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Intermediate accuracy integrating gyroscopes - Design criteria monographSingle degree of freedom, floated, intermediate accuracy, integrating gyroscope state of the art and design criteria for spacecraft control applications
Document ID
19700030457
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Haagens, R. G. (Little (Arthur D.), Inc. Cambridge, MA, United States)
Date Acquired
September 2, 2013
Publication Date
June 1, 1970
Subject Category
Instrumentation And Photography
Report/Patent Number
NASA-CR-113572
Report Number: NASA-CR-113572
Accession Number
70N39773
Funding Number(s)
CONTRACT_GRANT: NAS12-2077
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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