Attitude stability of artificial satellites subject to gravity gradient torque

DOI10.1007/S10569-009-9216-3zbMath1204.70025OpenAlexW2096083916MaRDI QIDQ1038757

Regina Elaine Santos Cabette, Rodolpho Vilhena de Moraes, Teresinha J. Stuchi, Maria Cecília F. P. S. Zanardi, Jorge Kennety Silva Formiga

Publication date: 20 November 2009

Published in: Celestial Mechanics and Dynamical Astronomy (Search for Journal in Brave)

Full work available at URL: http://urlib.net/J8LNKAN8RW/36GB4TP

zbMATH Keywords

nonlinear stabilitynormalizationrotational motion of artificial satellites

Mathematics Subject Classification ID

Orbital mechanics (70M20)

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Cites Work

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• Canonical perturbation theories. Degenerate systems and resonance
• Investigation of equilibria of a satellite subjected to gravitational and aerodynamic torques
• Some properties of the dumbbell satellite attitude dynamics
• Stability of Hamiltonian systems with three degrees of freedom and the three body-problem
• On the stability of uniform rotations of a rigid body around the principal axis
• Stability of uniform rotations of a rigid body about a principal axis
• Equilibria of a satellite subjected to gravitational and aerodynamic torques with pressure center in a principal plane of inertia
• Study of the terms of coupling between rotational and translational motions
• Gravity effects on the rotational motion of a uniaxial artificial satellite.

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