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基于拟合模态法的大范围运动柔性曲线梁动力学建模方法研究
引用本文:何柏岩,王树新,金国光,王辉.基于拟合模态法的大范围运动柔性曲线梁动力学建模方法研究[J].宇航学报,2003,24(3):273-277.
作者姓名:何柏岩  王树新  金国光  王辉
作者单位:1. 天津大学机械工程学院,天津,300072
2. 北京航空航天大学机器人研究所,北京,100083
基金项目:国家自然科学基金 (E0 5 990 5 0 19)资助项目
摘    要:大范围运动柔性曲线梁的动力学建模主要采用有限元法,这是由于很难得到曲线梁模态的解析模态表达式,求解的复杂程度随着单元的增加而增加。本文提出一种拟合模态法进行动力学建模,把大型有限元分析软件计算得出的模态拟合成为多项式的形式,得到曲线梁模态的近似解析表达式,从而大大简化了建模与计算的过程。以某型号卫星抛物面天线为例,验证了方法的可行性与准确型。

关 键 词:柔性体  动力学  ANSYS  模态
文章编号:1000-1328(2003)03-0273-05
修稿时间:2002年9月23日

Dynamic model of a moving flexible camber beam by the method of fitted modal
HE Bai-yan ,WANG Shu-xin ,JIN Guo-guang ,WANG Hui.Dynamic model of a moving flexible camber beam by the method of fitted modal[J].Journal of Astronautics,2003,24(3):273-277.
Authors:HE Bai-yan  WANG Shu-xin  JIN Guo-guang  WANG Hui
Institution:HE Bai-yan 1,WANG Shu-xin 1,JIN Guo-guang 2,WANG Hui 1
Abstract:Because of the difficulty in finding the analytic modal,the dynamics analysis of a moving flexible camber beam is often by means of Finite Element Method (FEM).The processes of FEM become very complex with the increasing of elements.A new method called Fitted Modal Method (FMM) was described in this paper as a alternative.The discrete modal solution of a camber beam was calculated by FEM software such as ANSYS and the approximate analytic modal expressions were obtained by fitting the discrete modal into the form of polynomial expression.This made the modeling and solving processes simple and convenient.The dynamic analysis of a paraboloid antenna was used as an illustrative example to verify the accuracy of FMM.
Keywords:Flexible body  Dynamics  ANSYS  Modal
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