| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 8055764 | Acta Astronautica | 2018 | 7 Pages |
Abstract
Relative equilibria of a pendulum attached to the surface of a uniformly rotating celestial body are considered. The locations of the tether anchor that correspond to a given spacecraft position are defined. The domains, where the spacecraft can be held with the help of such a pendulum, are also described. Stability of the found relative equilibria is studied.
Related Topics
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Aerospace Engineering
Authors
Alexander A. Burov, Anna D. Guerman, Ivan I. Kosenko, Vasily I. Nikonov,