Abstract

The differential code bias (DCB) of the Global Navigation Satellite Systems (GNSS) receiver should be precisely corrected when conducting ionospheric remote sensing and precise point positioning. The DCBs can usually be estimated by the ground GNSS network based on the parameterization of the global ionosphere together with the global ionospheric map (GIM). In order to reduce the spatial-temporal complexities, various algorithms based on GIM and local ionospheric modeling are conducted, but rely on station selection. In this paper, we present a recursive method to estimate the DCBs of Global Positioning System (GPS) satellites based on a recursive filter and independent reference station selection procedure. The satellite and receiver DCBs are estimated once per local day and aligned with the DCB product provided by the Center for Orbit Determination in Europe (CODE). From the statistical analysis with CODE DCB products, the results show that the accuracy of GPS satellite DCB estimates obtained by the recursive method can reach about 0.10 ns under solar quiet condition. The influence of stations with bad performances on DCB estimation can be reduced through the independent iterative reference selection. The accuracy of local ionospheric modeling based on recursive filter is less than 2 Total Electron Content Unit (TECU) in the monthly median sense. The performance of the recursive method is also evaluated under different solar conditions and the results show that the local ionospheric modeling is sensitive to solar conditions. Moreover, the recursive method has the potential to be implemented in the near real-time DCB estimation and GNSS data quality check.

Highlights

  • Nowadays, Global Navigation Satellite Systems (GNSS) observations provide various ways to estimate geophysical parameters, and one of the most important parameters is the total electron content (TEC) measurements for Earth’s ionosphere research [1,2,3,4,5,6]

  • We present a recursive method to estimate the differential code bias (DCB) of Global Positioning System (GPS) satellites based on a recursive filter and independent reference station selection procedure

  • It is necessary to point out that the zero-mean condition can vary with respect to the observable satellites, which may lead to a drift in DCB estimates with respect to DCB products provided by some international GNSS service (IGS) analysis centers like Center for Orbit Determination in Europe (CODE)

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Summary

Introduction

Global Navigation Satellite Systems (GNSS) observations provide various ways to estimate geophysical parameters, and one of the most important parameters is the total electron content (TEC) measurements for Earth’s ionosphere research [1,2,3,4,5,6]. Apart from the commonly adopted method by setting the DCB as a constant during the GNSS TEC estimation [10,11,12,13,14,15], some other algorithms are proposed to decrease the computation costs by utilizing global ionospheric maps [4]. Sarma et al [32] proposed an algorithm based on singular value decomposition to estimate three receiver biases Among all these methods, several fundamental assumptions are adopted. While these single-layer TEC models may adopt different ionospheric effective heights, ranging from 350 to 450 km according to the spatial and temporal variation of the electron maximum height of the F2 layer Another assumption is that both satellite and receiver DCBs are constant during a single day.

Carrier Phase Smoothing Pseudorange
Local Ionospheric Modeling
Model Initialization and Propagation
Recursive Filter
Experimental Data
Evaluation of Local Ionospheric TEC Modeling
Dependence on Solar Condition
Full Text
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