4.6 Article

Handling the satellite inter-frequency biases in triple-frequency observations

期刊

ADVANCES IN SPACE RESEARCH
卷 59, 期 8, 页码 2048-2057

出版社

ELSEVIER SCI LTD
DOI: 10.1016/j.asr.2017.02.002

关键词

Precise satellite clock; GNSS biases; Inter-frequency clock bias; Differential code biases; BeiDou Navigation Satellite System

资金

  1. National Science Fund for Distinguished Young Scholars [41525014]
  2. National 973 Program of China [2012CB957701]
  3. National Natural Science Foundation of China [41074008]
  4. Research Fund for the Doctoral Program of Higher Education of China [20120141110025]
  5. Non-profit Industry Financial Program of MWR [201401072]

向作者/读者索取更多资源

The new generation of GNSS satellites, including BDS, Galileo, modernized GPS, and GLONASS, transmit navigation sdata at more frequencies. Multi-frequency signals open new prospects for precise positioning, but satellite code and phase inter-frequency biases (IFB) induced by the third frequency need to be handled. Satellite code IFB can be corrected using products estimated by different strategies, the theoretical and numerical compatibility of these methods need to be proved. Furthermore, a new type of phase IFB, which changes with the relative sun spacecraft earth geometry, has been observed. It is necessary to investigate the cause and possible impacts of phase Time-variant IFB (TIFB). Therefore, we present systematic analysis to illustrate the relevancy between satellite clocks and phase TIFB, and compare the handling strategies of the code and phase IFB in triple-frequency positioning. First, the un-differenced L1/L2 satellite clock corrections considering the hardware delays are derived. And IFB induced by the dual-frequency satellite clocks to triple-frequency PPP model is detailed. The analysis shows that estimated satellite clocks actually contain the time-variant phase hardware delays, which can be compensated in Ll/L2 ionosphere-free combinations. However, the time-variant hardware delays will lead to TIFB if the third frequency is used. Then, the methods used to correct the code and phase IFB are discussed. Standard point positioning (SPP) and precise point positioning (PPP) using BDS observations are carried out to validate the improvement of different IFB correction strategies. Experiments show that code IFB derived from DCB or geometry-free and ionosphere-free combination show an agreement of 0.3 ns for all satellites. Positioning results and error distribution with two different code IFB correcting strategies achieve similar tendency, which shows their substitutability. The original and wavelet filtered phase TIFB long-term series show significant periodical characteristic for most GEO and IGSO satellites, with the magnitude varies between 5 cm and 5 cm. Finally, BDS Ll/L3 kinematic PPP is conducted with code IFB corrected with DCB combinations, and TIFB corrected with filtered series. Results show that the IFB corrected Ll/L3 PPP can achieve comparable convergence and positioning accuracy as Ll/L2 combinations in static and kinematic mode. (C) 2017 COSPAR. Published by Elsevier Ltd. All rights reserved.

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