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Integration of mechanism and control for large-angle slew maneuvers of flexible structuresA rolling contact noncircular gear system is applied to assist a desired controller in the slewing of a flexible space structure. The varying gear ratio in cooperation with the controller results in lower feedback gains at the controller, as well as considerably reducing flexural vibrations of the space structure. The noncircular gears consist of a pair of convex noncircular cylinders with specially designed profiles that are synthesized in conjunction with the optimal controller gains for minimizing the flexural vibrations of flexible structure during a slew maneuver. Convexity of the cylindrical profiles for this noncircular gear device must be ensured to maintain rolling contact between the two cylinders. Simulations of slewing control tasks for two kinds of flexible space structures, such as a planar flexible beam and the planar articulated flexible beams, are presented.
Document ID
19910008875
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Chew, Meng-Sang
(Old Dominion Univ. Norfolk, VA, United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1991
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-CR-187876
NAS 1.26:187876
Report Number: NASA-CR-187876
Report Number: NAS 1.26:187876
Accession Number
91N18188
Funding Number(s)
CONTRACT_GRANT: NAG1-952
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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