[1] Kim M, Grider K V.Terminal guidance for impact attitude angle constrained flight trajectories[J]. IEEE Transactions on Aerospace and Electronic Systems, 1973, 9(6):852-859. [2] Zarchan P. Tactical and strategic missile guidance[M]. Reston, VA, US: American Institute of Aeronautics and Astronautics, Inc, 2012: 569-576. [3] Byung S K, Jang G L, Hyung S H. Biased PNG law for impact with angular constraint[J]. IEEE Transactions on Aerospace and Electronic Systems, 1998, 34(1): 277-288. [4] 张春妍, 宋建梅, 侯博, 等. 带落角和时间约束的网络化导弹协同制导律[J]. 兵工学报, 2016, 37(3):431-438. ZHANG Chun-yan, SONG Jian-mei, HOU Bo, et al.Cooperative guidance law with impact angle and impact time constraints for networked missiles[J]. Acta Armamentarii, 2016, 37(3):431-438.(in Chinese) [5] 张友安, 孙阳平, 方悦, 等. 带落角和末端攻角约束的最优末制导律[J]. 海军航空工程学院学报, 2013, 28(4):368-371. ZHANG You-an, SUN Yang-ping, FANG Yue, et al.Optimal guidance law with constraint on terminal impact angle and angle of attack[J]. Journal of Naval Aeronautical and Astronautical University, 2013, 28(4):368-371.(in Chinese) [6] Cho H, Ryoo C K, Tsourdos A, et al.Optimal impact angle control guidance law based on linearization about collision triangle[J]. Journal of Guidance Control and Dynamics, 2014, 37(3):958-964. [7] Rao S, Ghose D.Terminal impact angle constrained guidance laws using variable structure systems theory[J]. IEEE Transactions on Control Systems Technology, 2013, 21(6):2350-2359. [8] Kumar S R, Rao S, Ghose D.Nonsingular terminal sliding mode guidance with impact angle constraints[J]. Journal of Guidance Control and Dynamics, 2014, 37(4):1114-1130. [9] 刁兆师, 单家元. 考虑自动驾驶仪动态特性的含攻击角约束的反演递推制导律[J]. 宇航学报, 2014, 35(7):818-826. DIAO Zhao-shi, SHAN Jia-yuan. Back stepping guidance law with autopilot lag for attack angle constrained trajectories[J]. Journal of Astronautics, 2014, 35(7):818-826. (in Chinese) [10] He S, Lin D, Wang J.Robust terminal angle constraint guidance law with autopilot lag for intercepting maneuvering targets[J]. Nonlinear Dynamics, 2015, 81(1/2):881-892. [11] Swaroop D, Hedrick J K, Yip P P, et al.Dynamic surface control for a class of nonlinear systems[J]. IEEE Transactions on Automatic Control, 2000, 45(10):1893-1899. [12] 熊少锋, 王卫红, 刘晓东, 等. 考虑导弹自动驾驶仪动态特性的带攻击角度约束制导律[J]. 控制与决策, 2015, 30(4): 585-592. XIONG Shao-feng, WANG Wei-hong, LIU Xiao-dong, et al. Impact angle guidance law considering missile's dynamics of autopilot[J]. Control and Decision, 2015, 30(4):585-592.(in Chinese) [13] 张尧, 郭杰, 唐胜景, 等. 机动目标拦截含攻击角约束的新型滑模制导律[J]. 兵工学报, 2015, 36(8):1443-1457. ZHANG Yao, GUO Jie, TANG Sheng-jing, et al. A novel sliding mode guidance law with impact angle constraint for maneuvering target interception[J]. Acta Armamentarii, 2015, 36(8):1443-1457.(in Chinese) [14] Yamasaki T, Balakrishnan S N , Takano H, et al. Sliding mode based intercept guidance with uncertainty and disturbance compensation[J]. IEEE Transactions on Aerospace and Electronic Systems, 2012, 48(4):3331-3345. [15] Shtessel Y, Edwards C, Fridman L, et al. Sliding mode control and observation[M]. NY, US: Birkhuser , 2013: 30-34. [16] Levant A. High-order sliding modes, differentiation and output-feedback control[J]. International Journal of Control, 2003, 76(9): 924-941.
第38卷第5期 2017 年5月兵工学报ACTA ARMAMENTARIIVol.38No.5May2017
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