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Decoder synchronization for deep space missionsThe Consultative Committee for Space Data Standards (CCSDS) recommends that space communication links employ a concatenated, error-correcting, channel-coding system in which the inner code is a convolutional (7,1/2) code and the outer code is a (255,223) Reed-Solomon code. The traditional implementation is to perform the node synchronization for the Viterbi decoder and the frame synchronization for the Reed-Solomon decoder as separate, sequential operations. This article discusses a unified synchronization technique that is required for deep space missions that have data rates and signal-to-noise ratios (SNR's) that are extremely low. This technique combines frame synchronization in the bit and symbol domains and traditional accumulated-metric growth techniques to establish a joint frame and node synchronization. A variation on this technique is used for the Galileo spacecraft on its Jupiter-bound mission.
Document ID
19940025161
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Statman, J. I.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Cheung, K.-M.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Chauvin, T. H.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Rabkin, J.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Belongie, M. L.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 6, 2013
Publication Date
February 15, 1994
Publication Information
Publication: The Telecommunications and Data Acquisition Report
Subject Category
Communications And Radar
Accession Number
94N29664
Funding Number(s)
PROJECT: RTOP 314-30-61-02-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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