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An open loop control system has the following state space model.
A=[[0,1,0,0,2,-2,-2]]
-4
-4
-1
B=[[0]]
2
1(a) Use Matlab to find the eigenvalues of the open-loop system. Is it stable? Please note that
aneutrally stable system (even with its name) is not considered stable in aerospace engineering. (b) Use Matlab to find the controller gain to locate the closed-loop eigenvalues at
\lambda _(1)=-1and
\lambda _(2,3)=-2 -3i. Is the closed-loop system stable PLEASE SHOW MATLAB CODES