📄 fig11_28.m
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% Chapter 11: Figure 11.28, p. 670%% Satellite controllability with a tangential thruster only % (i.e. failed radial 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];b2=[0;0;0;1];Pc=ctrb(A,b2);n=det(Pc); if abs(n) < eps disp('Satellite is uncontrollable with tangential thruster only!')else disp('Satellite is controllable with tangential thruster only!')end
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