Abstract
The stabilization of regular precessions of a satellite in a circular orbit is considered using control moments determined by Lorentzian forces. The linearized system of equations of motion belongs to a special class of linear time-varying systems that can be reduced to time-invariant ones. Controllability was studied both for the original time-varying systems and on the basis of the reduced time-invariant systems. Optimal stabilization algorithms have been constructed. Mathematical modeling of the proposed algorithms was carried out, confirming the performance and effectiveness of the proposed methodology.
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Translated by S. Avodkova
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Kalenova, V.I., Morozov, V.M. & Rak, M.G. Stabilization of Regular Satellite Precessions Using Lorentz Force Moments. Cosmic Res 62, 92–98 (2024). https://doi.org/10.1134/S0010952523700752
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DOI: https://doi.org/10.1134/S0010952523700752