Failure detection and adaptive compensation for fault tolerable flight control systems

被引:19
作者
Lin, Chun-Liang [1 ]
Liu, Chun-Te [2 ]
机构
[1] Natl Chung Hsing Univ, Dept Elect Engn, Taichung 402, Taiwan
[2] Feng Chia Univ, Inst Automat Control Engn, Taichung 40724, Taiwan
关键词
adaptive control; aircraft control; fault tolerance; neural network applications; real-time systems;
D O I
10.1109/TII.2007.913064
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 an advanced aircraft flight control system which is capable of providing failure detection, identification, and adaptive compensation in the event of the damage of control surfaces. The new approach is based on the detection of immediate changes of correlation between pitching, yawing, and rolling rates. The failure compensation mechanism is realized by an adaptive wavelet neural net-based proportional-integral-derivative (PID) controller. The fault-tolerant mechanism is activated to regain effective control of the damaged aircraft whenever a control surface failure is detected. Design of a real-time executive kernel based on the RT-Linux operating system is experimentally conducted to realize and verify functions of our proposed design.
引用
收藏
页码:322 / 331
页数:10
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