The speed control system of Figure DP4.1 is altered so that G(s) = l/(s + 5) and
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(a) Determine the range of K1 allowable so that the steady state is ess ¤ 1%.
(b) Determine a suitable value for K1 and K so that the magnitude of the steady-state error to a wind disturbance Td(t) = 2t mrad/s, 0 ¤ t Figure DP4.3
Speed control system.
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