727 lines
21 KiB
TeX
727 lines
21 KiB
TeX
% Created 2023-01-31 Tue 23:33
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% Intended LaTeX compiler: pdflatex
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\documentclass[a4paper, twoside, 11pt, onecolumn, bibliography=totoc, openright, appendixprefix=true]{scrreprt}
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\input{config.tex}
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\newacronym{mimo}{MIMO}{Multiple-Inputs Multiple-Outputs}
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\newacronym{siso}{SISO}{Single-Input Single-Output}
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\newacronym{nass}{NASS}{Nano Active Stabilization System}
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\newacronym{lti}{LTI}{Linear Time Invariant}
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\newglossaryentry{ka}{name=\ensuremath{k_a},description={{Actuator Stiffness in}}}
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\newglossaryentry{phi}{name=\ensuremath{\phi},description={{A woody bush}}}
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\input{config_extra.tex}
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\addbibresource{ref.bib}
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\author{Dehaeze Thomas}
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\date{2023-01-31}
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\title{Mechatronic approach for the design of a Nano Active Stabilization System}
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\subtitle{PhD Thesis}
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\hypersetup{
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pdfauthor={Dehaeze Thomas},
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pdftitle={Mechatronic approach for the design of a Nano Active Stabilization System},
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pdfkeywords={},
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pdfsubject={},
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pdfcreator={Emacs 28.2 (Org mode 9.5.2)},
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pdflang={English}}
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\usepackage{biblatex}
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\begin{document}
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\begin{titlepage}
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\vspace*{5cm}
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\makeatletter
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\begin{center}
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\begin{Huge}
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\@title
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\end{Huge}\\[0.1cm]
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%
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\begin{Large}
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\@subtitle
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\end{Large}\\
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%
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\emph{by}\\
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\@author
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%
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\vfill
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A thesis submitted in partial fulfillment of the requirements for the degree of Doctor of Philosophy (PhD) in Engineering Science\\
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at\\
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\textsc{Liège Université}
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\end{center}
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\makeatother
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\end{titlepage}
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\newpage
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\null
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\thispagestyle{empty}
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\newpage
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\chapter*{Abstract}
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\chapter*{Résumé}
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\chapter*{Acknowledgments}
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\dominitoc
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\tableofcontents
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\listoftables
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\listoffigures
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\chapter{Introduction}
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\section{Context of this thesis / Background and Motivation}
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\begin{itemize}
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\item ESRF (Figure \ref{fig:esrf_picture})
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\end{itemize}
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\begin{figure}[htbp]
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\centering
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\includegraphics[scale=1,width=0.7\linewidth]{figs/esrf_picture.jpg}
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\caption{\label{fig:esrf_picture}European Synchrotron Radiation Facility}
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\end{figure}
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\begin{itemize}
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\item ID31 and Micro Station (Figure \ref{fig:id31_microstation_picture})
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\end{itemize}
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\begin{figure}[htbp]
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\centering
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\includegraphics[scale=1,width=0.49\linewidth]{figs/id31_microstation_picture.png}
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\caption{\label{fig:id31_microstation_picture}Picture of the ID31 Micro-Station with annotations}
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\end{figure}
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Alternative: \texttt{id31\_microstation\_cad\_view.png} (CAD view)
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\begin{itemize}
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\item X-ray beam + detectors + sample stage (Figure \ref{fig:id31_beamline_schematic})
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\end{itemize}
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\begin{figure}[htbp]
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\centering
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\includegraphics[scale=1,width=0.49\linewidth]{figs/id31_beamline_schematic.png}
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\caption{\label{fig:id31_beamline_schematic}ID31 Beamline Schematic. With light source, nano-focusing optics, sample stage and detector.}
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\end{figure}
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\begin{itemize}
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\item Few words about science made on ID31 and why nano-meter accuracy is required
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\item Typical experiments (tomography, \ldots{}), various samples (up to 50kg)
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\item Example of picture obtained (Figure \ref{fig:id31_tomography_result})
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\end{itemize}
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\begin{figure}[htbp]
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\centering
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\includegraphics[scale=1,width=0.49\linewidth]{example-image-c.png}
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\caption{\label{fig:id31_tomography_result}Image obtained on the ID31 beamline}
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\end{figure}
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\begin{itemize}
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\item Explain wanted positioning accuracy and why micro-station cannot have this accuracy (backlash, play, thermal expansion, \ldots{})
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\end{itemize}
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\section{Challenge definition}
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\begin{figure}[htbp]
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\centering
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\includegraphics[scale=1]{figs/nass_concept_schematic.png}
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\caption{\label{fig:nass_concept_schematic}Nass Concept. 1: micro-station, 2: nano-hexapod, 3: sample, 4: 5DoF metrology}
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\end{figure}
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\begin{itemize}
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\item 6DoF vibration control platform on top of a complex positioning platform
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\item \textbf{Goal}: Improve accuracy of 6DoF long stroke position platform
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\item \textbf{Approach}: Mechatronic approach / model based / predictive
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\item \textbf{Control}: Robust control approach / various payloads.
