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IssuesArchive of Issues2019-2pp.204-210

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E.V. Sadovnikova and A.V. Shatina, "Spin-Orbital Resonance Motion of a Satellite with Two Flexible Viscoelastic Rods in an Elliptical Orbit," Mech. Solids. 54 (2), 204-210 (2019)
Year 2019 Volume 54 Number 2 Pages 204-210
DOI 10.3103/S0025654419030208
Title Spin-Orbital Resonance Motion of a Satellite with Two Flexible Viscoelastic Rods in an Elliptical Orbit
Author(s) E.V. Sadovnikova (Moscow Technological University (MIREA), Moscow, 119454 Russia, sadovnikova-e@mail.ru)
A.V. Shatina (Moscow Technological University (MIREA), Moscow, 119454 Russia, shatina_av@mail.ru)
Abstract The present work is aimed at studying the rotational motion of a satellite in a central force field in an elliptical orbit. A satellite is simulated by a dynamically symmetrical solid body with flexible viscoelastic rods, firmly fastened along the symmetry axis. In the absence of strain in the rods, the central ellipsoid of inertia of the satellite has a spherical shape. The averaged set of equations of perturbed motion near a 1 : 1 resonance at small eccentricities is obtained. Capture in a 1 : 1 spin-orbital resonance is substantiated.
Keywords satellite, central force field, dissipation, resonance
Received 11 July 2017
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