_r./((2*pi*rz.f).^2))))), 'DisplayName', 'Rz');
|
|
hold off;
|
|
set(gca, 'xscale', 'log'); set(gca, 'yscale', 'log');
|
|
xlabel('Frequency [Hz]'); ylabel('CAS of the relative displacement $[m]$')
|
|
legend('Location', 'southwest');
|
|
xlim([2, 500]); ylim([1e-11, 1e-6]);
|
|
#+end_src
|
|
|
|
#+HEADER: :tangle no :exports results :results none :noweb yes
|
|
#+begin_src matlab :var filepath="figs/dist_effect_relative_motion_cas.pdf" :var figsize="full-tall" :post pdf2svg(file=*this*, ext="png")
|
|
<<plt-matlab>>
|
|
#+end_src
|
|
|
|
#+NAME: fig:dist_effect_relative_motion_cas
|
|
#+CAPTION: Cumulative Amplitude Spectrum of the relative motion due to different sources of perturbation ([[./figs/dist_effect_relative_motion_cas.png][png]], [[./figs/dist_effect_relative_motion_cas.pdf][pdf]])
|
|
[[file:figs/dist_effect_relative_motion_cas.png]]
|
|
|
|
* Compute the Power Spectral Density of the disturbance force
|
|
:PROPERTIES:
|
|
:CUSTOM_ID: Compute-the-Power-Spectral-Density-of-the-disturbance-force
|
|
:END:
|
|
<<sec:psd_force_dist>>
|
|
|
|
Now, from the extracted transfer functions from the disturbance force to the relative motion of the hexapod with respect to the granite (section [[sec:sensitivity_disturbances]]) and from the measured PSD of the relative motion (section [[sec:psd_dist]]), we can compute the PSD of the disturbance force.
|
|
|
|
#+begin_src matlab
|
|
rz.psd_f = rz.pxsp_r./abs(squeeze(freqresp(G('Vm', 'Frz'), rz.f, 'Hz'))).^2;
|
|
tyz.psd_f = tyz.pxz_ty_r./abs(squeeze(freqresp(G('Vm', 'Fty'), tyz.f, 'Hz'))).^2;
|
|
#+end_src
|
|
|
|
#+begin_src matlab :exports none
|
|
figure;
|
|
hold on;
|
|
set(gca,'ColorOrderIndex',2);
|
|
plot(tyz.f, sqrt(tyz.psd_f), 'DisplayName', 'F - Ty');
|
|
plot(rz.f, sqrt(rz.psd_f), 'DisplayName', 'F - Rz');
|
|
hold off;
|
|
set(gca, 'xscale', 'log'); set(gca, 'yscale', 'log');
|
|
xlabel('Frequency [Hz]'); ylabel('ASD of the disturbance force $\left[\frac{F}{\sqrt{Hz}}\right]$')
|
|
legend('Location', 'southwest');
|
|
xlim([2, 500]);
|
|
#+end_src
|
|
|
|
#+HEADER: :tangle no :exports results :results none :noweb yes
|
|
#+begin_src matlab :var filepath="figs/dist_force_psd.pdf" :var figsize="full-tall" :post pdf2svg(file=*this*, ext="png")
|
|
<<plt-matlab>>
|
|
#+end_src
|
|
|
|
#+NAME: fig:dist_force_psd
|
|
#+CAPTION: Amplitude Spectral Density of the disturbance force ([[./figs/dist_force_psd.png][png]], [[./figs/dist_force_psd.pdf][pdf]])
|
|
[[file:figs/dist_force_psd.png]]
|
|
|
|
* Noise Budget
|
|
:PROPERTIES:
|
|
:CUSTOM_ID: Noise-Budget
|
|
:END:
|
|
<<sec:noise_budget>>
|
|
|
|
Now, from the compute spectral density of the disturbance sources, we can compute the resulting relative motion of the Hexapod with respect to the granite using the model.
|
|
We should verify that this is coherent with the measurements.
