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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

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Spacecraft Angular Reorientation Control by Means of Flywheels

Volume 40, Numéro 10, 2008, pp. 47-55
DOI: 10.1615/JAutomatInfScien.v40.i10.40
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RÉSUMÉ

For the problem of spatial reorientation of spacecraft from the initial position to terminal one we determine preset trajectory and control, realizing it. Optimization of the preset trajectory according to the given criterion is done. Result of numerical modeling is stated. The suggested algorithms are realized in the control system of the "Egyptsat-1" spacecraft, designed by State Design Office "Yuzhnoe" within framework of the international contract between Ukraine and Egypt.

CITÉ PAR
  1. Lapin Alexey V., Zubov Nikolay E., Analytic solution of the problem of stabilizing orbital orientation of a spacecraft with flywheel engines, XLIV ACADEMIC SPACE CONFERENCE: dedicated to the memory of academician S.P. Korolev and other outstanding Russian scientists – Pioneers of space exploration, 2318, 2021. Crossref

  2. Yefymenko Nikolay, Kudermetov Ravil, Quaternion models of a rigid body rotation motion and their application for spacecraft attitude control, Acta Astronautica, 194, 2022. Crossref

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