Attitude stability of rigid satellites via a normalized Hamiltonian

DOI10.1016/0094-5765(89)90025-8zbMath0671.70017OpenAlexW2017863475MaRDI QIDQ3823844

S. R. Marandi, V. J. Modi

Publication date: 1989

Published in: Acta Astronautica (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0094-5765(89)90025-8

zbMATH Keywords

KAM theorycanonical transformationsflexible satellitesattitude stability of a rigid satellite in a circular orbitlinearized techniquesstability analysis of higher order conservative systems

Mathematics Subject Classification ID

Computational methods for problems pertaining to mechanics of particles and systems (70-08) Orbital mechanics (70M20) Canonical and symplectic transformations for problems in Hamiltonian and Lagrangian mechanics (70H15)

Related Items (1)

Nonlinear Stability in the Spatial Attitude Motion of a Satellite in a Circular Orbit

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