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某卫星微振动建模与仿真
引用本文:蒋国伟,周徐斌,申军烽,顾亦磊,杜 冬,孔祥森.某卫星微振动建模与仿真[J].航天器环境工程,2011,28(1):36-40.
作者姓名:蒋国伟  周徐斌  申军烽  顾亦磊  杜 冬  孔祥森
作者单位:上海卫星工程研究所,上海,200240
基金项目:中国航天八院基金资助项目
摘    要:针对某卫星微振动力学环境,参考IME颤振分析建模方法,建立了一种卫星刚柔耦合多体动力学微振动仿真模型,并通过地面试验验证了利用微振动仿真模型预测卫星在轨微振动响应的有效性,阐述了卫星在轨微振动响应仿真计算预测方法.利用该微振动仿真模型能较准确地预测卫星在轨微振动响应以及微振动传递特性.

关 键 词:卫星  微振动  耦合动力学  建模
收稿时间:9/3/2010 12:00:00 AM

Modeling and simulation of micro-vibration for a satellite
Jiang Guowei,Zhou Xubin,Shen Junfeng,Gu Yilei,Du Dong and Kong Xiangsen.Modeling and simulation of micro-vibration for a satellite[J].Spacecraft Environment Engineering,2011,28(1):36-40.
Authors:Jiang Guowei  Zhou Xubin  Shen Junfeng  Gu Yilei  Du Dong and Kong Xiangsen
Institution:Shanghai Institute of Satellite Engineering, Shanghai 200240, China;Shanghai Institute of Satellite Engineering, Shanghai 200240, China;Shanghai Institute of Satellite Engineering, Shanghai 200240, China;Shanghai Institute of Satellite Engineering, Shanghai 200240, China;Shanghai Institute of Satellite Engineering, Shanghai 200240, China;Shanghai Institute of Satellite Engineering, Shanghai 200240, China
Abstract:Based on the method of micro-vibration modeling of IME, a multi-flexible coupling dynamics model is developed to analyze the micro-vibration of a satellite. The results agree well with the ground micro-vibration test, which shows that the model could be used to test the micro-vibration behavior of the satellite in orbit and the transfer characteristics of micro-vibration signals in the satellite structure.
Keywords:satellite  micro-vibration  coupling dynamics  modeling
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