Averaging method in the problem of the Lorentz stabilization of the indirect equilibrium position of a satellite in the orbital coordinate system

DOI10.1134/S1063454121010027zbMath1479.70066OpenAlexW3159471383MaRDI QIDQ2038524

N. R. Andriyanova, Alekseĭ Aleksandrovich Tikhonov, Alexander Yurjevich Aleksandrov

Publication date: 7 July 2021

Published in: Vestnik St. Petersburg University. Mathematics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1134/s1063454121010027

zbMATH Keywords

satellitestabilizationasymptotic stabilityLyapunov function methodrotary motion

Mathematics Subject Classification ID

Stability of solutions to ordinary differential equations (34D20) Orbital mechanics (70M20)

Cites Work

• Electrodynamic attitude stabilization of a satellite in the Konig frame
• Parametric control in the problem of spacecraft stabilization in the geomagnetic field
• The stability of equilibrium of nonstationary systems
• Some questions of the qualitative theory of ordinary differential equations and dynamics of a rigid body interacting with a medium
• Uniaxial attitude stabilization of a rigid body under conditions of nonstationary perturbations with zero mean values
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