Measuring Multipath Error of a Pseudo Quasi-Zenith Satellite

  • Tsujii, Toshiaki (Aviation Program Group, Japan Aerospace Exploration Agency) ;
  • Tomita, Hiroshi (Aviation Program Group, Japan Aerospace Exploration Agency) ;
  • Okuno, Yoshinori (Aviation Program Group, Japan Aerospace Exploration Agency) ;
  • Petrovski, Ivan (Institute of Advanced Satellite Positioning Technology, GNSS Technologies Inc.) ;
  • Asako, Masahiro (Institute of Advanced Satellite Positioning Technology, GNSS Technologies Inc.) ;
  • Okano, Kazuki (Institute of Advanced Satellite Positioning Technology, GNSS Technologies Inc.)
  • Published : 2006.10.18

Abstract

Japan has been investigating a new satellite based positioning system called Quasi-Zenith Satellite System (QZSS). Since the improvement of positioning availability in urban area is one of the most important advantages of the QZSS, multipath mitigation is a key factor for the QZSS positioning system. Therefore, Japan Aerospace Exploration Agency (JAXA) and GNSS Inc. have commenced the R&D of a pseudolite, which transmits the next-generation signal such as BOC(1,1), in order to evaluate the effect of multipath on the new signal. A prototype BOC pseudolite was developed in 2005, and ground tests showed a capability of generating proper pseudorange. Also, preliminary flight experiments using a pseudo quasi-zenith satellite, a helicopter on which the pseudolite is installed, were conducted in early 2006, and the BOC-type correlation function was monitored in real time.

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