The dynamics of a rocket are represented by and state variable feedback is used, where = - x1 - 25x2 + r.. Determine the

The dynamics of a rocket are represented by

and state variable feedback is used, where µ = - x1 - 25x2 + r.. Determine the roots of the characteristic equation of this system and the response of the system when the initial conditions are x1(0) = 1 and x2(Q) = - 1. Assume the reference input r(t) - 0.

0 1