RESTRUCTURABLE CONTROL USING PROPORTIONAL-INTEGRAL IMPLICIT MODEL FOLLOWING

被引：87

作者：

HUANG, CY ^{[1
]}

STENGEL, RF ^{[1
]}

机构：

[1] PRINCETON UNIV,DEPT MECH & AEROSP ENGN,PRINCETON,NJ 08544

来源：

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 1990年 / 13卷 / 02期

关键词：

D O I：

10.2514/3.20550

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

Studies of a proportional-integral implicit model-following control law are presented. The research focuses on the ability of the control law to recover the performance of a system with failed actuators or structural damage to its prefailure level. Properties of the implicit model-following strategy are examined, and conditions for control reconfiguration are stated. The control law is applied to the lateral-directional model of a fighter aircraft, and control restructuring is shown for changes in control and system matrices. It is concluded that the implicit model-following scheme is a good candidate for control reconfiguration. © 1990 American Institute of Aeronautics and Astronautics, Inc., All rights reserved.

引用

页码：303 / 309

页数：7

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