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Commutated automatic gain control systemA commutated automatic gain control (AGC) system was designed and built for a prototype Loran C receiver. The receiver uses a microcomputer to control a memory aided phase-locked loop (MAPLL). The microcomputer also controls the input/output, latitude/longitude conversion, and the recently added AGC system. The circuit designed for the AGC is described, and bench and flight test results are presented. The AGC circuit described actually samples starting at a point 40 microseconds after a zero crossing determined by the software lock pulse ultimately generated by a 30 microsecond delay and add network in the receiver front end envelope detector.
Document ID
19820009266
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Yost, S. R.
(Ohio Univ. Athens, OH, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1982
Subject Category
Aircraft Communications And Navigation
Report/Patent Number
NASA-CR-168440
TM-81
Report Number: NASA-CR-168440
Report Number: TM-81
Accession Number
82N17140
Funding Number(s)
CONTRACT_GRANT: NGR-36-009-017
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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