A fault-tolerant flight controller design for actuator faults

被引：0
|
作者：
Yee, JS [1 ]
Wang, JL [1 ]
Jiang, B [1 ]
机构：
[1] Nanyang Technol Univ, Sch Elect & Elect Engn, Singapore 639798, Singapore
来源：
THIRD INTERNATIONAL CONFERENCE ON NONLINEAR PROBLEMS IN AVIATION AND AEROSPACE, VOLS 1 AND 2, PROCEEDINGS | 2002年
关键词：
fault-tolerant control; flight control; H-infinity design;
D O I：
暂无
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
This paper presents a fault-tolerant flight controller design for actuator faults. Its principle is to use a new actuator fault estimation module which on-line estimates the actuator faults. The actuator faults are modeled in multiplicative form which is equal to one in the fault-free case and equal to actuator effectiveness when a fault occurs in the system. Output of the standard H-infinity flight controller is then re-configured to compensate the fault effect in the system. Performance of this method is tested in simulation on an F4-E aircraft to track a C* step command. Simulation results demonstrate good performance using the proposed design scheme.
引用
收藏
页码：723 / 730
页数：8
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