魏明英.直接侧向力与气动力复合控制技术综述\[J\]. 现代防御技术, 2012, 40(1): 52-55.?WEI Mingying. Summary of blended control technology for missiles with lateral jets and aerodynamic surfaces\[J\]. Modern Defence Technology, 2012, 40(1): 52-55. [2]程凤舟.拦截战术弹道导弹末段制导和复合控制研究\[D\].西安:西北工业大学, 2002: 7-8.CHENG Fengzhou. Studies of guidance and combined control in terminal phase when intercepting tactical ballistic missile\[D\]. Xi′an: Northwestern Polytechnical University, 2002: 7-8.? [3]RIDGELY D B,DRAKE D,TRIPLETT L.Dynamic control allocation of a missile with tails and reaction jets\[C\]// AIAA Guidance,Navigation,and Control Conference and Exhibit. Hilton Head,USA, 2007.? [4]SHTESSEL Y, TOURNES C, SHCOLNIKOV I. Guidance and autopilot for missiles steered by aerodynamic lift and divert thrusters using second order sliding modes\[C\]//AIAA Guidance, Navigation, and Control Conf. Keystone, USA, 2006.? [5]马克茂,赵辉,张德成. 导弹直接侧向力与气动力复合控制设计与实现\[J\].宇航学报, 2011, 32(2): 310-316.?MA Kemao, ZHAO Hui, ZHANG Decheng. Control design and implementation for missiles with blended lateral jets and aerodynamic control systems\[J\]. Journal of Astronautics, 2011, 32(2): 310-316.? [6]滕江川,吴晓燕,陈永兴. 基于模糊控制理论的脉冲推力器点火算法\[J\]. 四川大学学报:工程科学版, 2011, 43(1): 194-197.?TENG Jiangchuan, WU Xiaoyan, CHEN Yongxing. Fire algorithm of pluse thruster based on fuzzy control theory\[J\]. Journal of Sichuan University:Engineering Science Edition, 2011, 43(1): 194-197.? [7]周锐,王军.导弹气动力/直接力自适应控制分配及优化设计\[J\].航空学报, 2007, 28(1): 187-190.?ZHOU Rui, WANG Jun. Adaptive control allocation between aerodynamic fin and side thruster and controller design using multi-objective optimization\[J\]. Acta Aeronautica et Astronautic Sinica, 2007, 28(1): 187-190.? [8]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, 2002: 36-48. [9]李洪兴. 变论域自适应模糊控制器\[J\]. 中国科学(E辑), 1999, 29(1): 32-42.?LI Hongxing. Adaptive fuzzy controller based on variable universe\[J\].Science in China (Series E), 1999, 29(1): 32-42.? [10]斯维特洛夫 B T. 防空导弹设计\[M\]. 北京:中国宇航出版社, 2004: 349-354.? [11]WANG Xinhua, CHEN Zengqiang, YANG Geng. Finite time convergent differentiator based on singular perturbation technique\[J\].IEEE Transactions on Automatic Control, 2007, 52(9): 1731-1737.? [12]KROVEL T D. Optimal tuning of PWPF modulator for attitude control\[D\]. \[S.l.\] :Norwegian University of Science and Technology, 2005: 38-40.? [13]尹永鑫.气动力/直接力复合控制拦截弹制导与控制方法研究\[D\].哈尔滨:哈尔滨工业大学, 2008: 71?76.?YIN Yongxin. Research on guidance and control method of intercepter missile with aerodynamic and lateral thrust blended\[D\]. Harbin: Harbin Institute of Technology, 2008: 71-76.