[1] 蔡洪,胡正东,曹渊.具有终端角度约束的导引律综述[J].宇航学报,2010,31(2):315-323.CAI H,HU Z D,CAO Y.A survey of guidance law with terminal impact constraints[J].Journal of Astronautics,2010,31(2):315-323(in Chinese).
[2] PARK B G,KIM T H,TAHK M J.Biased PNG with terminal-angle constraint for intercepting nonmaneuvering targets under physical constraints[J].IEEE Transactions on Aerospace and Electronic System,2017,55(3):1562-1572.
[3] SHINAR J,SHIMA T,KEBKE A.On the validity of linearized analysis in the interception of reentry vehicles[C]//Proceedings of the AIAA Guidance,Navigation,and Control Conference.Reston:AIAA,1998:1050-1060.
[4] 张友安,黄诘,孙阳平.带有落角约束的一般加权最优制导律[J].航空学报,2014,35(3):848-856.ZHANG Y A,HUANG J,SUN Y P.Generalized weighted optimal guidance law with impact angle constraints[J].Acta Aeronautica et Astronautica Sincia,2014,35(3):848-856(in Chinese).
[5] 刘延芳,齐乃明,夏齐,等.基于非线性模型的大气层内拦截弹微分对策制导律[J].航空学报,2011,32(7):1171-1179.LIU Y F,QI N M,XIA Q,et al.Differential game guidance law for endoatmospheric interceptor missiles based on nonlinear model[J].Acta Aeronautica et Astronautica Sincia,2011,32(7):1171-1179(in Chinese).
[6] 周卫东,陈沿逵,熊少锋.带攻击角度约束的无抖振滑模制导律设计[J].北京航空航天大学学报,2016,42(2):669-676. ZHOU W D,CHEN Y K,XIONG S F.Chattering-free sliding mode guidance law with impact angle constraint[J].Journal of Beijing University of Aeronautics and Astronautics,2016,42(2):669-676(in Chinese).
[7] ATES U A.Lyapunov based nonlinear impact angle guidance law for stationary targets[C]//Proceeding of the AIAA Guidance,Navigation,and Control Conference.Reston:AIAA,2015:1-14.
[8] ZHANG Y X,SUN M W,CHEN Z Q.Finite time convergent guidance law with impact angle constraint based on sliding control[J].Nonlinear Dynamics,2012,7(3):619-625.
[9] HE S M,LIN D.Adaptive nonsingular sliding mode based guidance law with terminal angular constraint[J].International Journal of Aeronautical and Space Sciences,2014,15(2):146-152.
[10] 杨锁昌,张宽桥,陈鹏.带攻击角度约束的自适应终端滑模制导律[J].北京航空航天大学学报,2016,42(8):1566-1574.YANG S C,ZHANG K Q,CHEN P.Adaptive terminal sliding mode guidance with impact angle constraint[J].Journal of Beijing University of Aeronautics and Astronautics,2016,42(8):1566-1574(in Chinese).
[11] SONG J H,SONG S M,ZHOU H B.Adaptive nonsingular fast terminal sliding mode guidance law with impact angle constraints[J].International Journal of Control,Automation and Systems,2016,14(1):99-114.
[12] POLYAKOV A.Nonlinear feedback design for fixed-time stabilization of linear control systems[J].IEEE Transactions on Automatic Control,2012,57(8):2106-2110.
[13] ZUO Z Y.Nonlinear fixed-time consensus tracking for second-order multi-agent networks[J].Automatica,2015,54:305-309.
[14] LI H J,CAI Y L.On SFTSM control with fixed-time convergence[J].IET Control Theory and Applications,2017,11(6):766-773.
[15] ZHANG Y,TANG S J,GUO J.Adaptive terminal angle constraint interception against maneuvering targets with fast fixed-time convergence[J].International Journal of Robust and Nonlinear Control,2018,28(8):2996-3014.
[16] SUN S,ZHOU D,HOU W T.A guidance law with finite time convergence accounting for autopilot lag[J].Aerospace Science and Technology,2013,25(1):132-137.
[17] ZHAO B,ZHOU J.Smooth adaptive finite time guidance law with impact angle constraints[J].International Journal of Aerospace Engineering,2016,2016:5730168.
[18] YANG L,YANG J Y.Nonsingular fast terminal sliding-mode control for nonlinear dynamical systems[J].International Journal of Robust Nonlinear Control,2011,21(16):1865-1879.
[19] 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.
[20] XIONG S F,WANG W H,SONG S,et al.Extended state observer based impact angle constrained guidance law for maneuvering target interception[J].Journal of Aerospace Engineering,2015,29(14):2589-2607. |