EVOLUTION OF THE ROTATIONAL MOTION OF A SATELLITE WITH FLEXIBLE VISCOELASTIC RODS ON THE ELLIPTIC ORBIT

EVOLUTION OF THE ROTATIONAL MOTION OF A SATELLITE WITH FLEXIBLE VISCOELASTIC RODS ON THE ELLIPTIC ORBIT

The rotational motion of an artificial satellite in the central Newtonian force field is investigated. The satellite is modeled as a symmetric solid with rigid viscoelastic rods rigidly attached along the symmetry axis and with a spherical inertia tensor. A limited statement of the problem is consid...

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Bibliographic Details
Main Authors: E. V. Sadovnikova, A. V. Shatina
Format: Article
Language:Russian
Published: MIREA - Russian Technological University 2018-08-01
Series:Российский технологический журнал
Subjects:
satellite
kepler elliptic orbit
andoyer variables
averaging method
dissipative evolution of motion
Online Access:https://www.rtj-mirea.ru/jour/article/view/121

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