Please use this identifier to cite or link to this item:
http://hdl.handle.net/10397/89042
DC Field | Value | Language |
---|---|---|
dc.contributor | Interdisciplinary Division of Aeronautical and Aviation Engineering | en_US |
dc.creator | Jiang, Y | en_US |
dc.date.accessioned | 2021-01-15T07:15:04Z | - |
dc.date.available | 2021-01-15T07:15:04Z | - |
dc.identifier.issn | 1080-5370 | en_US |
dc.identifier.uri | http://hdl.handle.net/10397/89042 | - |
dc.language.iso | en | en_US |
dc.publisher | Springer | en_US |
dc.rights | © Springer-Verlag GmbH Germany, part of Springer Nature 2020 | en_US |
dc.rights | This version of the article has been accepted for publication, after peer review (when applicable) and is subject to Springer Nature’s AM terms of use (https://www.springernature.com/gp/open-research/policies/accepted-manuscript-terms), but is not the Version of Record and does not reflect post-acceptance improvements, or any corrections. The Version of Record is available online at: http://dx.doi.org/10.1007/s10291-020-01028-4. | en_US |
dc.subject | Ephemeris monitor | en_US |
dc.subject | GBAS | en_US |
dc.subject | GNSS | en_US |
dc.subject | Integrity monitor | en_US |
dc.title | Ephemeris monitor with ambiguity resolution for CAT II/III GBAS | en_US |
dc.type | Journal/Magazine Article | en_US |
dc.identifier.spage | 1 | en_US |
dc.identifier.epage | 7 | en_US |
dc.identifier.volume | 24 | en_US |
dc.identifier.issue | 4 | en_US |
dc.identifier.doi | 10.1007/s10291-020-01028-4 | en_US |
dcterms.abstract | In safety-critical applications, such as the Ground-Based Augmentation System for precision approaches in civil aviation, it is important to safeguard users under the case of ephemeris failures. For CAT II/III approaches, different ephemeris monitors with approaches for ambiguity resolution are proposed with the double differenced carrier phase as the test statistics. The continuity risks introduced by the ambiguity resolution are addressed by deriving the required averaging time for new, acquired, and re-acquired satellites. Since the ephemeris fault is closely related with the baseline length between ground stations, the minimum baseline length is derived to meet the probability of missed detection region. Current methods are compared with both the averaging time and the ground baseline length. It is demonstrated that a combination of two methods is able to achieve the best performance with 94 averaging epochs and 218 m ground baseline length. | en_US |
dcterms.accessRights | open access | en_US |
dcterms.bibliographicCitation | GPS solutions, 2020, v. 24, no. 4, 116, p. 1-7 | en_US |
dcterms.isPartOf | GPS solutions | en_US |
dcterms.issued | 2020 | - |
dc.identifier.scopus | 2-s2.0-85091268601 | - |
dc.identifier.eissn | 1521-1886 | en_US |
dc.identifier.artn | 116 | en_US |
dc.description.validate | 202101 bcrc | en_US |
dc.description.oa | Accepted Manuscript | en_US |
dc.identifier.FolderNumber | a0540-n01, a1253 | - |
dc.identifier.SubFormID | 44373 | - |
dc.description.fundingSource | Others | en_US |
dc.description.fundingText | NSFC | en_US |
dc.description.pubStatus | Published | en_US |
dc.description.oaCategory | Green (AAM) | en_US |
Appears in Collections: | Journal/Magazine Article |
Files in This Item:
File | Description | Size | Format | |
---|---|---|---|---|
Manuscript-Jiang-20200828_Leick_approved_Leick_approved.pdf | Pre-Published version | 4.25 MB | Adobe PDF | View/Open |
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