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Automatic gain controlAn automatic gain control (AGC), designed to operate with the prototype Loran-C receiver, is described. The device is used to eliminate error which occurs when signals are received at different magnitudes. The automatic gain control is a three transistor circuit which requires a constant dc voltage of 8 volts. Tests conclude that this value may be in the range of 4 to 12 v without change in circuit performance. Two transistors are cascaded to pass and amplify the input signal. Their gain is controlled by a third transistor which itself is controlled by an external AGC voltage between 0 and 8 volts dc. The integrated circuit used is an 8 pin chip, which is a differential cascade amplifier designed for use in communications operating at frequencies from dc to 120 MHz. The integrated circuit was balanced for AGC capabilities, and has a wide operating current range. The maximum input current at pins 1 and 5 is 0.1 mAmps. AGC testing is described.
Document ID
19810011525
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Roman, J. P.
(Ohio Univ. Athens, OH, United States)
Date Acquired
September 4, 2013
Publication Date
March 1, 1981
Subject Category
Aircraft Communications And Navigation
Report/Patent Number
NASA-CR-164081
TM-79
Report Number: NASA-CR-164081
Report Number: TM-79
Accession Number
81N20053
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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