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Tuning Concept for Resonant CavitiesDeviations from resonance detected by sampling phases. Automatic tuner feedback control system derives error signal from E and H plane probe signals. Control objective to maintain phase difference between E and H at 90 degrees. Technique estimated to sensitive to fractional frequency deviation of about 5 X 10-16 and applicable not only to masers but also other microwave elements, including klystrons, general purpose oscillators, and frequency standards.
Document ID
19840000004
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Sydnor, R. L.
(CALTECH)
Date Acquired
August 12, 2013
Publication Date
January 1, 1985
Publication Information
Publication: NASA Tech Briefs
Volume: 8
Issue: 3
ISSN: 0145-319X
Subject Category
Electronic Components And Circuits
Report/Patent Number
NPO-15890
Accession Number
84B10004
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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