每年出版 12 期
ISSN 打印: 1064-2315
ISSN 在线: 2163-9337
Indexed in
Spacecraft Angular Reorientation Control by Means of Flywheels
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摘要
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.
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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
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Yefymenko Nikolay, Kudermetov Ravil, Quaternion models of a rigid body rotation motion and their application for spacecraft attitude control, Acta Astronautica, 194, 2022. Crossref