A vertical takeoff (VTOL) aircraft is an inherently unstable vehicle and requires an automatic stabilization system. An
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The actuator and filter are represented by the transfer function
(a) Obtain the Bode diagram of the loop transfer function L(s) = Gc(s) Gis) H(s) when the gain is K] = 2. (b) Determine the gain and phase margins of this system, (c) Determine the steady-state error for a wind disturbance of Td(s) = l/s. (d) Determine the maximum amplitude of the resonant peak of the closed-loop frequency response and the frequency of the resonance, (e) Estimate the damping ratio of the system from MpÏ and the phase margin.
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