Proceedings of the Korean Institute of Navigation and Port Research Conference (한국항해항만학회:학술대회논문집)
- Volume 2
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- Pages.125-129
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- 2006
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.