Abstract

This paper presents observations on the WAAS L1 and L5 signals quality and their impact on the robustness of the navigation solution by quantifying the contributions of each broadcasted differential correction. This work is undertaken with the intent of defining performance benefits of L5 by dual frequency WAAS users and is to provide useful material for Minimum Operational Performance Standard (MOPS) development. In this perspective, a study of the WAAS signal characteristics is first carried out. The information gathered is then used to compare various GPS solutions in terms of frequency diversity, satellite diversity, pseudorange noise and different signal corrections and their impacts. These solutions are compared against a reference standalone GPS solution. All statistics are computed with respect to a post-processed Novatel Waypoint Real-Time Kinematics (RTK) GPS L1/L2 semi-codeless static solution, considered as the reference. A discussion on some simplifications with respect to specifications (i.e. MOPS) that could be considered by receiver manufacturers closes the paper. It is confirmed that the current WAAS navigation message definition is the same on both the L1 and L5 frequencies, the latter further being Manchester coded, thus avoiding data ambiguity. The +5 dB SNR on L5 has minor impacts in terms of reliability and continuous availability in the presented scenarios, but would become especially beneficial in hostile environments, despite a greater number of pulsed interferers. Another demonstration is that the WAAS message varies slightly from one WAAS satellite to another, even if corrections are generated centrally. Finally, it is observed that WAAS and GPS signals pseudorange noise are comparable on a “per frequency” basis.

Highlights

  • The civil international aircraft industry constantly seeks for satellite navigation performance improvements

  • The purpose of this paper is to provide an overview of the actual status of Wide Area Augmentation System (WAAS) signal precision and integrity on both L1 and L5, there are no plans for a WAAS L5 service; current WAASL5 signals are not officially declared online by the Federal Aviation Administration (FAA) [12]

  • Most results were related to the WAAS signal characteristics, the navigation message and the integration of the provided corrections, as opposed to previous work focused on the inclusion of WAAS pseudoranges in the navigation solution found in [13] [39], or to the WAAS L5 used in a L5-only PVT solution in [16]

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Summary

Introduction

The civil international aircraft industry constantly seeks for satellite navigation performance improvements. The most obvious effect of SBAS became to annihilate the Selective Availability (SA), which could be differentially corrected [2] This intended degradation of the signal quality with military purposes has been discontinued since May 2000; new GPS III satellites should no longer include SA capability, since it has been permanently deactivated [3]. The latest 8-year-old Minimum Operational Performance Standard (MOPS) [5] could be re-visited in terms of general SBAS implementation rules with an up-to-date environment (e.g. considering SA has completely been deactivated and will not come back) This is important since GPS L1 cannot satisfy performance required by Federal Aviation Administration (FAA) for various phases of flight on its own, especially for approach with vertical guidance. A robustness analysis of different WAAS signals is presented before a short discussion and conclusive remarks

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