Autopilot Structured H∞ Synthesis for Satisfying Gain and Phase Margin Constraints

被引：0

作者：

Ma X. ^{[1
]}

Yan J. ^{[1
]}

Fu W. ^{[1
]}

Chen K. ^{[1
]}

机构：

[1] School of Astronautics, Northwestern Polytechnical University, Xi'an

来源：

Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University | 2019年 / 37卷 / 02期

关键词：

Acceleration tracking; Autopilot; Gain margin; Phase margin; Structured H[!sub]∞[!/sub] synthesis;

D O I：

10.1051/jnwpu/20193720211

中图分类号：

学科分类号：

摘要：

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. © 2019 Journal of Northwestern Polytechnical University.

引用

页码：211 / 217

页数：6

共 18 条

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