Abstract

Ionospheric delay is a critical error source in Global Navigation Satellite Systems (GNSSs) and a principal aspect of Satellite Based Augmentation System (SBAS) corrections. Grid Ionospheric Vertical Delays (GIVDs) are derived from the delays on Ionosphere Pierce Points (IPPs), which are observed by SBAS reference stations. SBAS master stations calculate ionospheric delay corrections by several methods, such as planar fit or Kriging. However, when there are not enough IPPs around an Ionosphere Grid Point (IGP) or the IPPs are unevenly distributed, the fitting accuracy of planar fit or Kriging is unsatisfactory. Moreover, the integrity bounds of Grid Ionospheric Vertical Errors (GIVEs) are overly conservative. Since Artificial Neural Networks (ANNs) are widely used in ionospheric research due to their self-adaptation, parallelism, non-linearity, robustness, and learnability, the ANN method for GIVD and GIVE derivation is proposed in this article. Networks are separately trained for IGPs, and five years of historical data are applied on network training. Principal Component Analysis (PCA) is applied for dimensionality reduction of geomagnetic and solar indices, which is employed as a network input feature. Furthermore, the GIVE algorithm of the ANN method is derived based on the distribution of the residual random variable. Finally, experiments are conducted on 12 IGPs over the East China region. Under normal ionospheric conditions, compared with the planar fit and Kriging methods, the residual reduction of the ANN method is approximately 15%. The ANN method fits the ionospheric delay residual error better. The percentage of GIVE availability under 2.7 m increases at least 25 points in comparison to Kriging. Under disturbed conditions, due to a lack of training samples, the ANN method is incompetent compared with planar fit or Kriging.

Highlights

  • Global Navigation Satellite System (GNSS)-based positioning services have been extensively used in Safety-of-Life (SoL) aeronautical applications, containing aircraft en route navigation, precision approach, and automatic landing

  • Networks are separately trained for Ionosphere Grid Point (IGP), and five years of historical data are applied on network training

  • The positioning performance of fundamental GNSS services is restricted by various error sources: satellite orbit error, satellite clock error, and ionospheric delay correction error, which make it unable to meet the requirements placed on accuracy, integrity, availability, and continuity of GNSSs for civil aviation users [1,2]

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Summary

Introduction

Global Navigation Satellite System (GNSS)-based positioning services have been extensively used in Safety-of-Life (SoL) aeronautical applications, containing aircraft en route navigation, precision approach, and automatic landing. The positioning performance of fundamental GNSS services is restricted by various error sources: satellite orbit error, satellite clock error, and ionospheric delay correction error, which make it unable to meet the requirements placed on accuracy, integrity, availability, and continuity of GNSSs for civil aviation users [1,2] To this end, many countries and regions have established their Satellite-Based Augmentation System (SBAS) to provide GNSS users with additional differential correction information: satellite orbit correction, satellite clock correction, and ionospheric delay correction, and with integrity augmentation information: User Differential Range Error (UDRE) and Grid Ionospheric Vertical Error (GIVE) [3]. SBASs under construction include the Korean Augmentation Satellite System (KASS) and Chinese BeiDou SBAS (BDSBAS) [5,8]

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