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


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Abstract

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.

About the authors

N. I. Amel’kin

Moscow Institute of Physics and Technology

Author for correspondence.
Email: namelkin@mail.ru
Russian Federation, Dolgoprudny, 141701

V. V. Kholoshchak

Moscow Institute of Physics and Technology

Author for correspondence.
Email: khoviktoriya@yandex.ru
Russian Federation, Dolgoprudny, 141701

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