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Minimizing Vibrations While Orienting Large StructuresAttitute error and error rate minimized by properly-designed control law. Control thrustor returns attitude to point within control dead band whenever attitude error or error rate strays outside. Within dead band, attitude drifts under environmental torque. Leftward thrustor fires when system phase point is to right of error dead band. Opposite is case for rightward thrustor.
Document ID
19820000301
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Austin, F.
(Grumman Aerospace Corp.)
Date Acquired
August 10, 2013
Publication Date
May 1, 1983
Publication Information
Publication: NASA Tech Briefs
Volume: 7
Issue: 2
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
MFS-25439
Report Number: MFS-25439
ISSN: 0145-319X
Accession Number
82B10301
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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