Modeling the Angular Motion Dynamics of Small Spacecraft with a Magnetic Attitude Control System in a Three-Axis Stabilization Mode

Modeling the Angular Motion Dynamics of Small Spacecraft with a Magnetic Attitude Control System in a Three-Axis Stabilization Mode

The problem of modeling the attitude control modes of small spacecraft using electromagnetic systems interacting with the Earth’s magnetic field is considered. A mathematical model for the angular motion dynamics of small spacecraft has been developed. The control law for linear magnetic attitude co...

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Veröffentlicht in:Doklady. a journal of the Russian Academy of Sciences. Physics 2019-10, Vol.64 (10), p.389-393
Hauptverfasser: Kulkov, V. M., Egorov, Yu. G., Firsyuk, S. O., Terentyev, V. V., Shemyakov, A. O.
Format: Artikel
Sprache:eng
Schlagworte:
Classical Mechanics
Control systems
Control theory
Mathematical and Computational Physics
Mathematical models
Mechanics
Physics
Physics and Astronomy
Satellite attitude control
Spacecraft
Spacecraft attitude control
Theoretical
Three axis stabilization
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Beschreibung
Zusammenfassung:The problem of modeling the attitude control modes of small spacecraft using electromagnetic systems interacting with the Earth’s magnetic field is considered. A mathematical model for the angular motion dynamics of small spacecraft has been developed. The control law for linear magnetic attitude control systems of small spacecraft is formulated. The results of our numerical modeling of the motion of a satellite with a magnetic attitude control system are presented.
ISSN:1028-3358
1562-6903
DOI:10.1134/S1028335819100021