Design of Mixed H2/J∞ Robust Flight Control based on Genetic Algorithm and LMI
This paper is concerned with the mixed 2 / H H∞ 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.
Li Jian Zhang Wei-guo Li Guang-wen
Department of Automatic Control, Northwestern Polytechnical University, Xian 710072, China
国际会议
北京
英文
2007-08-05（万方平台首次上网日期，不代表论文的发表时间）