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
a
neutrally 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)=-1
and
\lambda _(2,3)=-2 -3i
. Is the closed-loop system stable PLEASE SHOW MATLAB CODES