|
|
|
|
#+begin_src matlab :exports none
|
|
% Power Spectral Density of the relative Displacement
|
|
psd_gm_d = gm.psd_gm.*abs(squeeze(freqresp(G('Vm', 'Dw')/s, gm.f, 'Hz'))).^2;
|
|
psd_ty_d = tyz.psd_f.*abs(squeeze(freqresp(G('Vm', 'Fty')/s, tyz.f, 'Hz'))).^2;
|
|
psd_rz_d = rz.psd_f.*abs(squeeze(freqresp(G('Vm', 'Frz')/s, rz.f, 'Hz'))).^2;
|
|
#+end_src
|
|
|
|
#+begin_src matlab :exports none
|
|
figure;
|
|
hold on;
|
|
plot(gm.f, sqrt(psd_gm_d), 'DisplayName', 'Ground Motion');
|
|
plot(tyz.f, sqrt(psd_ty_d), 'DisplayName', 'Ty');
|
|
plot(rz.f, sqrt(psd_rz_d), 'DisplayName', 'Rz');
|
|
plot(rz.f, sqrt(psd_gm_d + psd_ty_d + psd_rz_d), 'k--', 'DisplayName', 'tot');
|
|
hold off;
|
|
set(gca, 'xscale', 'log'); set(gca, 'yscale', 'log');
|
|
xlabel('Frequency [Hz]'); ylabel('ASD of the relative motion $\left[\frac{m}{\sqrt{Hz}}\right]$')
|
|
legend('Location', 'southwest');
|
|
xlim([2, 500]);
|
|
#+end_src
|
|
|
|
#+HEADER: :tangle no :exports results :results none :noweb yes
|
|
#+begin_src matlab :var filepath="figs/psd_effect_dist_verif.pdf" :var figsize="full-tall" :post pdf2svg(file=*this*, ext="png")
|
|
<<plt-matlab>>
|
|
#+end_src
|
|
|
|
#+NAME: fig:psd_effect_dist_verif
|
|
#+CAPTION: Computed Effect of the disturbances on the relative displacement hexapod/granite ([[./figs/psd_effect_dist_verif.png][png]], [[./figs/psd_effect_dist_verif.pdf][pdf]])
|
|
[[file:figs/psd_effect_dist_verif.png]]
|
|
|
|
|
|
#+begin_src matlab :exports none
|
|
figure;
|
|
hold on;
|
|
plot(gm.f, flip(sqrt(-cumtrapz(flip(gm.f), flip(psd_gm_d)))), 'DisplayName', 'Ground Motion');
|
|
plot(gm.f, flip(sqrt(-cumtrapz(flip(gm.f), flip(psd_ty_d)))), 'DisplayName', 'Ty');
|
|
plot(gm.f, flip(sqrt(-cumtrapz(flip(gm.f), flip(psd_rz_d)))), 'DisplayName', 'Rz');
|
|
plot(gm.f, flip(sqrt(-cumtrapz(flip(gm.f), flip(psd_gm_d + psd_ty_d + psd_rz_d)))), 'k-', 'DisplayName', 'tot');
|
|
hold off;
|
|
set(gca, 'xscale', 'log'); set(gca, 'yscale', 'log');
|
|
xlabel('Frequency [Hz]'); ylabel('Cumulative Amplitude Spectrum [m]')
|
|
legend('location', 'northeast');
|
|
xlim([2, 500]); ylim([1e-11, 1e-6]);
|
|
#+end_src
|
|
|
|
#+HEADER: :tangle no :exports results :results none :noweb yes
|
|
#+begin_src matlab :var filepath="figs/cas_computed_relative_displacement.pdf" :var figsize="full-tall" :post pdf2svg(file=*this*, ext="png")
|
|
<<plt-matlab>>
|
|
#+end_src
|
|
|
|
#+NAME: fig:cas_computed_relative_displacement
|
|
#+CAPTION: CAS of the total Relative Displacement due to all considered sources of perturbation ([[./figs/cas_computed_relative_displacement.png][png]], [[./figs/cas_computed_relative_displacement.pdf][pdf]])
|
|
[[file:figs/cas_computed_relative_displacement.png]]
|
|
|
|
* Save
|
|
:PROPERTIES:
|
|
:CUSTOM_ID: Save
|
|
:END:
|
|
The PSD of the disturbance force are now saved for further analysis.
