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弹道学报  2012 

一种控制多弹协同攻击时间和攻击角度的方法

, PP. 1-5

Keywords: 导弹,协同作战,虚拟球体,最优控制

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Abstract:

为了提高导弹的突防及精确打击能力,提出一种对协同作战的导弹进行攻击角度和攻击时间控制的方法.选取一枚导弹作为领弹,以目标为球心,以领弹距目标的距离为半径构造虚拟球体,根据从弹的理想攻击角在虚拟球体上确定从弹所对应的虚拟点.建立从弹与虚拟点的相对运动模型,然后基于最优控制理论设计了状态调节器,控制从弹逼近且跟踪虚拟点,最后实现几枚导弹攻击时间和攻击角度的协同.为了降低对从弹需用过载的要求,对虚拟点的轨迹进行了改进设计.仿真结果表明,所提出的控制方法及对虚拟点轨迹的改进设计是有效的.

References

[1]  SONGTL,SHINSJ,CHOH.Impactanglecontrolforplanarengagements[J].IEEE Transactions on Aerospace andElectronicSystems,1999,35(4):1439-1444.
[2]  RATNOO A, GHOSE D.Impact angle constrainedinterceptionofstationarytargets[J].Journalof Guidance,Control,andDynamics,2008,31(6):1816-1821.
[3]  顾文锦,雷军委,潘长鹏.带落角限制的虚拟目标比例导引律设计[J].飞行力学,2006,24(2):43-46.GU Wen-jin,LEIJun-wei,PAN Chang-peng.Designoftheclimbing trajectory using virtual target’s proportionalnavigationmethodwiththecontrolofterminalazimuthofamissile[J].FlightDynamics,2006,24(2):43-46.(inChinese)
[4]  JEONIS,LEEJI,TAHK M J.Homingguidancelawforcooperativeattackofmultiplemissiles[J].JournalofGuidance,Control,andDynamics,2010,33(1):275-280.
[5]  赵世钰,周锐.基于协调变量的多导弹协同制导[J].航空学报,2008,29(6):1605-1611.ZHAOShi-yu,ZHOU Rui.Multi-missilecooperativeguidanceusing coordination variable [J]. Acta Aeronautica etAstronauticaSinica,2008,29(6):1605-1611.(inChinese)
[6]  LEEJI,JEONIS,TAHK M J.Guidancelawtocontrolimpacttimeandangle[J].IEEE Transactionson AerospaceandElectronicSystems,2007,43(1):301-310.
[7]  JUNG B,KIM Y.Guidancelawforanti-ship missilesusingimpact angle and impact time [C].AIAA Guidance,Navigation,andControlConferenceandExhibit.USA:AIAA,2006:1-13.
[8]  张友安,马培蓓.带有攻击角度和攻击时间控制的三维制导[J].航空学报,2008,29(4):1020-1026.ZHANGYou-an,MAPei-bei.Three-dimensionalguidancelawwithimpactangle andimpacttime constraints[J].ActaAeronauticaet AstronauticaSinica,2008,29(4):1 020-1026.(inChinese)
[9]  韦常柱,郭继峰,崔乃刚.导弹协同作战编队队形最优保持控制器设计[J].宇航学报,2010,31(4):1043-1050.WEIChang-zhu,GUO Ji-feng,CUI Nai-gang.Researchonthemissile formation keeping optical control for cooperativeengagement[J].JournalofAstronautics,2010,31(4):1043-1050.(inChinese)
[10]  钱杏芳,林瑞雄,赵亚男.导弹飞行力学[M].北京:北京理工大学出版社,2003.QIAN Xing-fang,LIN Rui-xiong,ZHAO Ya-nan.Missileflightdynamics[M].Beijing:BeijingInstituteofTechnologyPress,2003.

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