| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 7175593 | Journal of Applied Mathematics and Mechanics | 2017 | 10 Pages |
Abstract
The rotational motion of a satellite in a central gravitational field in the presence of internal dissipation is studied. The satellite is modelled by a system consisting of two bodies, a shell and a spherical damper. The stability of the steady rotations is investigated for a dynamically symmetric satellite moving in a circular Kepler orbit.
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Authors
N.I. Amelkin, V.V. Kholoshchak,