Solutions homoclinic to regular precessions of a symmetric satellite

DOI10.1007/BF00049515zbMath0831.70017WikidataQ104405246 ScholiaQ104405246MaRDI QIDQ1898001

Krzysztof Goździewski, Andrzej J. Maciejewski

Publication date: 20 September 1995

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

zbMATH Keywords

non-integrabilityrotational motioncircular orbitrigid satelliteseparatricesasymptotic manifolds

Mathematics Subject Classification ID

Dynamical aspects of finite-dimensional Hamiltonian and Lagrangian systems (37J99) Celestial mechanics (70F15) Orbital mechanics (70M20)

Related Items (2)

The Taylor series method for the problem of the rotational motion of a rigid satellite ⋮ Numerical evidence of nonintegrability of certain Lie-Poisson system

Cites Work

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• Stabilization due to gyroscopic coupling in dual-spin satellites subject to gravitational torques
• Attitude stability of a symmetric satellite at the equilibrium points in the restricted three-body problem

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