Passive Fault-Tolerant Flight Controller Design against Actuator Outages

被引：0

作者：

Yu, Xiang ^{[1
]}

Zhang, Youmin ^{[1
]}

机构：

[1] Concordia Univ, Dept Mech & Ind Engn, Montreal, PQ H3G 1M8, Canada

来源：

2014 IEEE CHINESE GUIDANCE, NAVIGATION AND CONTROL CONFERENCE (CGNCC) | 2014年

关键词：

CONTROL-SYSTEM DESIGN; RELIABLE CONTROL;

D O I：

暂无

中图分类号：

TM [电工技术]; TN [电子技术、通信技术];

学科分类号：

0808 ; 0809 ;

摘要：

A model to represent multiple actuator failure cases is developed by polytopic concept. The design of passive fault-tolerant control (FTC) with considerations of both normal and actuator failure cases is investigated, depending on the availability of actuator redundancies. By introducing the parameter dependent Lyapunov and slack methods, an improved algorithm to minimize the peak-to-peak gain of the closed-loop system is proposed. Numerical simulation studies subject to all elevon outages are conducted to illustrate the effectiveness of the designed approach to passive FTC.

引用

页码：1276 / 1281

页数：6

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