The problem of satellite attitude stabilization in the geomagnetic field
A satellite moving along a circular Keplerian orbit in near-Earth space was explored, focusing on its attitude stabilization in the orbital coordinate system using the intrinsic magnetic and Lorentz force moments. Fluctuations in geomagnetic induction that occur as the satellite orbits cause the coe...
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| Hauptverfasser: | , , |
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| Format: | Artigo |
| Sprache: | Inglês |
| Veröffentlicht: |
Kazan Federal University
2024-12-01
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| Schriftenreihe: | Учёные записки Казанского университета: Серия Физико-математические науки |
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| Online-Zugang: | https://uzakufismat.elpub.ru/jour/article/view/128 |
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