Update figures to gain some space
@ -110,7 +110,7 @@ In order to design the NASS in a predictive way, a mechatronic approach, schemat
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#+name: fig:nass_mechatronics_approach
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#+attr_latex: :float multicolumn :width 0.9\linewidth
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#+caption: Overview of the mechatronic approach
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#+caption: Overview of the mechatronic approach used for the design of the NASS
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[[file:figs/nass_mechatronics_approach.pdf]]
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It consists of three main phases:
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@ -136,7 +136,7 @@ Indeed, several models are used throughout the design with increasing level of c
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\hfill
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\begin{subfigure}[t]{0.48\linewidth}
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\centering
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\includegraphics[width=0.89\linewidth]{figs/nass_simscape_3d.png}
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\includegraphics[width=0.89\linewidth]{figs/nass_simscape_3d.pdf}
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\caption{\label{fig:nass_simscape_3d} Multi Body Model}
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\end{subfigure}
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\hfill
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@ -180,12 +180,25 @@ Therefore, an alternative configuration with the encoders fixed to the plates wa
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** Nano-Hexapod Specifications
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The nano-hexapod should have a maximum height of $95\,mm$, support samples up to $50\,kg$ and have a stroke of $\approx 100\,\mu m$.
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Has shown in Fig.\nbsp{}ref:fig:nano_hexapod_elements, it only has few parts: two plates and 6 active struts in between.
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Each strut is composed of one flexible joint at each end, and one actuator in between (Fig.\nbsp{}ref:fig:picture_nano_hexapod_strut).
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Each strut is composed of one flexible joint at each end, and one actuator in between (Fig.\nbsp{}ref:fig:nano_heaxpod_strut_picture).
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#+name: fig:nano_hexapod_elements
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#+attr_latex: :float multicolumn :width 0.9\linewidth
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#+caption: CAD view of the nano-hexapod with key elements
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[[file:figs/nano_hexapod_elements.pdf]]
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#+begin_export latex
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\begin{figure*}[htbp]
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\begin{subfigure}[t]{0.80\linewidth}
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\centering
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\includegraphics[width=\linewidth]{figs/nano_hexapod_elements.pdf}
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\caption{\label{fig:nano_hexapod_elements} CAD view of the nano-hexapod with key elements}
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\end{subfigure}
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\hfill
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\begin{subfigure}[t]{0.19\linewidth}
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\centering
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\includegraphics[width=0.95\linewidth]{figs/nano_heaxpod_strut_picture.pdf}
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\caption{\label{fig:nano_heaxpod_strut_picture} Mounted strut}
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\end{subfigure}
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\caption{\label{fig:nano_hexapod}Nano-hexapod}
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\centering
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\end{figure*}
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#+end_export
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Based on the models used throughout the mechatronic approach, several specifications was obtained in order to maximize the performances of the system:
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- Actuator: axial stiffness $\approx \SI{2}{N/\um}$.
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@ -202,16 +215,11 @@ The top plate geometry was manually optimized to maximize its flexible modes.
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First flexible modes at around $\SI{700}{Hz}$ could be obtained.
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Amplified Piezoelectric Actuators (APA) were found to be the most suitable actuator for the nano-hexapod due to its compact size, large stroke and adequate stiffness.
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The chosen model was the APA300ML from Cedrat Technologies (shown in Fig.\nbsp{}ref:fig:picture_nano_hexapod_strut).
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The chosen model was the APA300ML from Cedrat Technologies (shown in Fig.\nbsp{}ref:fig:nano_heaxpod_strut_picture).
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It is composed of three piezoelectric stacks, a lever mechanism increasing the stroke up to $\approx \SI{300}{\um}$ and decreasing the axial stiffness down to $\approx \SI{1.8}{\um}$.
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One of the three stacks can be used as a force sensor, at the price of loosing $1/3$ of the stroke.
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This has the benefits providing good "collocation" between the sensor stack and the actuator stacks, meaning that the active damping controller will easily be made robust cite:souleille18_concep_activ_mount_space_applic.
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#+name: fig:picture_nano_hexapod_strut
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#+attr_latex: :width 0.9\linewidth
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#+caption: Picture of a nano-hexapod's strut
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[[file:figs/picture_nano_hexapod_strut.pdf]]
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** Nano-Hexapod Mounting
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A bench were developed to help the mounting of the struts such that the APA and the two flexible joints are well aligned.
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This helped reducing the effects of flexible modes of the APA.
