📄 fig11_27.m
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% Chapter 11: Figure 11.27, p. 670%% Satellite controllability with a radial thruster only % (i.e. failed tangential thruster).%w=0.0011;A=[0 1 0 0;3*w^2 0 0 2*w;0 0 0 1;0 -2*w 0 0];b1=[0;1;0;0];Pc=ctrb(A,b1);n=det(Pc); if abs(n) < eps disp('Satellite is uncontrollable with radial thruster only!')else disp('Satellite is controllable with radial thruster only!')end
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