[1] ZARCHAN P.Tactical and strategic missile guidance[M].6th ed.Reston:AIAA,2012:213-324,715-862.
[2] ZES D.Exo-atmospheric intercept using modified proportional guidance with gravity correction for coast phase:AIAA-94-0209[R].Reston:AIAA,1994.
[3] ZES D.Exo-atmospheric intercept with J2 correction:AIAA-98-4305[R].Reston:AIAA,1998.
[4] PHILLIPS C A,MALYEVAC D S.Pulse motor optimization via mission charts for an exoatmospheric interceptor[J].Journal of Guidance,Control,and Dynamics,1998,21(4):611-617.
[5] PHILLIPS C A,MALYEVAC D S.Exoatmospheric interceptor pulse motor optimization with discrete bias removal[J].Journal of Guidance,Control,and Dynamics,2000,23(2):376-378.
[6] GUTMAN S,RUBINSKY S.Exo-atmospheric mid-course guidance[C]//AIAA Guidance,Navigation,and Control Conference.Reston:AIAA,2015:1-17.
[7] HABLANI H B.Pulsed guidance of exoatmospheric interceptor with image processing delays in angle measurements:AIAA-2000-4272[R] Reston:AIAA,2000.
[8] HABLANI H B,PEARSON D W.Miss distance error analysis of exoatmospheric interceptors[J].Journal of Guidance,Control,and Dynamics,2004,27(2):283-289.
[9] GUO J G,ZHANG T B,ZHOU J,et al.The three dimensional guidance system design of terminal attack phase for exo-atmospheric kill vehicle[J].International Journal for Light and Electron Optics,2017,130:1158-1167.
[10] SHIMA T,GOLAN O M.Exo-atmospheric guidance of anaccelerating interceptor missile[J].Journal of the Franklin Institute,2012,349(2):622-637.
[11] ENDER T,LEURCK R F,WEAVER B.Systems-of-systems analysis of ballistic missile defense architecture effectiveness through surrogate modeling and simulation[J].IEEE Systems Journal,2010,4(2):156-166.
[12] 吴钰飞,罗小明,申之明,等.诱饵影响下多枚弹道导弹突防效能研究[J].装备学院学报,2008,19(3):57-62.WU Y F,LUO X M,SHEN Z M,et al.Study on the penetration effectiveness of multiple ballistic missiles considering the effect of decoys[J].Journal of the Academy of Equipment Command & Technology,2008,19(3):57-62(in Chinese).
[13] YAO J,HUANG Q,WANG W.Analyzing ballistic missile defense system effectiveness based on functional dependency network analysis[J].The Open Cybernetics & Systemics Journal,2015,9(1):678-682.
[14] 杨晓凌,邱涤珊.三种不确定性条件下的拦截器目标分配模型[J].弹箭与制导学报,2012,32(4):4-8.YANG X L,QIU D S.Interceptor allocation models under threr types of uncertainty[J].Journal of Projectiles,Rockets,Missiles and Guidance,2012,32(4):4-8(in Chinese).
[15] WILKENING D A.A simple model for calculating ballistic missile defense effectiveness[J].Science and Global Security,1999,8(2):183-255.
[16] GLASER C L,FETTER S.Should the United States reject MAD?Damage limitation and U.S.nuclear strategy toward China[J].International Security,2016,41(1):49-98.
[17] XIE J W,CHEN W C.Switching logic design for divert and attitude control system of exoatmospheric kill vehicle[C]//8th IEEE International Conference on Cybernetics and Intelligent Systems(CIS)/IEEE Conference on Robotics,Automation and Mechatronics (RAM).Piscataway,NJ:IEEE Press,2017:194-200.
[18] 谢经纬,陈万春.基于概率模型的攻防效能估算与仿真分析[J].导弹与航天运载技术,2017(4):1-5.XIE J W,CHEN W C.Estimation and simulation analysis based on probabilistic model for the effectiveness of penetration and defense[J].Missiles and Space Vehicles,2017(4):1-5(in Chinese). |