Please use this identifier to cite or link to this item: http://hdl.handle.net/10397/118563
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dc.contributorDepartment of Aeronautical and Aviation Engineering-
dc.creatorYan, P-
dc.creatorZhong, Y-
dc.creatorHsu, LT-
dc.date.accessioned2026-04-24T01:30:23Z-
dc.date.available2026-04-24T01:30:23Z-
dc.identifier.issn0018-9251-
dc.identifier.urihttp://hdl.handle.net/10397/118563-
dc.language.isoenen_US
dc.publisherInstitute of Electrical and Electronics Engineersen_US
dc.rights© 2024 IEEE. Personal use of this material is permitted. Permission from IEEE must be obtained for all other uses, in any current or future media, including reprinting/republishing this material for advertising or promotional purposes, creating new collective works, for resale or redistribution to servers or lists, or reuse of any copyrighted component of this work in other works.en_US
dc.rightsThe following publication P. Yan, Y. Zhong and L. -T. Hsu, 'Principal Gaussian Overbound for Heavy-Tailed Error Bounding,' in IEEE Transactions on Aerospace and Electronic Systems, vol. 61, no. 1, pp. 829-852, Feb. 2025 is available at https://doi.org/10.1109/TAES.2024.3448405.en_US
dc.subjectBounding methodsen_US
dc.subjectFast fourier transforms (FFT)en_US
dc.subjectGaussian mixture model (GMM)en_US
dc.subjectGlobal navigation satellite system (GNSS)en_US
dc.subjectHeavy-tailed error distributionen_US
dc.subjectIntegrity analysisen_US
dc.titlePrincipal Gaussian overbound for heavy-tailed error boundingen_US
dc.typeJournal/Magazine Articleen_US
dc.identifier.spage829-
dc.identifier.epage852-
dc.identifier.volume61-
dc.identifier.issue1-
dc.identifier.doi10.1109/TAES.2024.3448405-
dcterms.abstractA sharp yet conservative overbound for heavy-tailed error distributions is essential in integrity monitoring applications due to availability and continuity constraints. This article proposes the principal Gaussian overbound (PGO) for heavy-tailed error distributions by leveraging the characteristics of the Gaussian mixture model. The overbounding property of the PGO is proved to be preserved through convolution, which makes it possible to derive pseudorange-level requirements from the position domain integrity requirements. Experimental results on two datasets show that the PGO provides the most competitive bounding performance for heavy-tailed differential global navigation satellite system (GNSS) pseudorange errors when compared to the two-step Gaussian overbound and Gaussian-Pareto overbound, yielding a sharp bound in both the core and tail parts of the error distribution. The proposed method reduces the mean vertical protection level (VPL) by more than 78 compared to the two-step Gaussian overbounding method on the urban dataset. In addition, the mean computation time of VPL is only 0.08 s with 15 measurements by employing fast Fourier transforms, suggesting the substantial potential of the PGO in GNSS applications with strict integrity and real-time requirements. Furthermore, the feasibility of the PGO in fault detection is discussed.-
dcterms.accessRightsopen accessen_US
dcterms.bibliographicCitationIEEE transactions on aerospace and electronic systems, Feb. 2025, v. 61, no. 1, p. 829-852-
dcterms.isPartOfIEEE transactions on aerospace and electronic systems-
dcterms.issued2025-02-
dc.identifier.scopus2-s2.0-105002088670-
dc.identifier.eissn1557-9603-
dc.description.validate202604 bcjz-
dc.description.oaAccepted Manuscripten_US
dc.identifier.SubFormIDG001520/2026-04en_US
dc.description.fundingSourceRGCen_US
dc.description.fundingTextThis work was supported by the University Grants Committee of Hong Kong under the scheme Research Impact Fund under Project no. R5009-21 'Reliable Multiagent Collaborative Global Navigation Satellite System Positioning for Intelligent Transportation Systems.'en_US
dc.description.pubStatusPublisheden_US
dc.description.oaCategoryGreen (AAM)en_US
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