Multilayer trajectory optimization design for surface-to-air missile based on global sensitivity equation method

[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] 王振国,陈小前,罗文彩,等.飞行器多学科设计优化理论与应用研究[M].北京:国防工业出版社, 2006 Wang Zhenguo, Chen Xiaoqian, Luo Wencai, et al. Research on the theory and application of multidisciplinary design optimization of flight vehicles[M]. Beijing: National Defense Industry Press, 2006 (in Chinese) [4] Sobieszczanki-Sobieski J. Sensitivity of complex, internally coupled systems[J]. AIAA Journal, 1990, 28(1): 153-160 [5] 方卫国,郦正能. 基于全局敏度方程方法的飞机方案设计[J].航空学报, 1998, 19(3): 293-298 Fang Weiguo, Li Zhengneng. Aircraft scheme optimization design based on global sensitivity equation method[J].Acta Aeronautica et Astronautica Sinica, 1998, 19(3): 293-298 (in Chinese) [6] Zarchan P. Tactical and strategic missile guidance[M]. 3rd ed. Washington, DC: American Institute of Aeronautics and Astronautics Inc, 1998 [7] 斯维特洛夫В Г, 戈卢别夫И С.防空导弹设计[M].北京:中国宇航出版社, 2004: 42-44 Светлов В Г, Голубев И С. Air defense missile design[M]. Beijing: Chinese Astronautics Press, 2004: 42-44 (in Chinese) [8] 方开泰,马长兴.正交与均匀实验设计[M].北京:科学出版社, 2001 Fang Kaitai, Ma Changxing. Orthogonal and uniform design of experiments[M]. Beijing: Science Press, 2001 (in Chinese)