Technical Papers
Jul 28, 2017

Carrier-Phase-Based Quality Control for GNSS Dynamic Relative Navigation

Publication: Journal of Aerospace Engineering
Volume 30, Issue 6

Abstract

Carrier-phase-based global navigation satellite system (GNSS) dynamic relative navigation is essential for fields that require high integrity and accuracy. Code-based receiver autonomous integrity monitoring (RAIM) has been studied extensively; however, carrier-phase-based integrity monitoring requires further study to meet the requirements of high-performance navigation. This paper proposes a quality-control method for carrier-phase-based GNSS relative navigation. It proposes the double difference (DD) model of carrier-phase-based relative navigation, which includes high-integrity difference navigation architecture and a novel closed-loop extended Kalman filter (EKF) using partial ambiguity resolution. Quality-control procedures based on least-squares principle are extended to EKF, in which fault detection using carrier-phase-based RAIM (CRAIM) and fault identification using a double w-test are carried out, and the integrity performance of reliability and separability are studied. The field trial data are tested and analyzed, and it is shown that the proposed method is able to detect and identify both step and ramp failures. The proposed method can be used not only for code measurements but also for carrier-phase measurements, thus improving the performance of GNSS relative navigation significantly.

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Acknowledgments

Research for this paper was supported by the Aviation Science Foundation of China (20150852013), the Natural Science Foundation of Jiangsu province (BK20161490,) and the Fundamental Research Project for NUAA (NS2015087). The authors also gratefully acknowledge the helpful comments and suggestions of the reviewers, which have improved the presentation.

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Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 30Issue 6November 2017

History

Received: Nov 5, 2016
Accepted: Apr 17, 2017
Published online: Jul 28, 2017
Published in print: Nov 1, 2017
Discussion open until: Dec 28, 2017

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Authors

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Haiying Liu [email protected]
Associate Professor, College of Astronautics, Nanjing Univ. of Aeronautics and Astronautics, Nanjing 210016, P.R. China (corresponding author). E-mail: [email protected]
Research Assistant, Nottingham Geospatial Institute, Univ. of Nottingham, Nottingham Geospatial Bldg., Nottingham NG7 2TU, U.K. E-mail: [email protected]
Professor, Aviation Key Laboratory of Science and Technology on Inertial, Flight Automatic Control Research Institute, Xi’an 710065, P.R. China. E-mail: [email protected]
Associate Research Fellow, Aviation Key Laboratory of Science and Technology on Inertial, Flight Automatic Control Research Institute, Xi’an 710065, P.R. China. E-mail: [email protected]

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