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ISSN Druckformat: 1064-2315
ISSN Online: 2163-9337
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Magnetic Attitude Control and Stabilizing System of Egyptsat-1 Spacecraft
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ABSTRAKT
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.
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