太阳翼基板模态分析与试验验证
详细信息 查看官网全文
- 英文论文题名：Modal analysis and experimental verification on solar wing substrate
- 论文作者：刘少锋 ; 李珊珊
- 英文论文作者：LIU Shao-feng ; LI Shan-shan ; Beijing Institute of Spacecraft System Engineering ; Beijing Institute of Remote Sensing Equipment
- 年：2016
- 作者机构：北京空间飞行器总体设计部;北京遥感设备研究所;
- 论文关键词：太阳翼基板 ; 模态分析 ; 振动试验
- 英文论文关键词：solar wing substrate ; modal analysis ; vibration test
- 会议召开时间：2016-07-28
- 会议录名称：第二十七届全国振动与噪声应用学术会议论文集
- 语种：中文
- 分类号：V442
- 学会代码：ZDZD
- 会议名称：第二十七届全国振动与噪声应用学术会议
- 会议地点：中国黑龙江哈尔滨
- 主办单位：中国振动工程学会振动与噪声控制专业委员会
- 学会名称：中国振动工程学会振动与噪声控制专业委员会
- 页数：5
- 文件大小：441k
- 原文格式：D
- 会议级别：全国
摘要
模态分析是太阳翼基板设计过程中的重要环节,目的为获取基板的固有频率和固有特性,是分析太阳翼动态响应和其他动力学特性的基础,因此必须保证模态分析结果的正确性。文章通过基板正弦振动试验对模态分析结果进行了验证,模态分析结果与试验结果偏差仅0.5%,吻合良好。
Modal analysis is an important part of the designing process of solar wing substrate. The main purpose is to obtain inherent frequency and inherent characteristic. It is also the foundation of the analysis of the solar wing dynamic response and other kinetic characteristics. Correctness of the modal analysis results is very important. The modal analysis results are verified by the vibration test of the substrate, and the results of the modal analysis are in good agreement with the experimental results.
Modal analysis is an important part of the designing process of solar wing substrate. The main purpose is to obtain inherent frequency and inherent characteristic. It is also the foundation of the analysis of the solar wing dynamic response and other kinetic characteristics. Correctness of the modal analysis results is very important. The modal analysis results are verified by the vibration test of the substrate, and the results of the modal analysis are in good agreement with the experimental results.
引文
[1]谭维炽,胡金刚.航天器系统工程[M].北京:中国科学技术出版社,2009.
[2]陈烈民.航天器结构与机构[M].北京:中国科学技术出版社,2005.
[3]王泽宇,刘闯,冯咬齐.基于振动试验数据的有限元模型修正技术研究[J].航天器环境工程,2010,27(4):472-476.
[4]袁家军.卫星结构设计与分析[M].北京:中国宇航出版社,2004.
[2]陈烈民.航天器结构与机构[M].北京:中国科学技术出版社,2005.
[3]王泽宇,刘闯,冯咬齐.基于振动试验数据的有限元模型修正技术研究[J].航天器环境工程,2010,27(4):472-476.
[4]袁家军.卫星结构设计与分析[M].北京:中国宇航出版社,2004.