Resonant rotations of a dynamically symmetrical satellite with a ball damper in a circular orbit

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Abstract

For a satellite with a ball damper, the effect of internal dissipation on rotational motion in the central gravitational field is studied. The equations of rotational motion of a dynamically symmetric satellite with a spherical damper in an elliptical orbit are obtained. For the case of a circular orbit, the spatial resonance rotations of a dynamically symmetric satellite with a ball damper were investigated using the averaging method.

About the authors

N. I. Amel’kin

Moscow Institute of Physics and Technology

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

References

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