Investigation of the dynamics of angular motion and construction of algorithms for controlling the angular momentum of spacecraft using a magnetic attitude control system

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

doi:10.1134/S1028335816110069

Investigation of the dynamics of angular motion and construction of algorithms for controlling the angular momentum of spacecraft using a magnetic attitude control system

Authors: Egorov Y.G.¹, Kulkov V.M.¹, Terentyev V.V.¹, Firsyuk S.O.¹, Shemyakov A.O.¹
Affiliations:
1. Moscow Aviation Institute (National Research University)
Issue: Vol 61, No 11 (2016)
Pages: 558-561
Section: Mechanics
URL: https://journals.rcsi.science/1028-3358/article/view/190666
DOI: https://doi.org/10.1134/S1028335816110069
ID: 190666

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Abstract

The problem of controlling the angular momentum of spacecraft using magnetic attitude control systems interacting with the Earth’s magnetic field is considered. A mathematical model for the angular motion dynamics of a spacecraft has been constructed. An approach to determining the parameters of the control law for a spacecraft attitude control and stabilization system that ensures angular momentum dissipation is proposed.