航天器环境工程2015，Vol.32Issue(3)：291-295,5.DOI:10.3969/j.issn.1673-1379.2015.03.012
力限振动试验夹具设计要求和力测量装置校核方法
The design requirement of the fixture for the force limited vibration test and the FMD validation
岳志勇 1王剑 1李新明 1张俊刚 1冯咬齐1
作者信息
- 1. 北京卫星环境工程研究所,北京 100094
- 折叠
摘要
Abstract
This paper presents some method for the design of the fixture for the force limited vibration test and the validation of force measurement device (FMD). Based on the satellite force limited vibration test, the cause of the force measurement error is discussed. It is shown that the error can be reduced to 10% or less by improving the acceleration factor and the signal to noise ratio, which proves the effectiveness of the FMD is effective.关键词
振动试验/力限控制/试验夹具/力测量装置Key words
vibration test/force limited control/test fixture/force measurement device分类
航空航天引用本文复制引用
岳志勇,王剑,李新明,张俊刚,冯咬齐..力限振动试验夹具设计要求和力测量装置校核方法[J].航天器环境工程,2015,32(3):291-295,5.
