Endoatmospheric interceptor fast response control using impulse attitude control motor

[1] 徐斌. "爱国者"系列地空导弹[J]. 地面防空武器,2004,3:19-24 Xu Bin. Patriot series surface-to-air missile[J]. Surface-to-Air Weapon, 2004, 3:19-24(in Chinese) [2] Chadwick W R. Augmentation of high-altitude maneuver performance of a tail-controlled missile using lateral thrust . ADA328973, 1995 [3] Schroeder W K. Fuzzy logic autopilot synthesis for a nonlinearly behaved thruster-controlled missile . USA:Aerospace Engineering, The University of Texas at Arlington, 1999 [4] 邹晖. 大气层内气动力/脉冲推力复合控制的自旋导弹研究 .北京:北京航空航天大学宇航学院,2004 Zou Hui. The research on an endoatmospheric spin missile blended with aerodynamic and lateral jets . Beijing:School of Astronautics, Beijing University of Aeronautics and Astronautics, 2004(in Chinese) [5] B.T.斯维特洛夫,N.C.戈卢别夫. 防空导弹设计[M]. 北京:中国宇航出版社,2004 Svetlov B T, Golubev N C. Surface-to-air missile design[M]. Beijing:China Astronautics Publishing House, 2004(in Chinese) [6] Zarchan P. Tactical and strategic missile guidance[M]. 3rd edition. USA:AIAA Inc, 1998:510-513