[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) |