| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 1716771 | Acta Astronautica | 2008 | 9 Pages |
Abstract
Dynamics and control of two-body and nn-body tethered satellites are considered. At first, nonlinear roll and pitch motions of two-body systems are examined. Then the effects of aerodynamic and electrodynamic forces on the stability of a tethered satellite are discussed. Various control schemes to stabilize the dynamics during retrieval of the subsatellite are described. Finally, some dynamics and stability results for nn-body tethered satellites are presented.
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Physical Sciences and Engineering
Engineering
Aerospace Engineering
Authors
A.K. Misra,