Citation: | Jiang Huan, Zhou Hao, Chen Wanchun, et al. Trajectory optimization design for surface-to-air missile using multilayer approach[J]. Journal of Beijing University of Aeronautics and Astronautics, 2008, 34(02): 135-139. (in Chinese) |
[1] Imado F, Kuroda T. Optimal missile guidance system against Na hypersonic target . AIAA-92-4531, 1992 [2] Karsli G, Tekinalp O. Trajectory optimization of advanced launch system Proceedings of 2nd International Conference on Recent Advances in Space Technologies, 2005:374-378 [3] Taur D R. Midcourse trajectory optimization for a SAM against high-speed target . AIAA-2002-4514, 2002 [4] Phillips C A, Drake J C. Trajectory optimization for a SAM using a multi-tier approach . AIAA-94-4404, 1994 [5] Phillips C A, Drake J C. Trajectory optimization for a missile using a multitier approach [J]. Journal of Spacecraft and Rockets, 2000, 37(5): 653-662 [6] 陈宝林.最优化理论与算法[M].北京:清华大学出版社,1989 Chen Baolin. Optimal theory and algorithm [M]. Beijing: Tsinghua University Press, 1989 (in Chinese) [7] Zarchan P. Tactical and strategic missile guidance [M]. 3rd ed. Washington, DC: American Institute of Aeronautics and Astronautics Inc, 1998 [8] 赵善友,张望生,顾炳良,等.防空导弹武器寻的制导控制系统设计[M].北京:宇航出版社,1992 Zhao Shanyou, Zhang Wangsheng, Gu Bingliang, et al. Homing guidance and control system design for air defense missile [M]. Beijing: Astronautics Press, 1992(in Chinese) [9] 李廷杰.导弹武器系统的效能及其分析[M].北京:国防工业出版社,2000 Li Tingjie. Effectiveness analysis for missile weapon systems [M]. Beijing: National Defense Industry Press, 2000 (in Chinese) [10] В Г斯维特洛夫,И С戈卢别夫.防空导弹设计[M].北京:中国宇航出版社,2004 Светлов В Г, Голубев И С. Air defense missile design [M]. Beijing: Chinese Astronautics Press, 2004 (in Chinese)
|