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Abstract <p>For a three-axis satellite with a ball damper, resonant rotations in the central gravitational field are studied. The equations of the rotational motion of a satellite in an elliptical orbit are obtained. For the case of a circular orbit, spatial resonance rotations of 1 : 1 and 2 : 1 were investigated using the averaging method.</p>

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Spatial Resonant Rotations of a Three-Axis Satellite with a Ball Damper in a Circular Orbit

  • 期刊论文

  • 发表日期：

    2025年6月1日

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  • N. I. Amel’kin

摘要

Abstract

For a three-axis satellite with a ball damper, resonant rotations in the central gravitational field are studied. The equations of the rotational motion of a satellite in an elliptical orbit are obtained. For the case of a circular orbit, spatial resonance rotations of 1 : 1 and 2 : 1 were investigated using the averaging method.