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Digital control system for space structural dampersA recently developed concept for a damper was improved by adding a small taper to the proof-mass, and using a proximeter to determine position. Also, an experimental damper was built using a three-inch stroke in place of the standard one-inch stroke. The analog controller initially used was replaced by an independent digital controller slaved to a TRS-80 Model I computer, which also serves as a highly effective, low-cost development system. An overall system concept for the use of proof-mass dampers is presented.
Document ID
19840008178
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Haviland, J. K.
(Virginia Univ. Charlottesville, VA, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1984
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-CR-175355
NAS 1.26:175355
UVA/52824/MAE84/101
Report Number: NASA-CR-175355
Report Number: NAS 1.26:175355
Report Number: UVA/52824/MAE84/101
Accession Number
84N16246
Funding Number(s)
CONTRACT_GRANT: NAG1-349
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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