Zhao M Y, Wei M Y. Finite time stable variable structure guidance law with double closed-loop filters. Acta Aeronautica et Astronautica Sinica, 2010, 31(8): 1629-1635. (in Chinese) 赵明元, 魏明英. 带有双闭环滤波器的有限时间稳定变结构制导律. 航空学报, 2010, 31(8): 1629-1635.
[2]
Fan H T, Yang J, Zhu X P. Research on beam stable technology of phased array radar seeker. Acta Aeronautica et Astronautica Sinica, 2013, 34(2): 387-392. (in Chinese) 樊会涛, 杨军, 朱学平. 相控阵雷达导引头波束稳定技术研究. 航空学报, 2013, 34(2): 387-392.
[3]
Zarchan P. Tactical and strategic missile guidance fourth edition. Virginia: Astronautics and Aeronautics, Inc, 2002: 145-161.
[4]
Ryoo C K, Cho H J, Tahk M J. Optimal guidance laws with terminal impact angle constraint. Journal of Guidance, Control and Dynamics, 2005, 11(4): 724-732.
[5]
Hexner G, Pila A. A practical stochastic optimal guidance law for a bounded acceleration missile. AIAA Guidance Navigation and Control Conference and Exhibit, 2010: 1-23.
[6]
Liu D W, Xia Q L, Cui Y Y, et al. Generalized trajectory shaping guidance law with both impact position and angle constrains. Journal of Beijing Institute of Technology, 2011, 31(12): 1406-1413. (in Chinese) 刘大卫, 夏群利, 崔莹莹, 等. 具有终端位置和角度约束的广义弹道成型制导律. 北京理工大学学报, 2011, 31(12): 1406-1413.
[7]
Wang X H, Zhang M L. Researching and accomplishing for homing missile attacking maneuvering target. Acta Aeronautica et Astronautica Sinica, 2000, 21(1): 30-33. (in Chinese) 王小虎, 张明廉. 自寻的导弹攻击机动目标的最优制导规律的研究及实现. 航空学报, 2000, 21(1): 30-33.
[8]
Hexner G, Weiss H. Temporal multiple model estimator for a maneuvering target. AIAA Guidance Navigation and Control Conference and Exhibit, 2008: 1-26.
[9]
Xu P, Wang W, Lin D F. Effect of seeker isolation on guidance and control of terminal guided projectile. Journal of Ballistics, 2012, 24(1): 17-22.(in Chinese) 徐平, 王伟, 林德福. 导引头隔离度对末制导炮弹制导控制的影响. 弹道学报, 2012, 24(1): 17-22.
[10]
Spencer A, Moore W. Design trade-offs for homing missiles. AIAA SDIO Annual Interceptor Technology Conference, 1992: 1-20.
[11]
Nesline F W, Zarchan P. A new look at classical vs modern homing missile guidance. Journal of Guidance and Control, 1981, 1(4): 78-85.
[12]
Tahk M J, Ryoo C K, Cho H J. Recursive time-to-go estimation for homing guidance missiles. IEEE Transactions on Aerospace and Electronic Systems, 2002, 38(1): 13-24.
[13]
Whang I H, Ra W S. Time-to-go estimator for missiles guided by BPNG. International Conference on Control, Automation and Systems, 2008: 463-467.
[14]
Qi Z K, Xia Q L. Guided weapon control system. Beijing: Beijing Institute of Technology Press, 2004: 308-352.
[15]
Li F G, Xia Q L, Qi Z K, et al. Effect of parasitic loop on strap-down seeker and compensated with identification method. Systems Engineering and Electronics, 2013, 35(8): 73-78. (in Chinese) 李富贵, 夏群利, 祁载康, 等. 全捷联导引头寄生回路影响与辨识校正. 系统工程与电子技术, 2013, 35(8): 73-78.
[16]
Li F G, Xia Q L, Cui X X, et al. Effect of seeker disturbance rejection rate parasitic loop on line of sight rate extraction. Journal of Astronautics, 2013, 34(7): 1-6. (in Chinese) 李富贵, 夏群利, 崔晓曦, 等. 导引头隔离度寄生回路对视线角速度提取的影响. 宇航学报, 2013, 34(7): 1-6.
