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Control of acceleration in sine/random vibration testsSampling output levels of accelerometers using largest output or any combination of outputs provide control of shaker for spacecraft vibration qualification tests.
Document ID
19720000091
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Woodbury, R. C.
Date Acquired
August 6, 2013
Publication Date
January 1, 1972
Subject Category
Electronic Systems
Report/Patent Number
NPO-11482
Report Number: NPO-11482
Accession Number
72B10091
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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