Restructural controller design for a control-reconfigurable aircraft

被引：0
|
作者：
Li, Q [1 ]
机构：
[1] Tsing Hua Univ, Dept Automat, Beijing 100084, Peoples R China
来源：
PROCEEDINGS OF THE 5TH ASIA-PACIFIC CONFERENCE ON CONTROL & MEASUREMENT | 2002年
关键词：
flight control system; pseudo inverse; failure-tolerant systems; self-repairing systems; control mixer; aerodynamic redundancy;
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：
In today's aircraft, the hardware redundancy is driven by the critical surfaces resulting in single point-failures. Reconfiguration technology removes tile single surface criticality by employing control surfaces with aerodynamic redundancy. This paper studies a control reconfiguration scheme based on Control Mixer Concept. A technique for the design of a control mixer for an aircraft with damaged surfaces/actuators using the pseudo-inverse is developed and applied. This paper discusses its applications and limitations based on linear analysis and computer simulation.
引用
收藏
页码：77 / 81
页数：5
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