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Digital receiver simulationDigital simulation of the data link for the Saturn-Uranus spacecraft design is summarized. The data link is a 40 watt, 400 MegaHertz, 44 bit-a-second link, a power starved link, and uses convolution coding. Aspects of the link of particular interest are atmospheric scintillation and the Doppler to data rate ratio. The major characteristics of the scintillation are modeled in terms of tapped delay lines. A candidate system design and receiver design is developed. A computer flow diagram depicting a routine for the error rate and one for acquisition is presented. Various coding algorithms are analyzed since the convolution code is sensitive to the distribution of error and the actual pattern of the error.
Document ID
19750012324
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hinrichs, C.
(McDonnell-Douglas Corp. Saint Louis, MO, United States)
Date Acquired
August 8, 2013
Publication Date
August 1, 1974
Publication Information
Publication: Dynatrend, Inc. Proc. of Outer Planet Probe Technol. Workshop, Sect. 1 through 11
Subject Category
Communications And Radar
Accession Number
75N20396
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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