Force Limiting testing for the small explorer satellite program at NASA Goddard Space Flight Center

被引:0
|
作者
Kaufman, DS [1 ]
机构
[1] Orbital Sci Corp, Tech Serv Div, Greenbelt, MD 20770 USA
来源
PROCEEDINGS OF THE 18TH AEROSPACE TESTING SEMINAR | 1999年
关键词
Force Limiting; dual control; spacecraft testing; impedance; accelerance; Random Vibration;
D O I
暂无
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The Wide Field Infrared Explorer (WIRE) and Transition Region Coronal Explorer (TRACE) Spacecraft underwent Random Vibration Testing using Force Limiting Techniques as a means of controlling the vibration input motions. Interface force measurements were made for random vibration tests. Automatic force feedback notching was provided for the random vibration tests. This paper presents the methods employed to determine force spectrums. Test results are presented to show the effects of the force limiting technique.
引用
收藏
页码:131 / 149
页数:5
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