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First hexapod with control bandwidth higher than the suspension modes that accepts various payloads?
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\item Rotation aspect
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\item Compactness? (more related to mechanical design)
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\end{itemize}
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\section{Literature Review}
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\begin{figure}
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\begin{subfigure}{0.49\textwidth}
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\begin{center}
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\includegraphics[scale=1,width=0.8\linewidth]{example-image-a.png}
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\end{center}
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\subcaption{Stewart platform based on voice coil actuators}
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\end{subfigure}
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\begin{subfigure}{0.49\textwidth}
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\begin{center}
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\includegraphics[scale=1,width=0.8\linewidth]{example-image-b.png}
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\end{center}
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\subcaption{Stewart platform based on piezoelectric actuators}
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\end{subfigure}
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\caption{\label{fig:stewart_platform_examples}Examples of Stewart Platforms}
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\end{figure}
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\begin{itemize}
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\item Hexapods
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\cite{li01_simul_fault_vibrat_isolat_point}
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\cite{bishop02_devel_precis_point_contr_vibrat}
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\cite{hanieh03_activ_stewar}
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\cite{afzali-far16_vibrat_dynam_isotr_hexap_analy_studies}
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\cite{naves20_desig}
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\item Positioning stations
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\item Mechatronic approach?
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\cite{rankers98_machin}
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\cite{monkhorst04_dynam_error_budget}
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\cite{jabben07_mechat}
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\end{itemize}
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\section{Outline of thesis / Thesis Summary / Thesis Contributions}
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\textbf{Mechatronic Design Approach} / \textbf{Model Based Design}:
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\begin{itemize}
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\item \cite{monkhorst04_dynam_error_budget} high costs of the design process: the designed system must be \textbf{first time right}.
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When the system is finally build, its performance level should satisfy the specifications.
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No significant changes are allowed in the post design phase.
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Because of this, the designer wants to be able to predict the performance of the system a-priori and gain insight in the performance limiting factors of the system.
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\end{itemize}
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\begin{figure}[htbp]
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\centering
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\includegraphics[scale=1,width=\linewidth]{figs/nass_mechatronics_approach.png}
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\caption{\label{fig:nass_mechatronics_approach}Overview of the mechatronic approach used for the Nano-Active-Stabilization-System}
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\end{figure}
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\chapter{Conceptual Design Development}
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\minitoc
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\paragraph{Abstract}
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Schematic that summarizes this phase.
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Uniaxial => Rotation => Multi body => Simulations
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\section{Constrains on the system}
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\begin{itemize}
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\item Size
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\item Payload
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\item Connections to samples
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\item \ldots{} should justify the nano-hexapod design
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\begin{itemize}
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\item choice of parallel architecture
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\end{itemize}
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\item[{$\square$}] Picture/schematic of the micro-station with indicated location of Nano-Hexapod
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\end{itemize}
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\section{Uni-axial Model}
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\begin{itemize}
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\item Explain what we want to capture with this model
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\item Schematic of the uniaxial model (with X-ray)
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\item Identification of disturbances (ground motion, stage vibrations)
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\item Optimal nano-hexapod stiffness/actuator: Voice coil VS Piezo (conclusion?)
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\item Control architecture (IFF, DVF, \ldots{})?
