Design of mixed H2/J∞ robust flight control based on genetic algorithm and LMI

被引：0
|
作者：
Jian, Li [1 ]
Wei-guo, Zhang [1 ]
Guang-wen, Li [1 ]
机构：
[1] NW Polytech Univ, Dept Automat Control, Xian 710072, Shaanxi, Peoples R China
来源：
ISTM/2007: 7TH INTERNATIONAL SYMPOSIUM ON TEST AND MEASUREMENT, VOLS 1-7, CONFERENCE PROCEEDINGS | 2007年
关键词：
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 is concerned with the mixed H-2/H-infinity control problem in linear matrix inequality (LMI) regions. It is proposed that a hybrid approach based on Genetic Algorithm and LMI in order to find states feedback controller. This approach does not require that all specifications are enforced by a single closed-loop lyapunov function. The design of hybrid approach and digital simulation for lateral directional motion of a fighter aircraft are given. The simulation is shown that this method is very effective.
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收藏
页码：5229 / 5232
页数：4
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