Fuzzy control law design of hypersonic vehicle based on genetic algorithm

[1] Heller M, Sachs G. Flight dynamics and robust control of a hypersonic test vehicle with ramjet propulsion . AIAA-98-1521, 1998 [2] Wu F S, Engelen H J C, Babuska R, et al. Intelligent flight controller design with fuzzy logic for an atmospheric re-entry vehicle . AIAA-2000-0174, 2000 [3] 冯勇,郑雪梅,鲍晟.多变量线性模型不确定系统终端滑模分解控制方法[J].控制理论与应用,2004,21(1):11-16 Feng Yong, Zheng Xuemei, Bao Sheng. Terminal sliding mode decomposed control of multivariable linear uncertain systems[J]. Control Theory and Applications, 2004, 21(1): 11-16(in Chinese) [4] Wang Qian, Stengel R. Robust nonlinear control of a hypersonic aircraft . AIAA-99-4000, 1999 [5] 刘燕斌,陆宇平.基于变结构理论的高超音速飞机纵向逆飞行控制[J].信息与控制,2006,35(3):388-392 Liu Yanbin, Lu Yuping. Longitudinal inversion flight control based on variable structure theory for hypersonic vehicle[J]. Information and Control,2006,35(3):388-392(in Chinese) [6] 李爱军,沈毅,章卫国.基于神经网络的动态逆方法研究[J].工业仪表与自动化装置,2002(6):7-10 Li Aijun, Shen Yi, Zhang Weiguo. A study on neural network-based dynamic inversion methods[J].Industrial Instrumentation and Automation, 2002(6):7-10(in Chinese) [7] Austin J K, Mechanical E B. Evolutionary design of robust flight control for a hypersonic aircraft .Brisbane,Australia: Department of Mechanical Engineering, University of Queensland, 2002