Design of control systems for missiles based on dynamic inversion and decentralized control

[1] Snell S A. Nonlinear inversion flight control for a superma- neuverable aircraft[J]. Journal of Guidance,Control and Dynamics,1992,15(4):976-984 [2] 李扬,陈万春. 高超声速飞行器BTT非线性控制器设计与仿真[J]. 北京航空航天大学学报,2006,32(3):249-253 Li Yang,Chen Wanchun. Design and simulation of BTT nonlinear controller for hypersonic vehicle[J]. Journal of Beijing University of Aeronautics and Astronautics,2006,32(3):249-253(in Chinese) [3] McFarland M B. Augmentation of gain-scheduled missile autopilot using adaptive neural networks. AIAA-98-4491,1998 [4] Lin C F,Yu T J,Ge J H,et al. Nonlinear H_∞ flight control system design for aircraft. AIAA-97-3697,1997 [5] Tornambe A. A decentralized controller for the robust stabilization of a class of MIMO dynamic systems[J]. Journal of Dynamic Systems,Measurement and Control,1994,116:293-304 [6] 陈金莉,李东海,孙先仿. 航天器姿态的非线性鲁棒分散控制器设计[J]. 宇航学报,2006, 27(1):6-11 Chen Jinli,Li Donghai,Sun Xianfang. Nonlinear robust decentralized controller design for spacecraft attitude control system[J]. Journal of Astronautics,2006,27(1):6-11(in Chinese) [7] 钱杏芳,林瑞雄,赵亚男.导弹飞行力学[M].北京:北京理工大学出版社,2006:2-80 Qian Xingfang, Lin Ruixiong, Zhao Yanan. Missile flight dynamics[M]. Beijing:Beijing Institute of Technology Press, 2006:2-80(in Chinese) [8] 吴天宝,黄显林,卢鸿谦,等. 基于非线性动态逆方法的TF/TA控制器设计[J]. 宇航学报,2004,25(3):289-294 Wu Tianbao,Huang Xianlin,Lu Hongqian,et al. Design of a TF/TA controller for cruise missile using nonlinear dynamic inversion[J]. Journal of Astronautics,2004,25(3):289-294(in Chinese) [9] Menon P K,Iragavarapu V R, Ohlmeyer E J. Nonlinear missile autopilot design using time-scale separation. AIAA-97-3765, 1997 [10] 张友安,胡云安. 导弹控制和制导的非线性设计方法[M]. 北京:国防工业出版社,2003:9-77 Zhang Youan,Hu Yunan. Nonlinear design approaches for missile control and guidance[M]. Beijing:National Defence Industry Press, 2003:9-77(in Chinese)