Ratnoo A, Ghose D. Impact angle constrained interception of nonstationary nonmaneuvering targets[J]. Journal of Guidance, Control, and Dynamics, 2010,33(1):269-275.
[2]
Zarchan P. Tactical and strategic missile guidance[M]. 5th ed. Virginia: AIAA Inc., 2007:31-50,541-569.
[3]
Ryoo C K, Shin H S, Tahk M J. Energy optimal waypoint guidance synthesis for antiship missiles[J]. IEEE Transactions on Aerospace and Electronic Systems, 2010,46(1):80-95.
[4]
Yoon M G. Relative circular navigation guidance for the impact angle control problem[J]. IEEE Transactions on Aerospace and Electronic Systems, 2008,44(4):1449-1463.
[5]
Cherry G. A general explicit, optimizing guidance law for rocker-propelled spacecraft, AIAA 1964[R]. [S.l.]: AIAA, 1964:614-638.
[6]
Song T L, Shin S J. Time-optimal impact angle control for vertical plane engagements[J]. IEEE Transactions on Aerospace and Electronic Systems, 1999,35(2):738-742.
[7]
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.
[8]
Ryoo C K, Cho H, Tahk M J. Time-to-go weighted optimal guidance with impact angle constraints[J]. IEEE Transactions on Control Systems Technology, 2006,14(3):483-492.
[9]
Lee Y I, Kim S H, Tahk M J. Optimality of linear time-varying guidance for impact angle control[J]. IEEE Transactions on Aerospace and Electronic Systems, 2012,48(3):2802-2817.
[10]
Lee Y I, Kim S H, Lee J I. Analytic solutions of generalized impact angle control guidance law for first-order lag system[J]. Journal of Guidance, Control, and Dynamics, 2013,36(1):96-112.
[11]
Ohlmeyer E J, Phillips C A. Generalized vector explicit guidance [J]. Journal of Guidance, Control, and Dynamics, 2006,29(2):261-268.
[12]
刘大卫,夏群利,左媞媞,等.包含弹体动力学的终端角约束弹道成型制导律[J].北京理工大学学报,2013,33(4):363-368. Liu Dawei, Xia Quanli, Zuo Titi, et al. Trajectory shaping guidance law with terminal impact angle constraint including missile body dynamics [J]. Transactions of Beijing Institute of Technology, 2013,33(4):363-368. (in Chinese)
[13]
Wang H, Lin D F, Cheng Z X. Time-to-go weighted optimal trajectory shaping guidance law[J]. Journal of Beijing Institute of Technology, 2011,20(3):317-323.
[14]
王辉,林德福,崔晓曦.一类扩展的弹道成型制导律[J].北京理工大学学报,2014,34(6):597-603. Wang Hui, Lin Defu, Cui Xiaoxi. Extended trajectory shaping guidance laws[J]. Transactions of Beijing Institute of Technology, 2014,34(6):597-603. (in Chinese)
[15]
孙胜,张华明,周荻.考虑自动驾驶仪动特性的终端约束滑膜导引律[J].宇航学报,2013,34(1):69-78. Sun Sheng, Zhang Huaming, Zhou Di. Sliding mode guidance law with autopilot lag for terminal angle constrained trajectories[J]. Journal of Astronautics, 2013,34(1):69-78. (in Chinese)
