Attitude dynamics of a dual-spin nanosatellite with a gravitational damper

Author:

Doroshin Anton V.ORCID,Eremenko Alexandr V.

Funder

Russian Science Foundation

Publisher

Elsevier BV

Reference42 articles.

1. Evolution of rotational motion of a planet in a circular orbit under the influence of internal elastic and dissipative forces;Amel’kin;Mech. Solids,2020

2. Rotational motion of a non-symmetrical satellite with a damper in a circular orbit;Amel’kin;Mech. Solids,2019

3. Stability of the steady rotations of a satellite with internal damping in a central gravitational field;Amelkin;J. Appl. Math. Mech.,2017

4. Applied celestial mechanics and motion control. Collection of articles dedicated to the 90th anniversary of the birth of D.E. Okhotsimsky / Compiled by: T.M. Eneev, M.Yu. Ovchinnikov, A.R. Golikov. - Moscow: IPM im. M.V. Keldysh, 2010. - 368 p. — ISBN 978-5-98354-007-1.

5. Active magnetic damping attitude control for gravity gradient stabilized spacecraft;Arduini;J. Guid. Control Dynam.,1997

Cited by 1 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Attitude Dynamics of a Composite Nanosatellite with a Gravitational Damper and with a Movable Unit on a Rail System;2024 X International Conference on Information Technology and Nanotechnology (ITNT);2024-05-20

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