期刊文献+

BTT导弹的新型三维非线性寻的制导律 被引量:3

New Three Dimensional Nonlinear Homing Guidance Law for BTT Missile
在线阅读 下载PDF
导出
摘要 建立了导弹与目标的三维相对运动模型,分析了目前寻的制导律的一些局限性,提出了新型非线性寻的制导律。在更复杂的交战环境中,将此制导律用于高性能的BTT导弹。 Three dimensional relative motion model of missile and target is established in the paper Some limitation in today's most homing guidance laws are analyzed In order to overcome the drawback of the linearization near collision course,nonlinear homing guidance law is derived It is suited to high performance BTT missile in more complex combat enviroment and the guidance precision is greatly enhanced \;
作者 李君龙 江涌
出处 《现代防御技术》 2000年第1期42-46,,64,,共6页 Modern Defence Technology
关键词 寻的制导律 末制导 BTT导弹 非线性 Homing guidance Relative degree\++ Collision course\++ Interception + Terminal guidance
  • 相关文献

参考文献10

  • 1ShinarJ,GutmanS.Three-DimensionalOptimalPursuitandEvasionwithBoundedControls[C].IEEETransonAutomaticControl,1980,25(3):492~496
  • 2LaneSH,StengelRF.FlightControlDesignUsingNonlinearInverseDynamics[J].Automatic,1988,24:471~484
  • 3MenonPKA,BedgettME,WalkerRA,etal.NonlinearFlightTestTrajectoryControllersforAircraft[J].JofGuidance,ControlandDynamics,1987,10(1):67~72
  • 4SinghSN,IyerA.NonlinearDecouplingSlidingModeControlandAttitudeControlofSpacecraft[C].IEEETransonAerospaceandElectronicSystems,1989,25(5):621~633
  • 5DwyerTAW.ExactNonlinearControlofLargeAngleRotation[C].IEEETransonAutomaticControl,1984,29(9):769~774
  • 6HaI-J,ChongS.DesignofaCLOSGuidanceLawviaFeedbackLinearization[C].IEEETransonAerospaceandElectronicSystems,1992,28(1):51~62
  • 7HuangJ,LinC-F.AModifiedCLOSGuidanceLawviaRightInversion[C].IEEETransonAerospaceandElectronicSystems,1995,31(1):491~495
  • 8BezickS,RusnakI,GrayWS.GuidanceofaHomingMissileviaNonlinearGeometricControlMethods[J].JofGuidance,ControlandDynamics,1995,18(3):441~448
  • 9BlakelockJH.AutomaticControlofAircraftandMissiles[M].SecondEdition.NEWYORK:JohnWiley&Sons,1991.
  • 10IsidoriA.NonlinearControlSystems[M].SecondEdition.Heidelberg:Springer-Verlag,1989.

同被引文献10

  • 1周军,周凤岐,陈新海.非线性不确定性系统的变结构控制策略研究[J].西北工业大学学报,1995,13(4):614-618. 被引量:5
  • 2Dong Sang Yoo, Myung Jin Chung. A variable structure control with simple adaptation laws for upper bounds on the norm of the uncertainties[J]. IEEE Transactions on Automatic Control, 1992,37 (6) :860--864.
  • 3Yang Ciann-Dong and Chen Hsin-Yuan.Nonlinear Robust Guidance Law for Homing Missile.AIAA Journal of Guidance,Control,and Dynamics,1998,21(6):882-890
  • 4Sira-Ramirez,Nonlinear Variable Structure Systems in Sliding Mode,The General Case[J].IEEE Trans.Auto.Contr.,1989,34(11):1186-1188
  • 5Tanaka K,Sugeno M.Fuzzy Stability Criterion of A Class of Nonlinear System[J].Information Science,1993,70(1):1-26
  • 6Di Zhou,Chundi Mu,Wenli Xu.Adaptive Sliding-Mode Guidance of a Homing Missile[J].Journal of Guidance,Control and Dynamics,1999,22(4):589-594
  • 7Scott Bezic,Ilan Tusnak and W.Steven Gray.Guidance of Homing Missile via Nonlinear Geometric Control Method[J].J.of Guidance,Control and Dynamics:1995,18(3):441-448
  • 8Ravindra Babu K,Sarma I G,Swamy K N.Switch Bias Proportional Navigation for Homing Guidance Against Highly Maneuvering Targets[J].Journal of Guidance,Control and Dynamics,1994,17(6):1357-1363
  • 9李君龙,陈杰,胡恒章.目标机动时的一种非线性末制导律[J].宇航学报,1998,19(2):37-42. 被引量:13
  • 10李琳琳,赵光恒,赵长安.不确定非线性系统鲁棒控制研究[J].宇航学报,2003,24(4):331-336. 被引量:10

引证文献3

二级引证文献55

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部