Please use this identifier to cite or link to this item: http://hdl.handle.net/10397/109967
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dc.contributorDepartment of Aeronautical and Aviation Engineering-
dc.creatorJia, Q-
dc.creatorLuo, Y-
dc.creatorXu, B-
dc.creatorHsu, LT-
dc.creatorWu, R-
dc.date.accessioned2024-11-20T07:30:36Z-
dc.date.available2024-11-20T07:30:36Z-
dc.identifier.urihttp://hdl.handle.net/10397/109967-
dc.language.isoenen_US
dc.publisherChinese Society of Aeronautics and Astronauticsen_US
dc.rights© 2023 Production and hosting by Elsevier Ltd. on behalf of Chinese Society of Aeronautics and Astronautics. This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).en_US
dc.rightsThe following publication Jia, Q., Luo, Y., Xu, B., Hsu, L.-T., & Wu, R. (2024). A robust vector tracking loop structure based on potential bias analysis. Chinese Journal of Aeronautics, 37(4), 405-420 is available at https://doi.org/10.1016/j.cja.2023.11.013.en_US
dc.subjectGlobal Navigation Satellite System (GNSS)en_US
dc.subjectLeast Absolute Shrinkage and Selection Operator (LASSO)en_US
dc.subjectMultipathen_US
dc.subjectNon-Line-of-Sight (NLOS)en_US
dc.subjectTracking bias propagationen_US
dc.subjectVector Tracking Loop (VTL)en_US
dc.titleA robust vector tracking loop structure based on potential bias analysisen_US
dc.typeJournal/Magazine Articleen_US
dc.identifier.spage405-
dc.identifier.epage420-
dc.identifier.volume37-
dc.identifier.issue4-
dc.identifier.doi10.1016/j.cja.2023.11.013-
dcterms.abstractThis paper proposes a robust vector tracking loop structure based on potential bias analysis. The influence of four kinds of biases on the existing two implementations of Vector Tracking Loops (VTLs) is illustrated by theoretical analysis and numerical simulations, and the following findings are obtained. Firstly, the initial user state bias leads to steady navigation solution bias in the relative VTL, while new measurements can eliminate it in the absolute VTL. Secondly, the initial code phase bias is transferred to the following navigation solutions in the relative VTL, while new measurements can eliminate it in the absolute VTL. Thirdly, the user state bias induced by erroneous navigation solution of VTLs can be eliminated by both of the two VTLs. Fourthly, the multipath/NLOS likely affects the two VTLs, and the induced tracking bias in the duration of the multipath/NLOS would decrease the performance of VTLs. Based on the above analysis, a robust VTL structure is proposed, where the absolute VTL is selected for its robustness to the two kinds of initialization biases; meanwhile, the instant bias detection and correction method is used to improve the performance of VTLs in the duration of the multipath/NLOS. Numerical simulations and experimental results verify the effectiveness of the proposed robust VTL structure.-
dcterms.accessRightsopen accessen_US
dcterms.bibliographicCitationChinese journal of aeronautics, Apr. 2024, v. 37, no. 4, p. 405-420-
dcterms.isPartOfChinese journal of aeronautics-
dcterms.issued2024-04-
dc.identifier.scopus2-s2.0-85186175182-
dc.identifier.eissn1000-9361-
dc.description.validate202411 bcch-
dc.description.oaVersion of Recorden_US
dc.identifier.FolderNumberOA_Scopus/WOSen_US
dc.description.fundingSourceOthersen_US
dc.description.fundingTextScientific Research Program of Tianjin Municipal Education Commission, China; Special Project of the National Science Foundation of Chinaen_US
dc.description.pubStatusPublisheden_US
dc.description.oaCategoryCCen_US
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