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@ -223,7 +231,7 @@ The nano-hexapod fixed on top of the micro-station is shown in Fig.\nbsp{}ref:fi
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#+name: fig:nano_hexapod_picture
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#+attr_latex: :width 0.9\linewidth
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#+caption: Nano-hexapod on top of the ID31 micro-station
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[[file:figs/nano_hexapod_picture.jpg]]
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[[file:figs/nano_hexapod_picture.pdf]]
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* TEST-BENCHES
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** Flexible Joints and Instrumentation
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@ -1,4 +1,4 @@
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% Created 2021-07-15 jeu. 17:26
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% Created 2021-07-15 jeu. 21:33
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% Intended LaTeX compiler: pdflatex
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\documentclass[a4paper, keeplastbox, biblatex, boxit]{jacow}
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@ -72,7 +72,7 @@ In order to design the NASS in a predictive way, a mechatronic approach, schemat
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\begin{figure*}
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\centering
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\includegraphics[scale=1,width=0.9\linewidth]{figs/nass_mechatronics_approach.pdf}
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\caption{\label{fig:nass_mechatronics_approach}Overview of the mechatronic approach}
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\caption{\label{fig:nass_mechatronics_approach}Overview of the mechatronic approach used for the design of the NASS}
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\end{figure*}
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It consists of three main phases:
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@ -99,7 +99,7 @@ Indeed, several models are used throughout the design with increasing level of c
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\hfill
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\begin{subfigure}[t]{0.48\linewidth}
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\centering
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\includegraphics[width=0.89\linewidth]{figs/nass_simscape_3d.png}
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\includegraphics[width=0.89\linewidth]{figs/nass_simscape_3d.pdf}
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\caption{\label{fig:nass_simscape_3d} Multi Body Model}
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\end{subfigure}
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\hfill
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@ -142,12 +142,22 @@ Therefore, an alternative configuration with the encoders fixed to the plates wa
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\subsection{Nano-Hexapod Specifications}
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The nano-hexapod should have a maximum height of \(95\,mm\), support samples up to \(50\,kg\) and have a stroke of \(\approx 100\,\mu m\).
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Has shown in Fig.~\ref{fig:nano_hexapod_elements}, it only has few parts: two plates and 6 active struts in between.
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Each strut is composed of one flexible joint at each end, and one actuator in between (Fig.~\ref{fig:picture_nano_hexapod_strut}).
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Each strut is composed of one flexible joint at each end, and one actuator in between (Fig.~\ref{fig:nano_heaxpod_strut_picture}).
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\begin{figure*}
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\centering
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\includegraphics[scale=1,width=0.9\linewidth]{figs/nano_hexapod_elements.pdf}
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\caption{\label{fig:nano_hexapod_elements}CAD view of the nano-hexapod with key elements}
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\begin{figure*}[htbp]
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\begin{subfigure}[t]{0.80\linewidth}
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\centering
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\includegraphics[width=\linewidth]{figs/nano_hexapod_elements.pdf}
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\caption{\label{fig:nano_hexapod_elements} CAD view of the nano-hexapod with key elements}
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\end{subfigure}
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\hfill
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\begin{subfigure}[t]{0.19\linewidth}
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\centering
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\includegraphics[width=0.95\linewidth]{figs/nano_heaxpod_strut_picture.pdf}
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\caption{\label{fig:nano_heaxpod_strut_picture} Mounted strut}
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\end{subfigure}
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\caption{\label{fig:nano_hexapod}Nano-hexapod}
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\centering
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\end{figure*}
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Based on the models used throughout the mechatronic approach, several specifications was obtained in order to maximize the performances of the system:
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@ -167,17 +177,11 @@ The top plate geometry was manually optimized to maximize its flexible modes.
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First flexible modes at around \(\SI{700}{Hz}\) could be obtained.
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|
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Amplified Piezoelectric Actuators (APA) were found to be the most suitable actuator for the nano-hexapod due to its compact size, large stroke and adequate stiffness.
|
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The chosen model was the APA300ML from Cedrat Technologies (shown in Fig.~\ref{fig:picture_nano_hexapod_strut}).
|
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The chosen model was the APA300ML from Cedrat Technologies (shown in Fig.~\ref{fig:nano_heaxpod_strut_picture}).
|
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It is composed of three piezoelectric stacks, a lever mechanism increasing the stroke up to \(\approx \SI{300}{\um}\) and decreasing the axial stiffness down to \(\approx \SI{1.8}{\um}\).
|
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One of the three stacks can be used as a force sensor, at the price of loosing \(1/3\) of the stroke.
|
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This has the benefits providing good ``collocation'' between the sensor stack and the actuator stacks, meaning that the active damping controller will easily be made robust \cite{souleille18_concep_activ_mount_space_applic}.
