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

V. M. Kulkov; Yu. G. Egorov; S. O. Firsyuk; V. V. Terentyev; A. O. Shemyakov

doi:10.1134/S1028335819100021

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

Authors: Kulkov V.M.¹, Egorov Y.G.¹, Firsyuk S.O.¹, Terentyev V.V.¹, Shemyakov A.O.¹
Affiliations:
1. Moscow Aviation Institute (National Research University)
Issue: Vol 64, No 10 (2019)
Pages: 389-393
Section: Mechanics
URL: https://journals.rcsi.science/1028-3358/article/view/193641
DOI: https://doi.org/10.1134/S1028335819100021
ID: 193641

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Abstract

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.