Magnetic Attitude Control and Stabilizing System of Egyptsat-1 Spacecraft

被引：0
|
作者：
Yefimenko, N. V. [1 ]
机构：
[1] Dept Res & Prod Enterprise KHARTRON YUKOM, Zaporozhe, Ukraine
来源：
JOURNAL OF AUTOMATION AND INFORMATION SCIENCES | 2010年 / 42卷 / 11期
关键词：
attitude control and stabilizing system; electromagnets; three-component magnetometer; angular movement parameters;
D O I：
10.1615/JAutomatInfScien.v42.i11.70
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
Results of the flight test carried out with magnetic attitude control and stabilizing system of the Egyptsat-1 spacecraft are considered. The system uses electromagnets as magnetorquers and three-component magnetometer as a sensor of source information on angular movement parameters. There is a brief description of control system software and algorithmic support and results of the flight test for the present system.
引用
收藏
页码：64 / 70
页数：7
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