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Fiber Ring Optical Gyroscope (FROG)The design, construction, and testing of a one meter diameter fiber ring optical gyro, using 1.57 kilometers of single mode fiber, are described. The various noise components: electronic, thermal, mechanical, and optical, were evaluated. Both dc and ac methods were used. An attempt was made to measure the Earth rotation rate; however, the results were questionable because of the optical and electronic noise present. It was concluded that fiber ring optical gyroscopes using all discrete components have many serious problems that can only be overcome by discarding the discrete approach and adapting an all integrated optic technique that has the laser source, modulator, detector, beamsplitters, and bias element on a single chip.
Document ID
19800020189
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 4, 2013
Publication Date
December 31, 1979
Subject Category
Instrumentation And Photography
Report/Patent Number
NASA-CR-163387
PUBL-79-014
Report Number: NASA-CR-163387
Report Number: PUBL-79-014
Accession Number
80N28690
Funding Number(s)
CONTRACT_GRANT: JPL-954936
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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