The dynamics of a rocket are represented by ~0 0~ y = [0 l]x and state variable feedback
Chapter 0, Problem P11.10(choose chapter or problem)
The dynamics of a rocket are represented by ~0 0~ y = [0 l]x and state variable feedback is used, where a = IOJCI 25.v2 + i". Determine the roots of the characteristic equation of this system and the response of the system when the initial conditions are x}(0) = 1 and x2(Q) = -1 . Assume the reference input r(t) - 0.
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