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Digital control system for space structural dampersDigital control systems for space structural dampers, also referred to as inertia or proof-mass dampers are investigated. A damper concept is improved by adding a small taper to the proof-mass, and using a proximeter to determine position. Another damper using a three inch stroke rather than the standard one inch stroke is described. Provisions are made for a relative velocity feedback. In one approach, the digital controller is modified to accept the signal from a linear velocity transducer. In the other, the velocity feedback is included in the digital program. An overall system concept for the use of the dampers is presented.
Document ID
19840023197
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
July 1, 1984
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NAS 1.26:173867
UVA/528224/MAE85/102
NASA-CR-173867
Report Number: NAS 1.26:173867
Report Number: UVA/528224/MAE85/102
Report Number: NASA-CR-173867
Accession Number
84N31267
Funding Number(s)
CONTRACT_GRANT: NAG1-349
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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