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% -*-latex-*- Put EMACS into LaTeX-mode % Verbal description for system NonlinearMSD (NonlinearMSD_desc.tex) % Generated by MTT on Thu Mar 7 14:48:47 GMT 2002. % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% % %% Version control history % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% % %% $Id$ % %% $Log$ % %% Revision 1.1 2000/12/28 09:13:38 peterg % %% Initial revision % %% % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% This example illustrates the use of \textbf{MTT} to \emph{linaerise} a nonlinear system -- a non-linear mass-spring-damper system called \textbf{NonlinearMSD}. The model is considered in Section \ref{sec:model} and linearisation in Section \Ref{sec:linearisation}. Further work is suggested in Section \Ref{sec:further}. \subsection{Bond Graph model}\label{sec:model} The schematic diagram of the system \textbf{NonlinearMSD} is displayed in Figure \ref{fig:NonlinearMSD_abg.ps}. The system comprises \begin{itemize} \item a rigid foundation, \item a rod of length $L$ hinged at the left-hand end and \item a linear spring of stiffness $k$ attached to the rigid foundation a distance $L$ from the hinge and to the free end of the rod. \end{itemize} The spring is unstretched when the rod makes an angle $\theta = \alpa = \frac{pi}{3}$ with the foundation. Using elementary geometry, the effectice angular spring generates a torque $\tau$ given by (\ref{eq:spring}) \begin{equation}\label{eq:spring} \tau = -2kl^2 \cos{\frac{\theta}{2}} (\sin{\frac{\theta}{2}}-\sin{\frac{\alpha}{2}}) \end{equation} The acausal bond graph of system \textbf{NonlinearMSD} is also displayed in Figure \Ref{fig:NonlinearMSD_abg.ps}. This shows the three bond graph components representing the friction \textbf{R}, the inertia \textbf{I} and the spring \textbf{C} components. The non-linear spring characteristic is given explicitly\footnote{The additional 0*eta term has no effect - it merely introduced the variable $\eta$ -- the equilibrium angle -- into the model}. The (nonlinear) system ordinary differential equation is given by \textbf{MTT} in Section \Ref{sec:NonlinearMSD_ode.tex}. This is a special case of the general non-linear ordinary differential equation: \begin{equation} \label{eq:non-state} \begin{cases} \dot{x} = f(x,u)\\ y = g(x,u) \end{cases} \end{equation} \subsection{Linearisation} \label{sec:linearisation} The first step in linearisation is to determine a set of (constant) states $x_e$ and (constant) inputs $u_e$ so that the system is in equilibrium - that is \begin{equation} \label{eq:eqilibrium} \dot{x} = f(x_e,u_e) = 0 \end{equation} In this case, choosing an angle $\theta=\eta$ and an input: \begin{equation}\label{eq:u_e} u_e = -\tau = 2kl^2 \cos{\frac{\eta}{2}} (\sin{\frac{\eta}{2}}-\sin{\frac{\alpha}{2}}) \end{equation} together with zero velocity gives an equilibrium. With this choice The linearised system is given in terms of the $A$, $B$, $C$ and $D$ matrices appearing in the state equation: \begin{equation} \label{eq:state} \begin{cases} \dot{x} = Ax + Bu\\ y = Cx + Du \end{cases} \end{equation} \textbf{MTT} automatically generates these matrices -- see Section \Ref{sec:NonlinearMSD_sm.tex}. \subsection{Further work} \label{sec:further} \begin{enumerate} \item Derive the system ordinary differential equation appearing in Section \Ref{sec:NonlinearMSD_ode.tex}. \item Explain how the input of (\ref{eq:u_e}) gives equilibrium for all $\eta$. \item Explain how the elements of the $A$, $B$, $C$ and $D$ appearing Section \Ref{sec:NonlinearMSD_sm.tex} arise from the ordinary differential equation of Section \Ref{sec:NonlinearMSD_ode.tex} together with the input of (\ref{eq:u_e}). \item Setting up parameters, inputs and initial state as in Sections \Ref{sec:NonlinearMSD_numpar.tex}, \Ref{sec:NonlinearMSD_input.tex} and \Ref{sec:NonlinearMSD_state.tex}, perform simulations as in Section \Ref{sec:NonlinearMSD_state.tex} - the figure shows the angular \emph{velocity} $\dot{\theta}$. \item Repeat the simulation with different perturbations by modifying the file ``NonlinearMSD\_input.tex'' (see Section \Ref{sec:NonlinearMSD_input.tex}) \begin{enumerate} \item note that for smaller perturbations, the graphs are of similar shape (scaled by the perturbation input) \item note that for larger perturbations the graphs are quite different - this is a non-linear system. \end{enumerate} \item \label{item:1} Repeat the simulation with different equilibrium angles $\eta$ by modifying the file ``NonlinearMSD\_numpar.tex'' (see Section \Ref{sec:NonlinearMSD_numpar.tex}) appropriately. Note that when $\eta=\pi$, the linearised system is \emph{unstable}. \item The (2,1) element of the $A$ matrix in Section \Ref{sec:NonlinearMSD_sm.tex} is the \emph{linearised} stiffness $k_l$. Plot this against $\eta$ and explain the observation in item \ref{item:1}. \end{enumerate}