[1] Lloyd R M. Conventional warhead systems physics and engineering design[M]. Virginia, US: AIAA, 1998: 209-225. [2] 夏国洪, 王东进. 智能导弹[M]. 北京: 中国宇航出版社, 2008: 254-257. XIA Guo-hong, WANG Dong-jin. Intelligent missile[M].Beijing: China Astronautic Publishing House, 2008: 254-257.(in Chinese) [3] 张志鸿, 周申生.防空导弹引信与战斗部配合效率和战斗部设计[M]. 北京: 中国宇航出版社, 1994: 89-104. ZHANG Zhi-hong, ZHOU Shen-sheng. Fuze warhead coordination efficiency and warhead design of air defense missile [M]. Beijing: China Astronautic Publishing House, 1994: 89-104.(in Chinese) [4] 刘斌,樊养余,周军伟, 等.基于成像导引/激光测距的起爆控制算法[J].探测与控制学报,2012, 34(2): 57-66. LIU Bin, FAN Yang-yu, ZHOU Jun-wei, et al. A burst control algorithm based on imaging guidance and laser ranging [J]. Journal of Detection & Control, 2012, 34(2): 57-66.(in Chinese) [5] 刘剑锋, 庄志洪. 利用导引头测角信息进行遭遇段剩余飞行时间估计的算法[J].兵工学报, 2006, 27(1): 27-31. LIU Jian-feng, ZHUANG Zhi-hong. The algorithm of time-to-go using angle information provided by seeker during missile-target encounter[J]. Acta Armamentarii, 2006, 27(1): 27-31.(in Chinese) [6] ZHUANG Zhi-zhong, TU Jian-ping, WANG Hong-bo. Prediction of time to go during missile-target encounter[J]. Journal of Astronautics, 2002, 23(5):32-38. [7] 张志鸿. 防空导弹引信与导引头一体化设计[J].现代防御技术,1993(2): 15-20. ZHANG Zhi-hong.Guidance integrated fusing design of anti-aircraft[J].Modern Defense Technology, 1993(2):15-20.(in Chinese) |