首页 | 本学科首页   官方微博 | 高级检索  
     

大型空间刚柔耦合组合体的动力学建模
引用本文:和兴锁,邓峰岩,张烈霞,林胜勇.大型空间刚柔耦合组合体的动力学建模[J].机械科学与技术(西安),2004,23(5):543-545,607.
作者姓名:和兴锁  邓峰岩  张烈霞  林胜勇
作者单位:西北工业大学工程力学系 西安710072 (和兴锁,邓峰岩,张烈霞),西北工业大学工程力学系 西安710072(林胜勇)
摘    要:根据大型刚柔耦合空间组合体的结构特点 ,研究带挠性附件的空间结构的建模方法。文中组合体看成为在中心体上连接若干柔性附件 ,附件铰接于中心体 ,它相对于中心体运动。作者根据Lagrange方法建立了大型刚柔耦合空间组合体的动力学方程。

关 键 词:刚柔耦合系统  动力学  建模
文章编号:1003-8728(2004)05-0543-03

Dynamics Modeling of Large Coupled Rigid-Flexible Space Platform System
HE Xing-suo,DENG Feng-yan,ZHANG Lie-xia,LIN Sheng-yong.Dynamics Modeling of Large Coupled Rigid-Flexible Space Platform System[J].Mechanical Science and Technology,2004,23(5):543-545,607.
Authors:HE Xing-suo  DENG Feng-yan  ZHANG Lie-xia  LIN Sheng-yong
Abstract:In this paper, the dynamic equations for a coupled rigid-flexible space platform consisting of a central body and flexible appendages are derived by use of the hybrid coordinate method according to the Lagrange′s equations. The space platform is regarded as connecting some flexible appendages in central body. The central body performs orbit motion, appendages moves relatively to the central body. The behavior of flexible bodies undergoing large rigid-body motions and small elastic vibrations is a subject of major concern in the field of flexible multi-body system dynamics. The method proposed in this paper can be used for modeling and designing of coupled rigid-flexible multi-body spacecraft.
Keywords:Coupled rigid-flexible multi-body system  Dynamics  Modeling
本文献已被 CNKI 维普 万方数据 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号