Electrodynamic Attitude Stabilization of a Spacecraft in an Elliptical Orbit
One of the fundamental problems of spacecraft dynamics related to ensuring its angular orientation in the basic coordinate system is considered. The problem of electrodynamic attitude control for a spacecraft in an elliptical near-Earth Keplerian orbit is studied. A mathematical model describing the...
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| Κύριοι συγγραφείς: | , , |
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| Μορφή: | Artigo |
| Γλώσσα: | Inglês |
| Έκδοση: |
MDPI AG
2024-11-01
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| Σειρά: | Aerospace |
| Θέματα: | |
| Διαθέσιμο Online: | https://www.mdpi.com/2226-4310/11/11/956 |
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