Rotational Motion of a Non-Symmetrical Satellite with a Damper in a Circular Orbit


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In this paper, we report on a study of the effect of internal dissipation on the rotational motion of a nonsymmetrical satellite with a damper in a circular orbit using the Lavrent'ev model. Evolution equations are derived, and the stability of flat rotations of a satellite is studied. An evolution analysis of rotational motion depending on the parameter values and initial conditions is performed.

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N. Amel’kin

Moscow Institute of Physics and Technology

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Email: namelkin@mail.ru
俄罗斯联邦, Dolgoprudny, 141701

V. Kholoshchak

Moscow Institute of Physics and Technology

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Email: khoviktoriya@yandex.ru
俄罗斯联邦, Dolgoprudny, 141701

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