[1] Cao Hequan, Zhang Guangming, Sun Sujie, et al. Status and development of protection technology of armored vehicles[J]. Acta Armamentarii, 2012, 33(12): 1549-1554. (in Chinese)
[2] Fang Linghui, Zheng Xiangyu, Cai Hongtu, et al. Development of tank & armored vehicle protection technology[J]. Sichuan Ordnance Journal, 2014, 35(3): 23-26. (in Chinese)
[3] Zhou Ping, Zhao Chenxiao, Mei Lin, et al. Development situation and trends analysis of modern tank active protection system[J]. Command Control & Simulation, 2016, 38(2): 132-136. (in Chinese)
[4] Kim M, Grider K V. Terminal guidance for impact attitude angle constrained flight trajectories[J]. IEEE Trans. on Aerospace and Electronic Systems, 1973, 9(6): 852-859.
[5] Chang Chao, Lin Defu, Qi Zaikang, et al. Study on the optimal terminal guidance law with interception and impact angle[J]. Transactions of Beijing Institute of Technology, 2009, 29(3): 233-236. (in Chinese)
[6] Idan M, Golan O M, Guelman M. Optimal planar interception with terminal constraints[J]. Journal of Guidance, Control and Dynamics, 1995, 18(6): 1273-1279.
[7] Zhang Y A, Wang X L, Ma G X. Impact time control guidance law with large impact angle constraint[J]. Journal of Aerospace Engineering, 2015, 229(11): 2119 -2131.
[8] Ryoo C K, Cho H, Tahk M J. Optimal guidance laws with terminal impact angle constraint[J]. Journal of Guidance, Control and Dynamics, 2005, 28(4): 724-732.
[9] Ohlmeyer E J, Phillips C A. Generalized vector explicit guidance[J]. Journal of Guidance, Control and Dynamics, 2006, 29(2): 261-268.
[10] Park B G, Kim T H, Tahk M J. Optimal impact angle control guidance law considering the seeker′s field-of-view limits[J]. Journal of Aerospace Engineering, 2013, 227(8): 1347 -1364.
[11] Paul Z. Tactical and Strategic Missile Guidance[M]. 6th ed. Lexington: Progress in Astronautics and Aeronautics, 2012: 569-601.
[12] Wang Hui, Lin Defu, Wang Jiang, et al. Analysis and application study on the extended trajectory shaping guidance law[J]. Acta Armamentarii, 2013, 34(7): 801-809. (in Chinese)
[13] Wang Hui, Lin Defu, Cui Xiaoxi. Extended trajectory shaping guidance laws[J]. Transactions of Beijing Institute of Technology, 2014, 34(6): 597-602. (in Chinese)
[14] Wang Hui, Wang Jiang, Lin Defu, et al. Analytic study on extended trajectory shaping guidance system with first-order autopilot dynamics[J]. Systems Engineering and Electronics, 2014, 36(3): 509-518. (in Chinese)
[15] Koray S E. Indirect control of impact angle against stationary targets using biased PPN[C]//AIAA Guidance, Navigation, and Control Conference, 2010: 8148-8154.
[16] Koray S E, Osman M. Indirect impact angle control against stationary targets using biased pre proportional navigation[J]. Journal of Guidance, Control and Dynamics, 2012, 35(2): 700-703.
[17] Koray S E. Control of impact angle using biased proportional navigation[C]//AIAA Guidance, Navigation, and Control Conference, 2013: 5113-5127.
[18] Tekin R, Koray S E. Switched-gain guidance for impact angle control under physical constraints[J]. Journal of Guidance, Control, and Dynamics, 2015, 38(2): 205-216.
[19] Ratnoo A. Analysis of two-stage proportional navigation with impact angle and field-of-view constraints[C]//AIAA Guidance, Navigation, and Control Conference, 2015: 1195-1209.