邹晖,陈万春,殷兴良.自旋导弹的反馈线化控制器设计[J].弹箭与制导学报,2004,24(1):228-234 Zou hui,Chen Wanchun,Yin Xingliang.A spin missile autopilot designed using feedback linearization[J].Journal of Projectiles,Rockets,Missiles and Guidance,2004,24(1):228-234(in Chinese)
[2]
周慧钟.有翼导弹飞行动力学[M].北京:航空专业教材编审组,1983:27-47 Zhou Huizhong.Aerodynamic missile flight dynamcis[M].Beijing:Compilation and Deliberation Group of Teaching Material for Aviation Specialities,1983:27-47(in Chinese)
[3]
Liu Fang,Chen Wanchun.Controller design for spinning missile with the actuator limit//Wu Fan.Advanced Materials Research Volumes.Switzerland:Trans Tech Publications,2012:45-51
[4]
Zarchan P.Tactical and strategic missile guidance[M].3rd ed.USA:American Institute of Aeronautics and Astronautics,1997:461-465
[5]
周慧钟.有翼导弹飞行动力学[M].北京:航空专业教材编审组,1983:27-47 Zhou Huizhong.Aerodynamic missile flight dynamcis[M].Beijing:Compilation and Deliberation Group of Teaching Material for Aviation Specialities,1983:27-47(in Chinese)
[6]
Schumacher C.Tactical missile autopilots:gain-scheduled H∝ control and dynamic inversion.Michigan:The University of Michigan,1997
[7]
Schumacher C J,Khargonekar P P,McClamroch N H.Stability analysis of dynamic inversion controllers using time-scale separation.AIAA-98-4322,1998
[8]
Schumacher C,Khargonekar P P.Stability analysis of a missile control system with a dynamic inversion controller[J].Journal of Guidance,Control,and Dynamics,1998,21(3):508-515
[9]
McFarland M B,Hoque S M.Robustness of a nonlinear missile autopilot designed using dynamic inversion.AIAA-2000-3970,2000
[10]
邹晖,陈万春,殷兴良.自旋导弹的反馈线化控制器设计[J].弹箭与制导学报,2004,24(1):228-234 Zou hui,Chen Wanchun,Yin Xingliang.A spin missile autopilot designed using feedback linearization[J].Journal of Projectiles,Rockets,Missiles and Guidance,2004,24(1):228-234(in Chinese)
[11]
Schumacher C.Tactical missile autopilots:gain-scheduled H∝ control and dynamic inversion.Michigan:The University of Michigan,1997
[12]
Liu Fang,Chen Wanchun.Controller design for spinning missile with the actuator limit//Wu Fan.Advanced Materials Research Volumes.Switzerland:Trans Tech Publications,2012:45-51
[13]
Schumacher C,Khargonekar P P.Stability analysis of a missile control system with a dynamic inversion controller[J].Journal of Guidance,Control,and Dynamics,1998,21(3):508-515
[14]
Zarchan P.Tactical and strategic missile guidance[M].3rd ed.USA:American Institute of Aeronautics and Astronautics,1997:461-465