Spacecraft Angular Reorientation Control by Means of Flywheels

Nikolay V. Yefimenko

doi:10.1615/JAutomatInfScien.v40.i10.40

Journal of Automation and Information Sciences

Главный редактор: Arkadiy A. Chikriy (open in a new tab)

Ассоциированный редакторs: Vyacheslav F. Gubarev (open in a new tab) Yuriy P. Kondratenko (open in a new tab) Nonna V. Turovyerova (open in a new tab)

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ISSN Печать: 1064-2315

ISSN Онлайн: 2163-9337

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Spacecraft Angular Reorientation Control by Means of Flywheels

Том 40, Выпуск 10, 2008, pp. 47-55

DOI: 10.1615/JAutomatInfScien.v40.i10.40

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Nikolay V. Yefimenko
Research and Production Enterprise "Hartron-UCOM", Zaporozhye

Краткое описание

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.

ЦИТИРОВАНО В

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
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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