Matlab or Octave Script for this problem.: Difference between revisions
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(New page: % This octave/Matlab script demonstrates the state space model of the J=0.01; b=0.1; K=0.01; R=1; L=0.5; A1=[[0,1,0];[0,-b/J,K/J];[0,-K/L,-R/L]]; B1=[0,0,1/L]'; C1=[0,1,0]; % The outp...) |
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Revision as of 12:20, 10 March 2010
% This octave/Matlab script demonstrates the state space model of the
J=0.01; b=0.1;
K=0.01; R=1; L=0.5; A1=[[0,1,0];[0,-b/J,K/J];[0,-K/L,-R/L]]; B1=[0,0,1/L]'; C1=[0,1,0]; % The output is the angular velocity omega. sys1=ss(A1,B1,C1); % Note that theta cannot be controlled. % So we use only the theta dot, and i_a as state variables. A2=[[-b/J, K/J];[-K/L,-R/L]]; B2=[0,1/L]'; C2=[1,0]; sys2=ss(A2,B2,C2); figure(1) clf;