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Active damping of vibrations in SCOLE excited by slewingControl simulations were performed to study active damping of vibrations in SCOLE excited by minimum-time rapid slewing. Highlights of the numerical results are presented. Some conclusions reached are: (1) modal-dashpot and modal-spring controllers provide quick and effective vibration control; (2) high gain problems can be avoided by proper selection of modeled modes and proper level of augmentation; (3) modal dashpots and modal springs are most effective during the initial period of large vibrations; and (4) line of sight error due solely to each mode excited by the disturbance provides a sound measure of importance of individual modes.
Document ID
19870008398
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lin, Jiguan Gene
(Control Research Corp. Lexington, MA, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1987
Publication Information
Publication: NASA. Langley Research Center Proceedings of the 3rd Annual SCOLE Workshop
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
87N17831
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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