[1] Prasanna H M, Ghose D. Retro-proportional-navigation: a new guidance law for interception of high-speed targets[J]. Journal of Guidance, Control, and Dynamics, 2012,35(2):377-386. [2] 熊俊辉, 唐胜景,郭杰. 高超声速巡航飞行器防御方案探讨[J]. 飞航导弹, 2012(1): 13-15. XIONG Jun-hui, TANG Sheng-jing, GUO Jie. Discussion on defense methods of hypersonic cruise vehicle[J]. Winged Missiles Journal, 2012(1): 13-15. (in Chinese) [3] 肖增博, 雷虎民, 滕江川,等. 目标飞行器反拦截协同制导策略[J]. 兵工学报,2011,32(12):1486-1492. XIAO Zeng-bo, LEI Hu-min, TENG Jiang-chuan,et al. Cooperative guidance strategy in anti-interception for target aircrafts[J]. Acta Armamentarii, 2012,32(12):1486-1492. (in Chinese) [4] 周荻.寻的导弹新型导引规律[M].北京:国防工业出版社,2002. ZHOU Di. New guidance laws for homing missiles [M]. Beijing: National Defense Industry Press, 2002. (in Chinese) [5] Brierly S D, Longchamo R. Application of sliding mode control to air-air interception problem[C]. IEEE Transactions on Aerospace and Electronic System, 1990,26(2):306-324. [6] Zhou D, Mu C D, Xu W L. Adaptive sliding mode guidance of a homing missile[J]. Journal of Guidance, Control, and Dynamics, 1999, 22(4):589-594. [7] Zhou D, Mu C D, Xu W L. Fuzzy adaptive variable structure guidance for space interception[J]. Tsinghua Science and Technology, 1999,4(4): 1610-1614. [8] Moon J, Kim K, Kim Y. Design of missile guidance law via variable structure control[J]. Journal of Guidance, Control, and Dynamics, 2001, 24(4):659-664. [9] Shima T, Golan O M. Head pursuit guidance[J]. Jounal of Guidance, Control, and Dynamics, 2007, 30(5): 1437-1444. [10] Golan O M, Shima T. Head pursuit guidance for hypervelocity interception[C]∥AIAA Guidance, Navigation, and Control Conference and Exhibit. Providence, Rhode Island: AIAA, 2004: 16-19. [11] Golan O M, Shima T. Precursor interceptor guidance using the sliding mode approach[C]∥AIAA Guidance, Navigation, and Conference and Exhibit. San Francisco, California: AIAA, 2005: 15-18. [12] 郭建国, 周凤岐, 周军. 基于零脱靶量设计的变结构末制导律[J]. 宇航学报, 2005, 26(2):152-156. GUO Jian-guo, ZHOU Feng-qi, ZHOU Jun. Variable structure terminal guidance law based on zero miss-distance[J]. Journal of Astronautics, 2005,26(2):152-156. (in Chinese) [13] Lin C L, Chen Y Y. Design of fuzzy logic guidance law against high-speed target[J]. Journal of Guidance, Control, and Dynamics,2000,23(1):17-24. [14] 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. QIAN Xing-fang, LIN Rui-xiong, ZHAO Ya-nan. Flight dynamics of missiles [M].Beijing: Beijing Institute of Technology Press, 2006. (in Chinese) [15] 石辛民, 郝整清. 模糊控制及其MATLAB仿真[M]. 北京:清华大学出版社, 2008. SHI Xin-min, HAO Zheng-qing. Fuzzy control and MATLAB simulation[M]. Beijing: Tsinghua University Press, 2008. (in Chinese) |