GNSS yaw attitude estimation: Results for the Japanese Quasi‐Zenith Satellite System Block‐II satellites using single‐ or triple‐frequency signals from two antennas

Author:

Hauschild André1ORCID

Affiliation:

1. German Aerospace Center (DLR)German Space Operations Center (GSOC) Weßling Germany

Publisher

Institute of Navigation

Subject

Electrical and Electronic Engineering,Aerospace Engineering

Reference13 articles.

1. IwamaR SogaH OdagawaK et al.Operation of sub‐meter class augmentation system and demonstration experiments with Quasi‐Zenith Satellite MICHIBIKI. In:Proceedings of the 2012 International Technical Meeting of the Institute of Navigation;Newport Beach CA January 2012:1295‐1301.

2. HarimaK ChoyS WakabayashiY KogureS RizosC.Transmission of augmentation messages for precise point positioning utilizing Japanese QZSS LEX signal. In:Proceedings of the 27th International Technical Meeting of the Satellite Division of the Institute of Navigation (ION GNSS+ 2014);Tampa Florida; September 2014:2467‐2477.

3. Constellation completed: QZS‐3 and QZS‐4 join the Quasi‐Zenith Satellite System;Steigenberger P;GPS World,2018

4. IshijimaY InabaN MatsumotoA et al.Design and development of the first Quasi‐Zenith Satellite attitude and orbit control system. In:Proceedings of the IEEE Aerospace Conference; March2009;Big Sky MT:1‐8.

5. QZS-1 Yaw Attitude Estimation Based on Measurements from the CONGO Network

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