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834   MECHATRONICS
                              Frequency response related functions are illustrated in the example below.

                              num = [1] ;
                              den = [1     5   2    6];
                              sys = tf(num, den);

                              [mag, phase, w] = bode(sys) ; % Get Bode plot data
                              loglog(w, mag);                   % plot magnitude plot
                              semilogx(w, phase);               % plot phase plot

                              nyquist(sys) ;                    %   Plot Nyquist (polar) plot
                              [GM, PM, wgm, wpm] = margin(G) ; % Obtain Gain Margin, Phase
                                                                      margin
                                                                    % and the freqencies at those
                                                                      locations.

                              Given the A, B, C matrices of state-space representation, controllability and observability
                              matrices can be obtained as follows,

                              Wc = ctrb(A,B);     % Calcualate controllability matrix
                              Wo = obsv(A,C);     % ........... observability........

                              nc = rank(Wc) ;       % Get the rank of controllability matrix
                              value1 = det(Wc) ;     % ....... determinant of ..............
                              no = rank(Wo) ;      %  Same for observability matrices.
                              value2 = det(Wo) ;
                              Given the A, B, C, D matrices of state-space representation, and desired pole locations for
                              closed loop system p , the state feedback gain can be calculated by
                                               c
                              K = acker(A, B, p_c) ;
                              K = place(A, B, p_c) ;
                              For the observer design, given the observer poles, p ,
                                                                       e
                              L = (acker(A’, C’, p_e))’ ;
                              L = (place(A’, C’, p_e))’ ;

                                       ®
                              MATLAB Functions to Simulate Linear Dynamic Systems           MATLAB  ®
                              has three convenient functions to simulate linear dynamic systems. They are
                                1. impulse(sys,t) function for impulse response of the system for a given time duration,
                                2. step(sys,t) function for unit magnitude step function response,
                                3. lsim(sys,u,t) function to simulate the response to an arbitrary input function defined
                                   in vector “u.”
                                                      ®
                                   The example MATLAB script file below illustrates their use. Note that these func-
                              tions are usable only for dynamic systems defined by linear, constant coefficient differential
                              equations. Figure A.9 shows the results of the simulation.

                              % Simulating Linear Systems response using MATLAB® Functions
                              %   impulse()    and step() and lsim()
                              % Linear system definition:
                                wn=2∗pi∗1.0;
                                psi=0.5;
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