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dc.contributor.authorHansen, Søren
dc.contributor.authorBlanke, Mogens
dc.date.accessioned2014-05-19T11:53:22Z
dc.date.accessioned2016-06-16T12:12:38Z
dc.date.available2014-05-19T11:53:22Z
dc.date.available2016-06-16T12:12:38Z
dc.date.issued2014
dc.identifier.citationIEEE Transactions on Aerospace and Electronic Systems 2014, 50(1):86-101nb_NO
dc.identifier.issn0018-9251
dc.identifier.urihttp://hdl.handle.net/11250/2392884
dc.description.abstractAirspeed sensor faults are common causes for incidents with unmanned aerial vehicles with pitot tube clogging or icing being the most common causes. Timely diagnosis of such faults or other artifacts in signals from airspeed sensing systems could potentially prevent crashes. This paper employs parameter adaptive estimators to provide analytical redundancies and a dedicated diagnosis scheme is designed. Robustness is investigated on sets of flight data to estimate distributions of test statistics. The result is robust diagnosis with adequate balance between false alarm rate and fault detectability.nb_NO
dc.language.isoengnb_NO
dc.titleDiagnosis of Airspeed Measurement Faults for Unmanned Aerial Vehiclesnb_NO
dc.typeJournal articlenb_NO
dc.typePeer reviewed
dc.date.updated2014-05-19T11:53:23Z
dc.source.pagenumber224-239nb_NO
dc.source.volume50nb_NO
dc.source.journalIEEE Transactions on Aerospace and Electronic Systemsnb_NO
dc.source.issue1nb_NO
dc.identifier.doi10.1109/TAES.2013.120420
dc.identifier.cristin1073494
dc.relation.projectNorges forskningsråd: 223254nb_NO
dc.description.localcode(c) 2014 IEEE. Personal use of this material is permitted. Permission from IEEE must be obtained for all other users, 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 components of this work in other works.nb_NO


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