Improving the attitude determination accuracy for an Earth Remote sensing spacecraft

被引:0
|
作者
Odintsov B.V. [1 ]
机构
[1] Concern CSRI Elektropribor, JSC, St. Petersburg
关键词
Electrostatics;
D O I
10.1134/S207510871101007X
中图分类号
学科分类号
摘要
This paper considers the problem of improving the accuracy of spacecraft attitude determination through refining the drift model coefficients of strapdown electrostatic gyros and defining the misalignments between the gyro and the star sensor axes. The results of the office studies of the data of electrostatic gyros are presented. © Pleiades Publishing, Ltd., 2011.
引用
收藏
页码:10 / 15
页数:5
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