Abstract

The International GNSS Service (IGS) real-time service (RTS) provides access to real-time precise products. State-Space Representation (SSR) products are disseminated through the Internet using the Networked Transport of the RTCM (Radio Technical Commission for Maritime Services) via the Internet Protocol (NTRIP). However, communication outages caused by a loss of the communication link during ephemeris changes can occur. Unfortunately, any break in providing orbit and clock corrections affects the possibility to perform precise point positioning. To eliminate this problem, various methods have been developed and presented in the literature. The solution proposed by the authors is to directly predict geocentric corrections. This manuscript presents the results and analysis of geocentric correction predictions under two scenarios: the first between the IODE (issue of data ephemeris) value change and the second where prediction must be done for epochs containing a change in IODE ephemeris. In this case, the prediction uses data from a previous message. The Root Mean Square (RMS) values calculated based on the differences between the true correction values and the predicted geocentric corrections using a linear function, a second-degree polynomial and a constant value do not differ significantly. The numerical results show that, in most cases, maintaining the constant value of the last registered SSR correction is the best option.

Highlights

  • In the past few years, precise point positioning (PPP) has received a significant amount of attention in the GNSS community

  • The original geocentric corrections calculated based on the original State-Space Representation (SSR) are presented in blue

  • An extrapolation was performed based on 65 min of data as the maximum registered time of the data-stream

Read more

Summary

Introduction

In the past few years, precise point positioning (PPP) has received a significant amount of attention in the GNSS community. PPP can be an effective option for precise real-time positioning, but it requires more information than GNSS observations alone. Reliable satellite orbit and clock corrections [1,2,3,4,5], ionosphere [6] and troposphere model parameters [7], and antenna phase center offsets and variations must be provided in order to obtain precise results [8]. To provide maximum orbit accuracy in post processing PPP, precise orbit files (SP3) are usually used. Since ultra-rapid orbits and satellite clocks are available 3–9 h after observations, and final orbits are available 12–18 days after the observation time, this approach is not applicable to real time positioning

Methods
Results
Conclusion
Full Text
Published version (Free)

Talk to us

Join us for a 30 min session where you can share your feedback and ask us any queries you have

Schedule a call