Analysis of Receiver Implementation Losses for GNSS Signals

This paper presents an analysis of the implementation losses, <tex>$L_{i m p}$</tex>, affecting a GNSS receiver. The implementation losses are the SNR loss at the correlator output due to payload and receiver imperfections with respect to an ideal case. <tex>$L_{\text {imp }}$</tex> is necessary to compute the link budget <tex>$C / N_{0}$</tex>, which must be compared to different <tex>$C / N_{0}$</tex> thresholds to guarantee the correct processing of a GNSS signal. This paper provides a physical meaning as well as a mathematical definition of the 4 terms constituting the implementation losses; moreover, a computation scheme is also derived where the elements (signal noise, receiver) affecting each of the 4 terms are highlighted. Finally, this paper applies the theory to GPS L5, Galileo E5a and SBAS L5 signals for a civil aviation receiver; different signal definitions are considered (frequency bounding of the power spectrum density) and numerical values are calculated; 0.7 dB can be expected for GPS and Galileo, and 1.27 dB for SBAS, plus the accommodation of the miscellaneous loss term.

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Publication Details

Published
2025-09-08
DOI
https://doi.org/10.23919/eusipco63237.2025.11226742
Primary Topic
GNSS positioning and interference
Type
article
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article

Analysis of Receiver Implementation Losses for GNSS Signals

Axel Garcia‐Pena, Christophe Macabiau
GNSS positioning and interference
article

Analysis of Receiver Implementation Losses for GNSS Signals

Axel Garcia‐Pena, Christophe Macabiau
article en

Abstract

This paper presents an analysis of the implementation losses, <tex>$L_{i m p}$</tex>, affecting a GNSS receiver. The implementation losses are the SNR loss at the correlator output due to payload and receiver imperfections with respect to an ideal case. <tex>$L_{\text {imp }}$</tex> is necessary to compute the link budget <tex>$C / N_{0}$</tex>, which must be compared to different <tex>$C / N_{0}$</tex> thresholds to guarantee the correct processing of a GNSS signal. This paper provides a physical meaning as well as a mathematical definition of the 4 terms constituting the implementation losses; moreover, a computation scheme is also derived where the elements (signal noise, receiver) affecting each of the 4 terms are highlighted. Finally, this paper applies the theory to GPS L5, Galileo E5a and SBAS L5 signals for a civil aviation receiver; different signal definitions are considered (frequency bounding of the power spectrum density) and numerical values are calculated; 0.7 dB can be expected for GPS and Galileo, and 1.27 dB for SBAS, plus the accommodation of the miscellaneous loss term.

École Nationale de l’Aviation Civile (FR)
Openalex Percentile: Top 50%
GNSS positioning and interference
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