SOLUTION OF THE PROBLEM OF PRECISE ORIENTATION OF A SPACECRAFT

被引：0
|
作者：
Kulik, A. S.
Luchenko, O. A.
Gavrilenko, O. I.
机构：
来源：
RADIO ELECTRONICS COMPUTER SCIENCE CONTROL | 2005年 / 2卷
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暂无
中图分类号：
TP3 [计算技术、计算机技术];
学科分类号：
0812 ;
摘要：
The decision of a space vehicle precision orientation task in a nominal mode and in fault mode in angular speed vector gyroscope sensor is considered.
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页码：69 / 78
页数：10
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