Please use this identifier to cite or link to this item:
http://hdl.handle.net/10397/109967
DC Field | Value | Language |
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dc.contributor | Department of Aeronautical and Aviation Engineering | - |
dc.creator | Jia, Q | - |
dc.creator | Luo, Y | - |
dc.creator | Xu, B | - |
dc.creator | Hsu, LT | - |
dc.creator | Wu, R | - |
dc.date.accessioned | 2024-11-20T07:30:36Z | - |
dc.date.available | 2024-11-20T07:30:36Z | - |
dc.identifier.uri | http://hdl.handle.net/10397/109967 | - |
dc.language.iso | en | en_US |
dc.publisher | Chinese Society of Aeronautics and Astronautics | en_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.rights | The 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.subject | Global Navigation Satellite System (GNSS) | en_US |
dc.subject | Least Absolute Shrinkage and Selection Operator (LASSO) | en_US |
dc.subject | Multipath | en_US |
dc.subject | Non-Line-of-Sight (NLOS) | en_US |
dc.subject | Tracking bias propagation | en_US |
dc.subject | Vector Tracking Loop (VTL) | en_US |
dc.title | A robust vector tracking loop structure based on potential bias analysis | en_US |
dc.type | Journal/Magazine Article | en_US |
dc.identifier.spage | 405 | - |
dc.identifier.epage | 420 | - |
dc.identifier.volume | 37 | - |
dc.identifier.issue | 4 | - |
dc.identifier.doi | 10.1016/j.cja.2023.11.013 | - |
dcterms.abstract | This 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.accessRights | open access | en_US |
dcterms.bibliographicCitation | Chinese journal of aeronautics, Apr. 2024, v. 37, no. 4, p. 405-420 | - |
dcterms.isPartOf | Chinese journal of aeronautics | - |
dcterms.issued | 2024-04 | - |
dc.identifier.scopus | 2-s2.0-85186175182 | - |
dc.identifier.eissn | 1000-9361 | - |
dc.description.validate | 202411 bcch | - |
dc.description.oa | Version of Record | en_US |
dc.identifier.FolderNumber | OA_Scopus/WOS | en_US |
dc.description.fundingSource | Others | en_US |
dc.description.fundingText | Scientific Research Program of Tianjin Municipal Education Commission, China; Special Project of the National Science Foundation of China | en_US |
dc.description.pubStatus | Published | en_US |
dc.description.oaCategory | CC | en_US |
Appears in Collections: | Journal/Magazine Article |
Files in This Item:
File | Description | Size | Format | |
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1-s2.0-S1000936123003977-main.pdf | 3.83 MB | Adobe PDF | View/Open |
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