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末敏弹系统多刚体动力学分析与仿真 被引量:2

Multi-body Dynamics Analysis and Simulation of Target Sensitivity Drojectile
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摘要 对末敏弹实体模型简化后,运用多刚体动力学中的R-W方法和牛顿-欧拉方法对末敏弹系统各刚体之间的力学关系进行了分析,建立了末敏弹运动的数学模型。编制程序对末敏弹数学模型进行了仿真分析计算,得到了伞弹系统开伞后的运动规律和敏感器扫描的规律,为系统设计提供依据。 The exterior ballistic characteristics of terminally sensitive submunition were analyzed in detail, firsty the model was simplified, the mechanical relation of the three rigid bodies which were friction plate, parachute and numiton was analyzed with the method of R-W mutti-bodies, mathematic model,the movement law of the umbrella ball system parachute-opening and the scan laws of sensitive implement are gained. They provide a basis for system designs.
出处 《弹箭与制导学报》 CSCD 北大核心 2008年第1期173-176,共4页 Journal of Projectiles,Rockets,Missiles and Guidance
关键词 末敏弹 降落伞 外弹道 多刚体 仿真分析 terminally sensitive sabmutions parachute exterior ballistics animation multi-body simulation
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参考文献4

  • 1刘延柱,洪嘉振,扬海兴.多刚体系统动力学[M].北京:高等教育出版社,1997.
  • 2韩子鹏,孙乐.末敏弹刚柔二体相互作用力学模型探讨[J].弹道学报,1997,9(4):45-49. 被引量:1
  • 3White FM, Wolf D F. A theory of three-dimensional parachute dynamic stability[J]. Journal of Aircraft, 1968 (5):86-92.
  • 4Helmut G Heinrich, Robert A Noreen, David P Saari. Development of total trajectory simulation for single recovery parachute systems[R]. AD- 779527,1973.

二级参考文献1

  • 1曾颖超等.战术导弹弹道与姿态动力学[M]西北工业大学出版社,1991.

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