[1] 侯明善. 空-空导弹微分对策最佳导引律的研究[J]. 航空学报, 1987, 8(11): 579-586. Hou Mingshan. A study of differential game optimal guidance laws for air-to-air missiles[J]. Acta Aeronautica et Astronautica Sinica, 1987, 8(11): 579-586. (in Chinese)
[2] Shinar J, Shima T, Kebke A. On the validity of linearized analysis in the interception of reentry vehicles//Proceedings of the AIAA Guidance, Navigation, and Control Conference. Reston, VA: AIAA, 1998: 1050-1060.
[3] Gutman S, Leitmann G. Optimal strategies in the neighbourhood of a collision course[J]. AIAA Journal, 1976, 14: 1210-1212.
[4] 蔡远利, 吕学富. 最优策略的导引特性分析[J]. 航空学报, 1990, 11(3): 132-139. Cai Yuanli, Lü Xuefu. The steering characteristic analysis of optimal strategy[J]. Acta Aeronautica et Astronautica Sinica, 1990, 11(3): 132-139. (in Chinese)
[5] Gutman S. On optimal guidance for homing missile[J]. Journal of Guidance, Control, and Dynamics, 1979(3): 296-300.
[6] Shinar J, Gutman S. Three-dimensional optimal pursuit and evasion with bounded control[J]. IEEE Transactions on Automatic Control, 1980(3): 492-496.
[7] Shinar J. Solution techniques for realistic pursuit-evasion game[M]//Advances in Control and Dynamic Systems. New York: Academic Press, 1981: 63-124.
[8] 陈学愚. 一种考虑一阶惯性环节的最优制导律[J]. 航空学报, 1982, 3(4): 84-92. Chen Xueyu. An optimal guidance law via first order inertial loop[J]. Acta Aeronautica et Astronautica Sinica, 1982, 3(4): 84-92. (in Chinese)
[9] Qi N M, Liu Y F, Sun X L. Differential game guidance law for interceptor missile with time-varying lateral acce-leration limits[J]. Transaction of the Japan Society for Aeronautical and Space Sciences (in press).
[10] Shima T. Shinar J. Time varying pursuit-evasion game models with bounded controls[J]. Journal of Guidance, Control, and Dynamics, 2002, 25(3): 425-432.
[11] 李运迁, 齐乃明, 孙小雷, 等. 大气层内拦截弹微分对策制导律对策空间分布研究[J]. 航空学报, 2010, 31(8): 1600-1607. Li Yunqian, Qi Naiming, Sun Xiaolei, et al. Game space decomposition study of differential game guidance law for endoatmospheric interceptor missiles[J]. Acta Aeronautica et Astronautica Sinica, 2010, 31(8): 1600-1607. (in Chinese)
[12] Li Y Q, Qi N M, Zhang W H, et al. Bounded differential game guidance law for interceptor missiles with aero-fins and reaction-jets[J]. Transaction of the Japan Society for Aeronautical and Space Sciences, 2011, 53(182): 275-282.
[13] 郭建国, 周军. 基于H∞控制的非线性末制导律设计[J]. 航空学报, 2009, 30(12): 2423-2427. Guo Jianguo, Zhou Jun. Design of H∞ control based nonlinear terminal guidance law[J]. Acta Aeronautica et Astronautica Sinica, 2009, 30(12): 2423-2427. (in Chinese)
[14] 周锐,张鹏. 基于神经网络的鲁棒制导律设计[J]. 航空学报, 2002, 23(3): 262-264. Zhou Rui, Zhang Peng. Robust guidance law design for homing missile using neural networks[J]. Acta Aeronautica et Astronautica Sinica, 2002, 23(3): 262-264. (in Chinese)
[15] Shima T, Golan O M. Head pursuit guidance[J]. Journal of Guidance, Control, and Dynamics, 2007, 30(5): 1437-1444.
[16] Shima T. Deviated velocity pursuit//AIAA Guidance, Navigation, and Control Conference and Exhibit. Hilton Head, South Carolina: AIAA, 2007: 1537-1552. |