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\item Conclusion
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\end{itemize}
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\begin{figure}[htbp]
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\centering
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\includegraphics[scale=1]{figs/mass_spring_damper_nass.png}
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\caption{\label{fig:mass_spring_damper_nass}3-DoF uniaxial mass-spring-damper model of the NASS}
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\end{figure}
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\subsection{Noise Budgeting}
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\begin{figure}[htbp]
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\centering
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\includegraphics[scale=1,width=0.4\linewidth]{measurement_microstation_vibration_picture.jpg}
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\caption{\label{fig:measurement_microstation_vibration_picture}Setup used to measure the micro-station vibrations during operation}
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\end{figure}
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\begin{figure}[htbp]
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\centering
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\includegraphics[scale=1,width=0.49\linewidth]{example-image-b.png}
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\caption{\label{fig:asd_ground_motion_ustation_dist}Amplitude Spectral density of the measured disturbance sources}
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\end{figure}
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\subsection{Effect of support compliance}
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\href{file:///home/thomas/Cloud/work-projects/ID31-NASS/matlab/nass-simscape/org/uncertainty\_support.org}{study}
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\begin{itemize}
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\item \textbf{goal}: make the nano-hexapod independent of the support compliance
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\item Simple 2DoF model
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\item Generalized to any support compliance
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\item \textbf{conclusion}: frequency of nano-hexapod resonances should be lower than first suspension mode of the support
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\end{itemize}
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\subsection{Effect of payload dynamics}
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\href{file:///home/thomas/Cloud/work-projects/ID31-NASS/matlab/nass-simscape/org/uncertainty\_payload.org}{study}
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\begin{itemize}
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\item \textbf{goal}: be robust to a change of payload
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\item Simple 2DoF model
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\item Generalized to any payload dynamics
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\end{itemize}
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\subsection{Active Damping}
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Conclusion: IFF is better for this application
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\paragraph{Integral Force Feedback}
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\begin{itemize}
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\item Mass spring damper model
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\item Root Locus
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\item Sensitivity to disturbances
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\end{itemize}
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\paragraph{Direct Velocity Feedback}
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\begin{itemize}
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\item Mass spring damper model
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\item Root Locus
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\item Sensitivity to disturbances
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\end{itemize}
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\section{Effect of rotation}
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\cite{dehaeze20_activ_dampin_rotat_platf_integ_force_feedb,dehaeze21_activ_dampin_rotat_platf_using}
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\subsection{X-Y rotating platform model}
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\begin{itemize}
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\item x-y-Rz model
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\item explain why this is representing the NASS
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\item Equation of motion
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\item Centrifugal forces, Coriolis
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\end{itemize}
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\begin{figure}[htbp]
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\centering
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\includegraphics[scale=1]{figs/2dof_rotating_system.png}
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\caption{\label{fig:2dof_rotating_system}Mass spring damper model of an X-Y stage on top of a rotating stage}
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\end{figure}
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\subsection{Effect of rotational velocity on the system dynamics}
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\begin{itemize}
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\item Campbell diagram
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\end{itemize}
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\subsection{Decentralized Integral Force Feedback}
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\begin{itemize}
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\item Control diagram
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\item Root Locus: unstable with pure IFF
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\end{itemize}
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\subsection{Two proposed modification of IFF}
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\begin{itemize}
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\item Comparison of parallel stiffness and change of controller
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\item Transmissibility
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\end{itemize}
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\subsection{Conclusion}
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\begin{itemize}
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\item problem with voice coil actuator
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\item Two solutions: add parallel stiffness, or change controller
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\item Conclusion: minimum stiffness is required
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\item APA is a nice architecture for parallel stiffness + integrated force sensor (have to speak about IFF before that)
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\end{itemize}
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\section{Multi Body Model - Nano Hexapod}
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\begin{itemize}
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\item What we want to capture with this model
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\item Explain what is a multi body model (rigid body, springs, etc\ldots{})
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\item Key elements (plates, joints, struts): for now simplistic model (rigid body elements, perfect joints, \ldots{}), but in next section, FEM will be used
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\item Matlab/Simulink developed toolbox for the study of Stewart platforms
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\end{itemize}
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\subsection{Stewart Platform Architecture}
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\begin{itemize}
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\item Little review
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\item explain key elements:
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\begin{itemize}
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\item two plates
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\item joints
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\item actuators
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\end{itemize}
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\item explain advantages compared to serial architecture
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\end{itemize}
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\subsection{Kinematics}
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\begin{itemize}
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\item Well define elements, frames, \ldots{}
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\item Derivation of jacobian matrices: for forces and for displacement
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\item Explain this is true for small displacements (show how small)
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\end{itemize}
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\subsection{Model of an Amplified Piezoelectric Actuator}
