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dc.contributor.authorRotondo, Damiano
dc.contributor.authorCristofaros, A
dc.contributor.authorJohansen, T
dc.contributor.authorNejjari Akhi-Elarab, Fatiha
dc.contributor.authorPuig Cayuela, Vicenç
dc.contributor.otherUniversitat Politècnica de Catalunya. Departament d'Enginyeria de Sistemes, Automàtica i Informàtica Industrial
dc.date.accessioned2017-02-24T13:15:31Z
dc.date.available2017-02-24T13:15:31Z
dc.date.issued2016
dc.identifier.citationRotondo, D., Cristofaros, A., Johansen , T., Nejjari, F., Puig, V. Detection of icing and actuators faults in the longitudinal dynamics of small UAVs using an LPV proportional integral unknown input observer. A: International Conference on Control and Fault-Tolerant Systems. "SYSTOL 2016 - 3rd Conference on Control and Fault-Tolerant Systems, Barcelona, Spain, Sept. 7-9, 2016, proceedings book". Barcelona: IEEE Press, 2016, p. 675-682.
dc.identifier.isbn978-1-5090-0658-8
dc.identifier.urihttp://hdl.handle.net/2117/101543
dc.description.abstractThis paper proposes a linear parameter varying proportional integral unknown input observer (PI-UIO) for the diagnosis of actuator faults and icing in unmanned aerial vehicles. It is shown that in presence of sensor noise, the proposed PI-UIO has the advantage of being affected by the noise, but not by its derivative. Another contribution of the paper is the introduction of an icing to wind/noise ratio, which allows performing an optimal tuning of some PI-UIO design parameters. Results obtained with a Zagi Flying Wing simulator are used to validate the effectiveness of the proposed approach.
dc.format.extent8 p.
dc.language.isoeng
dc.publisherIEEE Press
dc.subjectÀrees temàtiques de la UPC::Informàtica::Automàtica i control
dc.subject.lcshGlaç
dc.subject.lcshAutomatic control
dc.subject.lcshDrone aircraft
dc.subject.otherAircraft
dc.subject.otherActuators
dc.subject.otherMathematical model
dc.subject.otherObservers
dc.subject.otherEstimation error
dc.subject.otherVehicle dynamics
dc.subject.otherIce
dc.titleDetection of icing and actuators faults in the longitudinal dynamics of small UAVs using an LPV proportional integral unknown input observer
dc.typeConference report
dc.subject.lemacGel
dc.subject.lemacControl automàtic
dc.subject.lemacAvions no tripulats
dc.contributor.groupUniversitat Politècnica de Catalunya. SAC - Sistemes Avançats de Control
dc.identifier.doi10.1109/SYSTOL.2016.7739829
dc.description.peerreviewedPeer Reviewed
dc.rights.accessOpen Access
drac.iddocument19707651
dc.description.versionPostprint (author's final draft)
dc.relation.projectidinfo:eu-repo/grantAgreement/MINECO/1PE/DPI2013-48243-C2-1-R
upcommons.citation.authorRotondo, D.; Cristofaros, A.; Johansen, T.; Nejjari, F.; Puig, V.
upcommons.citation.contributorInternational Conference on Control and Fault-Tolerant Systems
upcommons.citation.pubplaceBarcelona
upcommons.citation.publishedtrue
upcommons.citation.publicationNameSYSTOL 2016 - 3rd Conference on Control and Fault-Tolerant Systems, Barcelona, Spain, Sept. 7-9, 2016, proceedings book
upcommons.citation.startingPage675
upcommons.citation.endingPage682


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