Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
1716773 | Acta Astronautica | 2008 | 15 Pages |
The dynamics of certain multi-tethered satellite formations containing a parent (or central) body are examined in this paper. Some simplifications are made prior to the analysis: the satellites are point-masses, the tethers are massless and straight, and the motion of the parent body of the formations is prescribed. First, planar formations are investigated: these are termed “hub-and-spoke”—which comprises a parent body located at the center (hub) of the formation, from which stem tethers (spokes), each having a satellite at its end—and “closed-hub-and-spoke” (which has the same description but also has, in addition, tethers joining successive satellites). These formations are placed in the orbital plane, or in the Earth-facing plane normal to the orbit, and are given an initial spin rate about an axis orthogonal to their nominal plane. The ensuing motion is studied in order to ascertain the conditions under which the formations remain in dynamic stability. Later, the motion of three-dimensional configurations, whose initial spin vector is along the radial direction, is examined. These formations are deployed along the local vertical. They are a “closed-hub-and-spoke” formation, which is found to be unstable and a “double-pyramid” configuration, which is found to be stable.