[1] Garnell P. Guided Weapon Control Systems[M]. Beijing: National Defence Industry Press, 1985: 248-299.
[2] Zarchan P. Tactical and Strategic Missile Guidance[M]. 6th ed. Virginia: AIAA Inc, 2012: 31-50, 541-569.
[3] Ohlmeyer E J, Phillips C A. Generalized vector explicit guidance[J]. Journal of Guidance Control and Dynamics, 2006, 29(2): 261-268.
[4] 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.
[5] 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.
[6] 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.
[7] Kim B S, Lee J G, Han H S. Biased PNC law for impact with angular constraint[J]. IEEE Transactions on Aerospace and Electronic Systems, 1998, 34(1): 277-288.
[8] Wang Hui, Lin Defu, Qi Zaikang, et al. Study of time-varying optimal augmented proportional navigation and miss distance closed-form solutions[J]. Infrared and Laser Engineering, 2013, 42(3): 92-698. (in chinese)
[9] Xu Ping, Wang Wei, Lin Defu, et al. Fluence of zero position error of angular rate on the precision of proportional navigation[J]. Infrared and Laser Engineering, 2011, 40(11): 2255-2260. (in Chinese)
[10] Ben-Asher J Z, Yaesh I. Advances in Missile Guidance Theory[M]. Virginia: AIAA Inc, 1998.
[11] Ryoo C K, Cho H, Tahk M J. Closed-form solutions of optimal guidance with terminal impact angle constraint [C]//IEEE Int Conf Control Application, 2003: 504-509.
[12] Wang Hui, Lin Defu, Cheng Zhenxuan. Time-to-go weighted optimal trajectory shaping guidance law[J]. Journal of Beijing Institute of Technology, 2011, 20(3): 317-323.
[13] Wang Hui, Lv Yingjie, Lin Defu, et al. Miss distance analysis of the extended trajectory shaping guided systems[J]. Infrared and Laser Engineering, 2013, 42(5): 1322-1329. (in chinese)
[14] Yang C D, Hsiao F B, Yeii F B. Generalized guidance law for homing missiles[J]. IEEE Transactions on Aerospace and Electronic Systems, 1989, AES-25(2): 197-212.