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IssuesArchive of Issues2025-3pp.1485-1499

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N.I. Amel’kin, "Spatial Resonant Rotations of a Three-Axis Satellite with a Ball Damper in a Circular Orbit," Mech. Solids. 60 (3), 1485-1499 (2025)
Year 2025 Volume 60 Number 3 Pages 1485-1499
DOI 10.1134/S0025654424607201
Title Spatial Resonant Rotations of a Three-Axis Satellite with a Ball Damper in a Circular Orbit
Author(s) N.I. Amel’kin (Moscow Institute of Physics and Technology, Dolgoprudny, 141701 Russia, namelkin@mail.ru)
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.
Keywords gravitational field, satellite with ball damper, averaging method, evolutionary equations, resonant rotations
Received 25 December 2024Revised 10 January 2025Accepted 10 January 2025
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