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\begin{itemize}
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\item APA test bench
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\item Piezoelectric effects
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\item mass spring damper representation (2dof)
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\item Compare the model and the experiment
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\end{itemize}
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\subsection{Dynamics}
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\begin{itemize}
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\item Effect of joints stiffnesses
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\end{itemize}
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\begin{figure}[htbp]
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\centering
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\includegraphics[scale=1,width=\linewidth]{figs/simscape_nano_hexapod.png}
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\caption{\label{fig:simscape_nano_hexapod}3D view of the multi-body model of the Nano-Hexapod (simplified)}
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\end{figure}
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\section{Multi Body Model - Micro Station}
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\begin{figure}[htbp]
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\centering
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\includegraphics[scale=1,width=0.7\linewidth]{figs/simscape_first_model_screenshot.jpg}
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\caption{\label{fig:simscape_first_model_screenshot}3D view of the multi-body model of the micro-station}
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\end{figure}
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\subsection{Kinematics}
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\begin{itemize}
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\item Small overview of each stage and associated stiffnesses / inertia
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\item schematic that shows to considered DoF
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\item import from CAD
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\end{itemize}
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\subsection{Modal Analysis}
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\href{file:///home/thomas/Cloud/work-projects/ID31-NASS/matlab/nass-measurements/modal-analysis/index.org}{study}
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\begin{itemize}
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\item Picture of the experimental setup
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\item Location of accelerometers
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\item Show obtained modes
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\item Validation of rigid body assumption
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\item Explain how this helps tuning the multi-body model
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\end{itemize}
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\subsection{Validation of the Model}
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\begin{itemize}
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\item Most important metric: support compliance
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\item Compare model and measurement
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\end{itemize}
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\section{Control Architecture}
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Discussion of:
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\begin{itemize}
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\item Transformation matrices / control architecture
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\item Control in the frame of struts or cartesian?
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\item Effect of rotation on IFF? => APA
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\item HAC-LAC
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\end{itemize}
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\subsection{High Authority Control - Low Authority Control (HAC-LAC)}
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\begin{itemize}
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\item general idea
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\item case for parallel manipulator: decentralized LAC + centralized HAC
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\end{itemize}
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\subsection{Decoupling Strategies for parallel manipulators}
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\href{file:///home/thomas/Cloud/research/matlab/decoupling-strategies/svd-control.org}{study}
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\begin{itemize}
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\item Jacobian matrices, CoK, CoM, \ldots{}
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\item Discussion of cubic architecture
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\item SVD, Modal, \ldots{}
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\end{itemize}
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\subsection{Decentralized Integral Force Feedback (LAC)}
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\begin{itemize}
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\item Root Locus
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\item Damping optimization
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\end{itemize}
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\subsection{Control Kinematics}
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\begin{itemize}
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\item Explain how the position error can be expressed in the frame of the nano-hexapod
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\item block diagram
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\item Explain how to go from external metrology to the frame of the nano-hexapod
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\end{itemize}
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\subsection{Decoupled Dynamics}
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\begin{itemize}
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\item Centralized HAC
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\item Control in the frame of the struts
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\item Effect of IFF
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\end{itemize}
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\subsection{Centralized Position Controller (HAC)}
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\begin{itemize}
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\item Decoupled plant
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\item Controller design
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\end{itemize}
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\section{Simulations - Concept Validation}
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\begin{itemize}
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\item Tomography experiment
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\item Open VS Closed loop results
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\item \textbf{Conclusion}: concept validation
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nano hexapod architecture with APA
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decentralized IFF + centralized HAC
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\end{itemize}
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\begin{figure}[htbp]
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\centering
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\includegraphics[scale=1,width=\linewidth]{figs/simscape_nass_final.png}
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\caption{\label{fig:simscape_nass_final}3D view of the multi-body model including the micro-station, the nano-hexapod and the associated metrology}
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\end{figure}
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\section{Conclusion}
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\chapter{Detailed Design}
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\minitoc
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\paragraph{Abstract}
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CAD view of the nano-hexapod with key components:
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\begin{itemize}
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\item plates
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\item flexible joints
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\item APA
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\item required instrumentation (ADC, DAC, Speedgoat, Amplifiers, Force Sensor instrumentation, \ldots{})
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\end{itemize}
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\section{Optimal Nano-Hexapod geometry}
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\begin{itemize}
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\item[{$\square$}] Geometry?
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\begin{itemize}
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\item[{$\square$}] Cubic architecture?
