Magnetic Attitude Control and Stabilizing System of Egyptsat-1 Spacecraft

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.