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Precession and circularization of elliptical space-tether motionIn this paper, we present a simplified analytic model for predicting motion of long space tethers. The perturbation model developed here addresses skip rope motion, where each end of the tether is held in place and the middle of the tether swings with a motion similar to that of a child's skip rope. If the motion of the tether midpoint is elliptical rather than circular, precession of the ellipse complicates the procedures required to damp this motion. The simplified analytic model developed in this paper parametrically predicts the precession of elliptical skip rope motion. Furthermore, the model shows that elliptic skip rope motion will circularize when damping is present in the longitudinal direction. Compared with high-fidelity simulation results, this simplified model provides excellent predictions of these phenomena.
Document ID
19930067320
Document Type
Conference Paper
Authors
Chapel, Jim D.
(Martin Marietta Astronautics Group Denver, CO, United States)
Grosserode, Patrick
(Orbital Sciences Corp. Chandler, AZ, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1993
Publication Information
Publication: In: AIAA Guidance, Navigation and Control Conference, Monterey, CA, Aug. 9-11, 1993, Technical Papers. Pt. 1 (A93-51301 22-63)
Publisher: American Institute of Aeronautics and Astronautics
Subject Category
Astrodynamics
Report/Patent Number
AIAA PAPER 93-3716
Accession Number
93A51317
Funding Number(s)
CONTRACT_GRANT: NAS8-3600
Distribution Limits
Public
Copyright
Other

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