Citation: | Zhu Bo, Quan Quan, Cai Kaiyuanet al. BP networks method of handing-over point of KKV[J]. Journal of Beijing University of Aeronautics and Astronautics, 2007, 33(03): 332-335. (in Chinese) |
[1] Pini Gurfil, Jodorkovsky M, Guelman M. Neoclassical guidance for homing missiles[J].Journal of Guidance, Control, and Dynamics,2001, 24(3):452-459 [2] Pini Gurfil.Zero-miss-distance guidance law based on line-of-sight rate measurement only[J]. Control Engineering Practice, 2003, 1(17):819-832 [3] 李振营,沈毅,胡恒章.攻击机动目标的最优导引规律研究[J]. 哈尔滨工业大学学报, 1999, 31(6):56-58 Li Zhenying, Shen Yi, Hu Hengzhang. An optimal guidance law for interception of maneuvering targets [J]. Journal of Harbin Institute of Technology, 1999, 31(6):56-58(in Chinese) [4] 邱玲,沈振康. KKV小型化的神经网络制导规律研究[J].宇航学报,2000, 21(4):124-128 Qiu Ling, Shen Zhenkang. Minimizing KKV size using neural networks [J].Journal of Astronautics,2000, 21(4):124-128(in Chinese) [5] 董朝阳,景韶光,王青,等.基于模糊神经网络的导弹最优寻的末制导律[J].北京航空航天大学学报,2002, 28(4):373-375 Dong Chaoyang, Jing Shaoguang, Wang Qing, et al. Optimal terminal missile guidance law based on fuzzy neural networks[J]. Journal of Beijing University of Aeronautics and Astronautics, 2002, 28(4):373-375(in Chinese) [6] Lin C, Chen Y. Design of fuzzy logic guidance law against high speed target [J].Journal of Guidance, Control and Dynamics, 2000, 23(1):17-25 [7] 周荻, 幕春棣.被动式寻的导弹的运动跟踪变结构制导[J].航空学报, 1998, 19(2):179-183 Zhou Di, Mu Chundi. Motion tracking variable structure guidance for passive homing-missile[J]. Acta Aeronautica et Astronautica Sinica, 1998, 19(2):179-183(in Chinese) [8] Lin Chunliang, Hung Haozhen, Chen Yungyue. Development of an integrated fuzzy-logic-based missile guidance law against high speed target [J]. IEEE Transactions on Fuzzy Systems, 2004, 12(2):157-169 [9] Haykin S.神经网络原理[M].第2版.叶世伟译.北京:机械工业出版社,2004 Haykin S. Neural Networks:a comprehensive foundation[M]. 2nd edition.Translated by Ye Shiwei.Beijing:China Machine Press, 2004
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