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\begin{figure}[htbp]
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\centering
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\includegraphics[scale=1,width=0.9\linewidth]{figs/picture_nano_hexapod_strut.pdf}
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\caption{\label{fig:picture_nano_hexapod_strut}Picture of a nano-hexapod's strut}
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\end{figure}
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\subsection{Nano-Hexapod Mounting}
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A bench were developed to help the mounting of the struts such that the APA and the two flexible joints are well aligned.
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This helped reducing the effects of flexible modes of the APA.
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@ -188,7 +192,7 @@ The nano-hexapod fixed on top of the micro-station is shown in Fig.~\ref{fig:nan
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\begin{figure}[htbp]
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\centering
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\includegraphics[scale=1,width=0.9\linewidth]{figs/nano_hexapod_picture.jpg}
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\includegraphics[scale=1,width=0.9\linewidth]{figs/nano_hexapod_picture.pdf}
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\caption{\label{fig:nano_hexapod_picture}Nano-hexapod on top of the ID31 micro-station}
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\end{figure}
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paper/figs/nano_heaxpod_strut_picture.pdf
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paper/figs/nano_heaxpod_strut_picture.svg
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paper/figs/nano_hexapod_picture.svg
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paper/figs/nass_simscape_3d.pdf
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paper/figs/nass_simscape_3d.svg
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@ -45,7 +45,7 @@
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\node[myblock, fill=lightred, label={[mylabel] Implementation}, below = 2pt of testbenches] (implementation) {};
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% Text
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\node[anchor=south, above, text width=8cm, align=left] at (model.south) {Extensive use of models for:\begin{itemize}[noitemsep,topsep=5pt]\item Extraction of transfer functions \\ \item Choice of control architecture \\ \item Tuning of control laws \\ \item Closed loop simulations \\ \item Noise budgets / Evaluation of performances \\ \item Sensibility to parameters / disturbances\end{itemize}Helpful for proper and predictive design!};
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\node[anchor=south, above, text width=8cm, align=left] at (model.south) {Extensive use of models for:\begin{itemize}[noitemsep,topsep=5pt]\item Extraction of transfer functions \\ \item Choice of appropriate control architecture \\ \item Tuning of control laws \\ \item Closed loop simulations \\ \item Noise budgets / Evaluation of performances \\ \item Sensibility to parameters / disturbances\end{itemize}\centerline{Models are at the core the mecatronic approach!}};
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\node[mymodel] at (mustation.south) {Multiple stages \\ Complex dynamics};
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\node[mymodel] at (dist.south) {Ground motion \\ Position errors};
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@ -76,13 +76,13 @@
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\draw[<-] ($(instrumentation.south|-model.north)-(0.15, 0)$) -- node[left, midway]{{\small Model}} ($(instrumentation.south)-(0.15,0)$);
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\draw[->] ($(mounting.west-|model.east)+(0, 0.15)$) -- node[above, midway]{{\small Requirements}} ($(mounting.west)+(0, 0.15)$);
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\draw[<-] ($(mounting.west-|model.east)-(0, 0.15)$) -- node[below, midway]{{\small Refinement}} ($(mounting.west)-(0, 0.15)$);
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\draw[<-] ($(mounting.west-|model.east)-(0, 0.15)$) -- node[below, midway]{{\small Model refinement}} ($(mounting.west)-(0, 0.15)$);
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\draw[->] ($(testbenches.west-|model.east)+(0, 0.15)$) -- node[above, midway]{{\small Control Laws}} ($(testbenches.west)+(0, 0.15)$);
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\draw[<-] ($(testbenches.west-|model.east)-(0, 0.15)$) -- node[below, midway]{{\small Refinement}} ($(testbenches.west)-(0, 0.15)$);
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\draw[<-] ($(testbenches.west-|model.east)-(0, 0.15)$) -- node[below, midway]{{\small Model refinement}} ($(testbenches.west)-(0, 0.15)$);
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\draw[->] ($(implementation.west-|model.east)+(0, 0.15)$) -- node[above, midway]{{\small Control Laws}} ($(implementation.west)+(0, 0.15)$);
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\draw[<-] ($(implementation.west-|model.east)-(0, 0.15)$) -- node[below, midway]{{\small Refinement}} ($(implementation.west)-(0, 0.15)$);
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\draw[<-] ($(implementation.west-|model.east)-(0, 0.15)$) -- node[below, midway]{{\small Model refinement}} ($(implementation.west)-(0, 0.15)$);
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% Main steps
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\node[font=\bfseries, rotate=90, anchor=south, above] (conceptual_phase_node) at (dist.west) {1 - Conceptual Phase};
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