满足增益相位裕度的自动驾驶仪结构化H_∞综合

Aiming at the static unstable Hypersonic vehicle, a method for designing H_∞ autopilot to satisfy gain margin and phase margin is proposed. Structured H_∞ synthesis is used to synthesize the autopilot under the fixed structure. The gain margin and phase margin were constrained by using H_∞ norm of the complementary of the scaled plant. The requirement for the gain margin and phase margin is represented by the distance between the open loop Nyquist curve and the circle that represents the gain margin and phase margin in the complex plane. The distance is adjusted by tuning the parameter of performance specifications automatically to reduce the conservatism of the controller. The present method is applicable to both static stable vehicle and static unstable vehicle, and a three loops acceleration tracking autopilot is design. The numerical simulations have demonstrated that the autopilot satisfys the performance specifications, gain margin and phase margin simultaneously.