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NASA NTRS ยท 19840000004

Tuning Concept for Resonant Cavities

Abstract

Deviations 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.

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BibTeXRIS

Sydnor, R. L.. 1985-01-01. Tuning Concept for Resonant Cavities. https://ntrs.nasa.gov/citations/19840000004

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