 | | Journal of Applied
Mathematics and Mechanics
Russian Academy of Sciences | | Founded
in January 1936
(Translated from 1958)
Issued 6 times a year
ISSN 0021-8928
(print version) |
Archive of Issues
| Total articles in the database: | | 10512 |
| In Russian (ΟΜΜ): | | 9713
|
| In English (J. Appl. Math. Mech.): | | 799 |
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| << Previous article | Volume 81, Issue 6 / 2017 | Next article >> |
| N.I. Amelkin and V.V. Kholoshchak, "Steady rotations of a satellite with internal elastic and dissipative forces," J. Appl. Math. Mech. 81 (6), 431-441 (2017) |
| Year |
2017 |
Volume |
81 |
Issue |
6 |
Pages |
431-441 |
| DOI |
10.1016/j.jappmathmech.2018.03.011 |
| Title |
Steady rotations of a satellite with internal elastic and dissipative forces |
| Author(s) |
N.I. Amelkin (Moscow Institute of Physics and Technology, Dolgoprudnyi, Russia, namelkin@mail.ru)
V.V. Kholoshchak (Moscow Institute of Physics and Technology, Dolgoprudnyi, Russia, khoviktoriya@yandex.ru) |
| Abstract |
Lavrent'ev's model (a satellite is simulated by a rigid shell with a spherical damper) is used to study the effect of internal forces on the motion of a satellite in a central gravitational field assuming that both dissipative and elastic internal forces arise with relative displacements of the damper. All the steady rotations are determined within the framework of this model for a dynamically symmetric satellite in a circular orbit and their stability is investigated as a function of the values of the damping and stiffness coefficients. |
| Keywords |
rigid body; inertia tensor in a circular orbit; orbital plane; dissipative torque; gravitational torque |
| Received |
19 January 2017 |
| Link to Fulltext |
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