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Flight test of 4-Hz and 30-Hz Omega receiver front-endIn-flight information was gathered on two Omega receiver analog modules, one having a 4-Hz bandwidth and the other a 30-Hz bandwidth. The Mini-O receiver was also monitored. An improved signal-to-noise characteristic of the narrower bandwidth front-end with negligible loss in dynamic range indicates that the 4-Hz front-end is the more desirable for the prototype Omega receivers. The Mini-O receiver was found to function quite satisfactorily on its second test flight, and has a very real potential for a low-cost, low-power, compact and light-weight Omega receiver.
Document ID
19760009997
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Wright, L.
(Ohio Univ. Athens, OH, United States)
Date Acquired
September 3, 2013
Publication Date
February 1, 1976
Subject Category
Aircraft Communications And Navigation
Report/Patent Number
REPT-21
NASA-CR-146383
Report Number: REPT-21
Report Number: NASA-CR-146383
Accession Number
76N17085
Funding Number(s)
CONTRACT_GRANT: NGR-36-009-107
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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