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Dynamic characterization and microprocessor control of the NASA/UVA proof mass actuatorThe self-contained electromagnetic-reaction-type force-actuator system developed by NASA/UVA for the verification of spacecraft-structure vibration-control laws is characterized and demonstrated. The device is controlled by a dedicated microprocessor and has dynamic characteristics determined by Fourier analysis. Test data on a cantilevered beam are shown.
Document ID
19840048960
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Zimmerman, D. C. (State Univ. of New York Buffalo, NY, United States)
Inman, D. J. (New York, State University Buffalo, NY, United States)
Horner, G. C. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1984
Subject Category
Ground Support Systems And Facilities (Space)
Report/Patent Number
AIAA PAPER 84-1077
Report Number: AIAA PAPER 84-1077
Accession Number
84A31747
Funding Number(s)
CONTRACT_GRANT: NGT-33-183-801
Distribution Limits
Public
Copyright
Other

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