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\item[{$\square$}] Kinematics
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\item[{$\square$}] Trade-off for the strut orientation
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\end{itemize}
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\item[{$\square$}] Sensors required
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\end{itemize}
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\subsection{Optimal strut orientation}
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|
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\subsection{Cubic Architecture: a Special Case?}
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|
|
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\section{Including Flexible elements in the Multi-body model}
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Reduced order flexible bodies \cite{brumund21_multib_simul_reduc_order_flexib_bodies_fea}
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\begin{itemize}
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\item Used with APA, Flexible joints, Plates
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\end{itemize}
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|
|
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\subsection{Reduced order flexible bodies}
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|
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\begin{itemize}
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\item Quick explanation of the theory
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\item Implementation with Ansys (or Comsol) and Simscape
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\end{itemize}
|
|
|
|
\subsection{Numerical Validation}
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|
|
|
\begin{itemize}
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\item Numerical Validation Ansys VS Simscape (APA)
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\item Figure with 0 and 1kg mass
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\end{itemize}
|
|
|
|
\subsection{Experimental Validation}
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|
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\begin{itemize}
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\item Test bench
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\item Obtained transfer functions and comparison with Simscape model with reduced order flexible body
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\end{itemize}
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|
|
|
\section{Amplified Piezoelectric Actuator}
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\href{file:///home/thomas/Cloud/work-projects/ID31-NASS/matlab/test-bench-apa/index.org}{study 1}, \href{file:///home/thomas/Cloud/work-projects/ID31-NASS/matlab/test-bench-apa300ml/test-bench-apa300ml.org}{study 2}
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|
|
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\begin{figure}[htbp]
|
|
\centering
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|
\includegraphics[scale=1,width=0.49\linewidth]{example-image-a.png}
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\caption{\label{fig:apa_schmeatic}Schematical representation of an Amplified Piezoelectric Actuator}
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|
\end{figure}
|
|
|
|
\begin{itemize}
|
|
\item First tests with the APA95ML
|
|
\end{itemize}
|
|
|
|
\subsection{Model}
|
|
|
|
Piezoelectric equations
|
|
|
|
\begin{figure}[htbp]
|
|
\centering
|
|
\includegraphics[scale=1,width=0.49\linewidth]{example-image-a.png}
|
|
\caption{\label{fig:apa_schmeatic_2dof}Schematical representation of a 2DoF model of an Amplified Piezoelectric Actuator}
|
|
\end{figure}
|
|
|
|
\begin{figure}[htbp]
|
|
\centering
|
|
\includegraphics[scale=1,width=0.49\linewidth]{example-image-b.png}
|
|
\caption{\label{fig:apa_schmeatic_fem}Schematical representation of a FEM of an Amplified Piezoelectric Actuator}
|
|
\end{figure}
|
|
|
|
\begin{itemize}
|
|
\item FEM
|
|
\item Simscape model
|
|
\item (2 DoF, FEM, \ldots{})
|
|
\end{itemize}
|
|
|
|
\subsection{Experimental System Identification}
|
|
|
|
\begin{itemize}
|
|
\item Experimental validation (granite test bench)
|
|
\item Electrical parameters
|
|
\item Required instrumentation to read force sensor?
|
|
\item Add resistor to include high pass filtering: no risk of saturating the ADC
|
|
\item Estimation of piezoelectric parameters
|
|
\end{itemize}
|
|
|
|
\subsection{Validation with Simscape model}
|
|
|
|
\begin{itemize}
|
|
\item Tuned Simscape model
|
|
\item IFF results: OK
|
|
\end{itemize}
|
|
|
|
\section{Flexible Joints}
|
|
\subsection{Effect of flexible joint characteristics on obtained dynamics}
|
|
|
|
\begin{itemize}
|
|
\item Based on Simscape model
|
|
\item Effect of axial stiffness, bending stiffness, \ldots{}
|
|
\item Obtained specifications (trade-off)
|
|
\end{itemize}
|
|
|
|
\subsection{Flexible joint geometry optimization}
|
|
|
|
\begin{itemize}
|
|
\item Chosen geometry
|
|
\item Optimisation with Ansys
|
|
\item Validation with Simscape model
|
|
\end{itemize}
|
|
|
|
\subsection{Experimental identification}
|
|
|
|
\begin{itemize}
|
|
\item Experimental validation, characterisation (\href{file:///home/thomas/Cloud/work-projects/ID31-NASS/matlab/test-bench-flexible-joints-adv/bending.org}{study})
|
|
\item Visual inspection
|
|
\item Test bench
|
|
\item Obtained results
|
|
\end{itemize}
|
|
|
|
\section{Instrumentation}
|
|
\subsection{DAC}
|
|
|
|
|
|
\subsection{ADC}
|
|
|
|
Force sensor
|
|
|
|
\subsection{Voltage amplifier (\href{https://research.tdehaeze.xyz/test-bench-pd200/}{link})}
|
|
|
|
\begin{itemize}
|
|
\item Test Bench: capacitive load, ADC, DAC, Instrumentation amplifier
|
|
\item Noise measurement
|
|
\item Transfer function measurement
|
|
\end{itemize}
|
|
|
|
\subsection{Encoder (\href{https://research.tdehaeze.xyz/test-bench-vionic/}{link})}
|
|
\begin{itemize}
|
|
\item Noise measurement
|
|
\end{itemize}
|
|
|
|
\section{Obtained Mechanical Design}
|
|
|
|
\begin{itemize}
|
|
\item CAD view of the nano-hexapod
|
|
\item Chosen geometry, materials, ease of mounting, cabling, \ldots{}
|
|
\end{itemize}
|
|
|
|
\chapter{Experimental Validation}
|
|
\minitoc
|
|
\paragraph{Abstract}
|
|
|
|
Schematic representation of the experimental validation process.
