Citation: | Liu Hengjun, Jiang Huan, Chen Wanchunet al. Application of MDO algorithm to multi-tier trajectory optimization design for a surface-to-air missile kinetic kill[J]. Journal of Beijing University of Aeronautics and Astronautics, 2010, 36(2): 145-149. (in Chinese) |
[1] Phillips C A,Drake J C.Trajectory optimization for a SAM using a multi-tier approach .AIAA-94-4404,1994 [2] 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 [3] 姜欢,周浩,陈万春,等.多层次法防空导弹弹道优化设计[J].北京航空航天大学学报,2008,34(2):135-139 Jiang Huan,Zhou Hao,Chen Wanchun,et al.The research of trajectory optimization design for a surface-to-air missile using a multilayer approach[J].Journal of Beijing University of Aeronautics and Astronautics,2008,34(2):135-139 (in Chinese) [4] Sobieszczanki-Sobieski J.Sensitivity of complex,internally coupled systems[J].AIAA Journal,1990,28(1):153-160 [5] Grossman B,Gurdal Z,Stauch G J,et al.Integrated aerodynamic/structure design of a sailplane wing[J].Journal of Aircraft,1988,25(9):855-860 [6] Zarchan P.Tactical and strategic missile guidance[M].3rd Edition.Washington,DC:American Institute of Aeronautics and Astronautics Inc,1998 [7] 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) [8] 秦如雯.钨杆杀伤增强器动能拦截TBM杀伤概率计算与仿真研究 .北京:北京航空航天大学宇航学院,2003 Qin Ruwen.Calculation and simulation of hit-to-kill probability to TBM by LE terminal interception .Beijing:School of Astronautics,Beijing University of Aeronautics and Astronautics,2003 (in Chinese) [9] Lloyd R M.Conventional warhead systems physics and engineering design[M].Washington,DC:American Institute of Aeronautics and Astronautic Inc,1998
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