DocumentCode :
2769684
Title :
The role of margin in link design and optimization
Author :
Cheung, K.
Author_Institution :
Jet Propulsion Lab., Pasadena, CA, USA
fYear :
2015
fDate :
7-14 March 2015
Firstpage :
1
Lastpage :
11
Abstract :
Link analysis is a system engineering process in the design, development, and operation of communication systems and networks. Link models that are mathematical abstractions representing the useful signal power and the undesirable noise and attenuation effects (including weather effects if the signal path transverses through the atmosphere) that are integrated into the link budget calculation that provides the estimates of signal power and noise power at the receiver. Then the link margin is applied which attempts to counteract the fluctuations of the signal and noise power to ensure reliable data delivery from transmitter to receiver. (Link margin is dictated by the link margin policy or requirements.)A simple link budgeting approach assumes link parameters to be deterministic values typically adopted a rule-of-thumb policy of 3 dB link margin. This policy works for most Sand X-band links due to their insensitivity to weather effects. But for higher frequency links like Ka-band, Ku-band, and optical communication links, it is unclear if a 3 dB link margin would guarantee link closure. Statistical link analysis that adopted the 2-σ or 3-σ link margin incorporates link uncertainties in the σ calculation. (The Deep Space Network (DSN) link margin policies are 2-σ for downlink and 3-σ for uplink.) The link reliability can therefore be quantified statistically even for higher frequency links. However in the current statistical link analysis approach, link reliability is only expressed as the likelihood of exceeding the signal-to-noise ratio (SNR) threshold that corresponds to a given bit-error-rate (BER) or frame-error-rate (FER) requirement. The method does not provide the true BER or FER estimate of the link with margin, or the required signalto-noise ratio (SNR) that would meet the BER or FER requirement in the statistical sense. In this paper, we perform in-depth analysis on the relationship between BER/FER requirement, opera- ing SNR, and coding performance curve, in the case when the channel coherence time of link fluctuation is comparable or larger than the time duration of a codeword. We compute the “true” SNR design point that would meet the BER/FER requirement by taking into account the fluctuation of signal power and noise power at the receiver, and the shape of the coding performance curve. This analysis yields a number of valuable insights on the design choices of coding scheme and link margin for the reliable data delivery of a communication system - space and ground. We illustrate the aforementioned analysis using a number of standard NASA error-correcting codes.
Keywords :
electromagnetic wave attenuation; error correction codes; error statistics; radio receivers; space communication links; statistical analysis; telecommunication network reliability; wireless channels; Ka-band link; Ku-band link; S-band link; X-band link; attenuation effect; bit-error-rate requirement; channel coherence time; coding performance curve; communication system design; communication system development; communication system operation; data delivery reliability; deep space network link margin policies; frame-error-rate requirement; ground communication system; link budget calculation; link budgeting approach; link closure; link design; link fluctuation; link models; link uncertainties; mathematical abstractions; noise power estimation; noise power fluctuation; optical communication links; rule-of-thumb policy; signal power estimation; signal power fluctuation; signal-to-noise ratio threshold; space communication system; standard NASA error-correcting codes; statistical link analysis; system engineering process; undesirable noise effect; Bit error rate; Encoding; Meteorology; Receivers; Signal to noise ratio;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference, 2015 IEEE
Conference_Location :
Big Sky, MT
Print_ISBN :
978-1-4799-5379-0
Type :
conf
DOI :
10.1109/AERO.2015.7119220
Filename :
7119220
Link To Document :
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