Abonnement à la biblothèque: Guest
Journal of Automation and Information Sciences

Publication de 12  numéros par an

ISSN Imprimer: 1064-2315

ISSN En ligne: 2163-9337

SJR: 0.173 SNIP: 0.588 CiteScore™:: 2

Indexed in

Magnetic Attitude Control and Stabilizing System of Egyptsat-1 Spacecraft

Volume 42, Numéro 11, 2010, pp. 64-70
DOI: 10.1615/JAutomatInfScien.v42.i11.70
Get accessGet access

RÉSUMÉ

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.

RÉFÉRENCES
  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.

Portail numérique Bibliothèque numérique eBooks Revues Références et comptes rendus Collections Prix et politiques d'abonnement Begell House Contactez-nous Language English 中文 Русский Português German French Spain