孙未蒙,刘湘洪.多约束条件下的制导律研究综述[J].飞行力学,2010,28(4):1-4. Sun Weimeng, Liu Xianghong. Survey on the developments on the guidance law with impact angular constraints[J]. Flight Dynamics,2010,28(4):1-4.(in Chinese)
[2]
蔡洪,胡正东,曹渊.具有终端角约束的导引律总述[J].宇航学报,2010,31(2):315-332. Cai Hong, Hu Zhengdong, Cao Yuan. A survey of guidance law with terminal impact angle constraints [J]. Journal of Astronautics, 2010,31(2):315-332. (in Chinese)
[3]
Zarchan P. Tactical and strategic missile guidance[M]. 4th ed. Reston, VA: Progress in Astronautics and Aeronautics, AIAA, 2002:541-548.
[4]
Ryoo C K, Cho H J, Tahk M J. Optimal guidance laws with terminal impact angle constraint[J]. Journal of Guidance, Control and Dynamics, 2005,11(4):724-732.
[5]
陈克俊,赵汉元.-种适用于攻击地面固定目标的最优再入机动制导律[J].宇航学报,1994,15(1):1-7. Chen Kejun,Zhao Hanyuan. An optimal reentry maneuver guidance law applying to attack the ground fixed target[J]. Journal of Astronautics,1994,15(1):1-7. (in Chinese)
[6]
刘丹,祁载康.限制导弹落角和落点的最优制导律[J].北京理工大学学报,2001,21(3):278-281. Liu Dan,Qi Zaikang. Impact angle and final position constrained optimal guidance law[J]. Transactions of Beijing Institute of Technology,2001,21(3):278-281. (in Chinese)
[7]
常超,林德福,祁载康,等.带落点和落角约束的最优末制导律研究[J].北京理工大学报,2009,29(3):233-236. 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)
[8]
Liu Dawei, Xia Qunli, Wu Tao, et al. Trajectory shaping guidance law with terminal impact angle constraint[J]. Journal of Beijing Institute of Technology, 2011,20(3):345-350.