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Optical gyroscopeInstrument uses phase difference between two beams of light to measure rotation. It is considerably simpler and more reliable than conventional spinning-mass gyroscopes used for inertial guidance and is more compact, lighter, and potentially less expensive. Moreover, optical gyroscope requires no warmup period. Although conceived for spacecraft and satellite stabilization, gyroscope should also find applications in flight instruments for private, commercial, and military aircraft.
Document ID
19780000176
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Goldstein, R. M.
Goss, W. C.
Date Acquired
August 9, 2013
Publication Date
October 1, 1978
Publication Information
Publication: NASA Tech Briefs
Volume: 3
Issue: 2
ISSN: 0145-319X
Subject Category
Physical Sciences
Report/Patent Number
NPO-14258
Accession Number
78B10176
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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