Drag-free control for MiniSTEP

被引：6
|
作者：
Jafry, Y
机构：
[1] Space Science Department of ESA, ESTEC, Noordwijk
来源：
CLASSICAL AND QUANTUM GRAVITY | 1996年 / 13卷 / 11A期
关键词：
D O I：
10.1088/0264-9381/13/11A/025
中图分类号：
P1 [天文学];
学科分类号：
0704 ;
摘要：
The MiniSTEP drag-free control system must reduce the atmospheric drag forces acting on the spacecraft by seven orders of magnitude, to yield an average residual acceleration of less than 3 x 10(-14) m s(-2) averaged over the measurement bandwidth. The origins of the drag-free requirements are discussed, and a control system is presented which meets the requirements under realistic assumptions for noise levels.
引用
收藏
页码：A179 / A184
页数：6
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