Abstract

Space-based augmentation system (SBAS) provides correction information for improving the global navigation satellite system (GNSS) positioning accuracy in real-time, which includes satellite orbit/clock and ionospheric delay corrections. At SBAS service area boundaries, the correction is not fully available to GNSS users and only a partial correction is available, mostly satellite orbit/clock information. By using the geospatial correlation property of the ionosphere delay information, the ionosphere correction coverage can be extended by a spatial extrapolation algorithm. This paper proposes extending SBAS ionosphere correction coverage by using a biharmonic spline extrapolation algorithm. The wide area augmentation system (WAAS) ionosphere map is extended and its ionospheric delay error is compared with the GPS Klobuchar model. The mean ionosphere error reduction at low latitude is 52.3%. The positioning accuracy of the extended ionosphere correction method is compared with the accuracy of the conventional SBAS positioning method when only a partial set of SBAS corrections are available. The mean positioning error reduction is 44.8%, and the positioning accuracy improvement is significant at low latitude.

Highlights

  • Global navigation satellite system (GNSS) positioning accuracy is limited by variousGNSS error sources; satellite orbit error, satellite clock error, and ionospheric delay among others

  • This paper proposes a spatial extrapolation algorithm for Space-based augmentation systems (SBAS) ionosphere corrections

  • The availability was analyzed with one month of SBAS

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Summary

Introduction

Global navigation satellite system (GNSS) positioning accuracy is limited by various. GNSS error sources; satellite orbit error, satellite clock error, and ionospheric delay among others. External correction data can be used to reduce the effect of those error sources. SBAS uses Global Positioning System (GPS)-compatible signals that make it easy to add SBAS signal reception capabilities to GPS receivers without significant hardware modifications. In addition to the correction data, SBAS provides integrity information for the position error bound. This integrity information consists of the error covariance of each correction, orbit, clock, and ionosphere. Those covariances are used to determine measurement weightings during the positioning process and are used to determine error bound estimation. An SBAS-aided GNSS can determine whether to use GNSS or not

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