| | 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
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In English (J. Appl. Math. Mech.): | | 799 |
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<< Previous article | Volume 72, Issue 3 / 2008 | Next article >> |
A.P. Markeyev, "Linear problems of the stability of a type of rotation of a satellite about the centre of mass," J. Appl. Math. Mech. 72 (3), 250-258 (2008) |
Year |
2008 |
Volume |
72 |
Issue |
3 |
Pages |
250-258 |
Title |
Linear problems of the stability of a type of rotation of a satellite about the centre of mass |
Author(s) |
A.P. Markeyev (Moscow, Russia, markeev@ipmnet.ru) |
Abstract |
The stability in the first approximation of the rotation of a satellite about a centre of mass is investigated. In the unperturbed motion the satellite performs, in absolute space, three rotations around the normal to the orbital plane in a time equal to two periods of rotation of its centre of mass in the orbit (Mercury-type rotation). Three cases of such rotations are considered: the rotations of a dynamically symmetrical satellite and a satellite, the central ellipsoid of inertia of which is close to a sphere, in an elliptic orbit of arbitrary eccentricity, and the rotation of a satellite with three different principal central moments of inertia in a circular orbit. |
Received |
25 September 2007 |
Link to Fulltext |
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