Galileo orbit determination using combined GNSS and SLR observations

S. Hackel, P. Steigenberger, U. Hugentobler, M. Uhlemann, O. Montenbruck

Research output: Contribution to journalArticlepeer-review

48 Scopus citations

Abstract

The first two Galileo In-Orbit Validation satellites were launched in October 2011 and started continuous signal transmission on all frequencies in early 2012. Both satellites are equipped with two different types of clocks, namely rubidium clocks and hydrogen masers. Based on two test periods, the quality of the Galileo orbit determination based on Global Navigation Satellite System (GNSS) and Satellite Laser Ranging (SLR) observations is assessed. The estimated satellite clock parameters are used as quality indicator for the orbits: A bump at orbital periods in the Allan deviation indicates systematic errors in the GNSS-only orbit determination. These errors almost vanish if SLR observations are considered in addition. As the internal consistency is degraded by the combination, the offset of the SLR reflector is shifted by +5 cm, resulting in an improved orbit consistency as well as accuracy. Another approach to reduce the systematic errors of the GNSS-only orbit determination employs constraints for the clock estimates with respect to a linear model. In general, one decimeter orbit accuracy could be achieved.

Original languageEnglish
Pages (from-to)15-25
Number of pages11
JournalGPS Solutions
Volume19
Issue number1
DOIs
StatePublished - Jan 2014

Keywords

  • Galileo In-Orbit Validation (IOV)
  • Global Navigation Satellite System (GNSS)
  • Satellite Laser Ranging (SLR)
  • Satellite orbits

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