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ISSN 打印: 1064-2315

ISSN 在线: 2163-9337

SJR: 0.173 SNIP: 0.588 CiteScore™:: 2

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Magnetic Attitude Control and Stabilizing System of Egyptsat-1 Spacecraft

卷 42, 册 11, 2010, pp. 64-70
DOI: 10.1615/JAutomatInfScien.v42.i11.70
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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.

参考文献
  1. Yefimenko N.V., Novikov A.K., Regularized ellipsoidal observers and their application in problem of determining space craft attitude.

  2. Lebedev D.V., Tkachenko A.I., Shtepa Yu.N., Magnetic system of satellite angular motion control.

  3. Psiaki M.L., Martel F., Pal P.K., Three axis attitude determination via Kalman filtering of magnetometer data.

  4. Yefimenko N.V., Lutsenko N.V., Control synthesis for magnetic attitude control and stabilizing system of spacecraft.

  5. Tikhonov A.N., Goncharskiy A.V., Stepanov V.V., Yagola A.G., Regularizing algorithms and a priori information.

  6. Tikhonov A.N., Arsenin V.Ya., Solution methods of incorrect problems.

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