Survey of drag-free satellite

被引：0
|
作者：
Shi L. [1 ]
Cao X.-B. [1 ]
Zhang J.-X. [1 ]
Zhang S.-J. [1 ]
Dong X.-G. [1 ]
机构：
[1] Research Center of Satellite Technology, Harbin Institute of Technology
来源：
Yuhang Xuebao/Journal of Astronautics | 2010年 / 31卷 / 06期
关键词：
Accelerometer mode; Displacement mode; Drag-free satellite; Proof mass;
D O I：
10.3873/j.issn.1000-1328.2010.06.001
中图分类号：
学科分类号：
摘要：
A review of the development and the related techniques of a kind of drag-free satellite are presented. Firstly, the concept is introduced, and the differences between the displacement mode and accelerometer mode in drag-free satellite are compared in the paper. Both advantages and disadvantages of the two modes are also given. Secondly, the architecture of drag free satellite is analyzed. And then the control system is divided into three parts: drag free control loop, suspension control loop and satellite control loop. Thirdly, the main functions and features of hardwares such as proof mass and so on in the drag free satellite are described. Lastly, the key techniques for the drag free satellite are listed.
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页码：1511 / 1520
页数：9
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