|
|
\begin{itemize}
|
|
\item APA
|
|
\item Strut
|
|
\item Nano-hexapod on suspended table
|
|
\item Nano-hexapod with Spindle
|
|
\end{itemize}
|
|
|
|
\section{Amplified Piezoelectric Actuator (\href{https://research.tdehaeze.xyz/test-bench-apa300ml/}{link})}
|
|
|
|
APA alone:
|
|
\begin{itemize}
|
|
\item \textbf{Goal}: Tune model of APA
|
|
\item[{$\square$}] FRF and fit with FEM model
|
|
\item[{$\square$}] Show all six FRF and how close they are
|
|
\item[{$\square$}] IFF
|
|
\end{itemize}
|
|
|
|
\section{Struts}
|
|
|
|
Strut (APA + joints):
|
|
\begin{itemize}
|
|
\item[{$\square$}] FRF, tune model
|
|
\item[{$\square$}] Issue with encoder (comparison with axial motion)
|
|
\item[{$\square$}] IFF
|
|
\end{itemize}
|
|
|
|
\section{Nano-Hexapod}
|
|
|
|
Mounting
|
|
|
|
Test bench on top of soft table:
|
|
\begin{itemize}
|
|
\item \textbf{Goal}: Tune model of nano-hexapod, validation of dynamics
|
|
\item modal analysis soft table (first mode at xxx Hz => rigid body in Simscape)
|
|
\item FRF + comp model (multiple masses)
|
|
\item IFF and robustness to change of mass
|
|
\end{itemize}
|
|
|
|
\section{Rotating Nano-Hexapod}
|
|
|
|
\begin{itemize}
|
|
\item \textbf{Goal}: validation of control strategy with rotation
|
|
\item Interferometers to have more stroke
|
|
\end{itemize}
|
|
|
|
\begin{figure}[htbp]
|
|
\centering
|
|
\includegraphics[scale=1,width=0.49\linewidth]{example-image-a.png}
|
|
\caption{\label{fig:rot_nano_hexapod_bench_schematic}Schematic of the rotating nano-hexapod test bench}
|
|
\end{figure}
|
|
|
|
\section{ID31 Micro Station}
|
|
|
|
\begin{itemize}
|
|
\item \textbf{Goal}: full validation without the full metrology
|
|
\end{itemize}
|
|
|
|
\chapter{Conclusion and Future Work}
|
|
|
|
\appendix
|
|
|
|
\chapter{Stewart Platform - Kinematics}
|
|
\chapter{Comments on something}
|
|
\printbibliography[heading=bibintoc,title={Bibliography}]
|
|
|
|
\chapter*{List of Publications}
|
|
\begin{refsection}[ref.bib]
|
|
% List all papers even if not cited
|
|
\nocite{*}
|
|
% Sort by year
|
|
\newrefcontext[sorting=ynt]
|
|
% Articles
|
|
\printbibliography[keyword={publication},heading={subbibliography},title={Articles},env=mypubs,type={article}]
|
|
% Proceedings
|
|
\printbibliography[keyword={publication},heading={subbibliography},title={In Proceedings},env=mypubs,type={inproceedings}]
|
|
\end{refsection}
|
|
|
|
\printglossary[type=\acronymtype]
|
|
\printglossary
|
|
\end{document}
|