The dynamics of a rocket are represented by and state variable feedback is used, where =
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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.
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The system with feedback is given by where x 1 0 1 and x 2 0 1 The characteris...View the full answer
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