REDUCED-ORDER H-INFINITY COMPENSATOR DESIGN FOR AN AIRCRAFT CONTROL PROBLEM

被引：7

作者：

OSBORNE, RC ^{[1
]}

ADAMS, RJ ^{[1
]}

HSU, CS ^{[1
]}

BANDA, SS ^{[1
]}

机构：

[1] WRIGHT LAB,FLIGHT DYNAM DIRECTORATE,WRIGHT PATTERSON AFB,OH 45433

来源：

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 1994年 / 17卷 / 02期

关键词：

D O I：

10.2514/3.21203

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

A recently introduced method for designing H(infinity) compensators based on minimal-order observers is considered for an aircraft control problem. The purpose of this paper is to bridge the gap between theory and application by presenting a practical utilization of a new design approach. Manual flight control systems for the lateral axis of a fighter aircraft are developed using both full-order and reduced-order compensators, and the results are compared. It is demonstrated that this method can be used to directly design reduced-order compensators that result in a system satisfying a closed-loop H. bound.

引用

页码：341 / 345

页数：5

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