|
|
|
|
#+begin_src matlab
|
|
dist_f = struct();
|
|
|
|
dist_f.f = gm.f; % Frequency Vector [Hz]
|
|
|
|
dist_f.psd_gm = gm.psd_gm; % Power Spectral Density of the Ground Motion [m^2/Hz]
|
|
dist_f.psd_ty = tyz.psd_f; % Power Spectral Density of the force induced by the Ty stage in the Z direction [N^2/Hz]
|
|
dist_f.psd_rz = rz.psd_f; % Power Spectral Density of the force induced by the Rz stage in the Z direction [N^2/Hz]
|
|
|
|
save('./mat/dist_psd.mat', 'dist_f');
|
|
#+end_src
|
|
|
|
* Error motion of the Sample without Control
|
|
#+begin_src matlab
|
|
initializeGround();
|
|
initializeGranite('Foffset', false);
|
|
initializeTy('Foffset', false);
|
|
initializeRy('Foffset', false);
|
|
initializeRz('Foffset', false);
|
|
initializeMicroHexapod('Foffset', false);
|
|
initializeAxisc('type', 'rigid');
|
|
initializeMirror('type', 'rigid');
|
|
#+end_src
|
|
|
|
The nano-hexapod is a piezoelectric hexapod and the sample has a mass of 50kg.
|
|
#+begin_src matlab
|
|
initializeNanoHexapod('type', 'rigid');
|
|
initializeSample('type', 'rigid', 'mass', 50);
|
|
#+end_src
|
|
|
|
We set the references and disturbances to zero.
|
|
#+begin_src matlab
|
|
initializeReferences();
|
|
initializeDisturbances();
|
|
#+end_src
|
|
|
|
We set the controller type to Open-Loop.
|
|
#+begin_src matlab
|
|
initializeController('type', 'open-loop');
|
|
#+end_src
|
|
|
|
And we put some gravity.
|
|
#+begin_src matlab
|
|
initializeSimscapeConfiguration('gravity', false);
|
|
#+end_src
|
|
|
|
We do not need to log any signal.
|
|
#+begin_src matlab
|
|
initializeLoggingConfiguration('log', 'all');
|
|
#+end_src
|
|
|
|
#+begin_src matlab
|
|
initializePosError('error', false);
|
|
#+end_src
|
|
|
|
#+begin_src matlab
|
|
load('mat/conf_simulink.mat');
|
|
set_param(conf_simulink, 'StopTime', '1');
|
|
#+end_src
|
|
|
|
We simulate the model.
|
|
#+begin_src matlab
|
|
sim('nass_model');
|
|
#+end_src
|
|
|
|
#+begin_src matlab
|
|
figure;
|
|
subplot(1, 2, 1);
|
|
hold on;
|
|
plot(simout.Em.Eg.Time, simout.Em.Eg.Data(:, 1), 'DisplayName', 'X');
|
|
plot(simout.Em.Eg.Time, simout.Em.Eg.Data(:, 2), 'DisplayName', 'Y');
|
|
plot(simout.Em.Eg.Time, simout.Em.Eg.Data(:, 3), 'DisplayName', 'Z');
|
|
hold off;
|
|
xlabel('Time [s]');
|
|
ylabel('Position error [m]');
|
|
legend();
|
|
|
|
subplot(1, 2, 2);
|
|
hold on;
|
|
plot(simout.Em.Eg.Time, simout.Em.Eg.Data(:, 4));
|
|
plot(simout.Em.Eg.Time, simout.Em.Eg.Data(:, 5));
|
|
plot(simout.Em.Eg.Time, simout.Em.Eg.Data(:, 6));
|
|
hold off;
|
|
xlabel('Time [s]');
|
|
ylabel('Orientation error [rad]');
|
|
#+end_src
|
|
|
|
#+begin_src matlab
|
|
Eg = simout.Em.Eg;
|
|
save('./mat/motion_error_ol.mat', 'Eg');
|
|
#+end_src
|