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contributor authorHaiying Liu
contributor authorYang Gao
contributor authorYazhou Yue
contributor authorLei Kou
date accessioned2017-12-16T09:22:14Z
date available2017-12-16T09:22:14Z
date issued2017
identifier other%28ASCE%29AS.1943-5525.0000780.pdf
identifier urihttp://138.201.223.254:8080/yetl1/handle/yetl/4241966
description abstractCarrier-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.
publisherAmerican Society of Civil Engineers
titleCarrier-Phase-Based Quality Control for GNSS Dynamic Relative Navigation
typeJournal Paper
journal volume30
journal issue6
journal titleJournal of Aerospace Engineering
identifier doi10.1061/(ASCE)AS.1943-5525.0000780
treeJournal of Aerospace Engineering:;2017:;Volume ( 030 ):;issue: 006
contenttypeFulltext


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