Linear problems of the stability of a ty
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A.P. Markeyev
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Article
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2008
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Elsevier Science
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English
⚖ 422 KB
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