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Turbo codes for deep-space communicationsTurbo codes were recently proposed by Berrou, Glavieux, and Thitimajshima, and it has been claimed these codes achieve near-Shannon-limit error correction performance with relatively simple component codes and large interleavers. A required E(b)/N(o) of 0.7 dB was reported for a bit error rate of 10(exp -5), using a rate 1/2 turbo code. However, some important details that are necessary to reproduce these results were omitted. This article confirms the accuracy of these claims, and presents a complete description of an encoder/decoder pair that could be suitable for deep-space applications, where lower rate codes can be used. We describe a new simple method for trellis termination, analyze the effect of interleaver choice on the weight distribution of the code, and introduce the use of unequal rate component codes, which yield better performance.
Document ID
19950015118
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Divsalar, D.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Pollara, F.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 6, 2013
Publication Date
February 15, 1995
Publication Information
Publication: The Telecommunications and Data Acquisition Report 29-39 (SEE N95-21532 06-32)
Subject Category
Communications And Radar
Accession Number
95N21535
Funding Number(s)
PROJECT: RTOP 315-91-20-20-53
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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