dc.creator | Heredia Benot, Guillermo | es |
dc.creator | Ollero Baturone, Aníbal | es |
dc.date.accessioned | 2017-04-03T15:20:11Z | |
dc.date.available | 2017-04-03T15:20:11Z | |
dc.date.issued | 2010 | |
dc.identifier.citation | Heredia Benot, G. y Ollero Baturone, A. (2010). Virtual Sensor for Failure Detection, Identification and Recovery in the Transition Phase of a Morphing Aircraft. Sensors, 3 (10), 2188-2201. | |
dc.identifier.issn | 1424-8220 | es |
dc.identifier.uri | http://hdl.handle.net/11441/56979 | |
dc.description.abstract | The Helicopter Adaptive Aircraft (HADA) is a morphing aircraft which is able to
take-off as a helicopter and, when in forward flight, unfold the wings that are hidden under
the fuselage, and transfer the power from the main rotor to a propeller, thus morphing from
a helicopter to an airplane. In this process, the reliable folding and unfolding of the wings is
critical, since a failure may determine the ability to perform a mission, and may even be
catastrophic. This paper proposes a virtual sensor based Fault Detection, Identification and
Recovery (FDIR) system to increase the reliability of the HADA aircraft. The virtual sensor
is able to capture the nonlinear interaction between the folding/unfolding wings
aerodynamics and the HADA airframe using the navigation sensor measurements. The
proposed FDIR system has been validated using a simulation model of the HADA aircraft,
which includes real phenomena as sensor noise and sampling characteristics and turbulence
and wind perturbations. | es |
dc.format | application/pdf | es |
dc.language.iso | eng | es |
dc.publisher | MDPI AG | es |
dc.relation.ispartof | Sensors, 3 (10), 2188-2201. | |
dc.rights | Attribution-NonCommercial-NoDerivatives 4.0 Internacional | * |
dc.rights.uri | http://creativecommons.org/licenses/by-nc-nd/4.0/ | * |
dc.subject | Virtual sensors | es |
dc.subject | UAV,s | es |
dc.subject | Fault detection | es |
dc.subject | Identification and recovery | es |
dc.subject | Morphing aircraft | es |
dc.title | Virtual Sensor for Failure Detection, Identification and Recovery in the Transition Phase of a Morphing Aircraft | es |
dc.type | info:eu-repo/semantics/article | es |
dcterms.identifier | https://ror.org/03yxnpp24 | |
dc.type.version | info:eu-repo/semantics/publishedVersion | es |
dc.rights.accessRights | info:eu-repo/semantics/openAccess | es |
dc.contributor.affiliation | Universidad de Sevilla. Departamento de Ingeniería de Sistemas y Automática | es |
dc.relation.publisherversion | http://www.mdpi.com/1424-8220/10/3/2188 | es |
dc.identifier.doi | 10.3390/s100302188 | es |
dc.contributor.group | Universidad de Sevilla. TEP151: Robótica, Visión y Control | es |
idus.format.extent | 14 p. | es |
dc.journaltitle | Sensors | es |
dc.publication.volumen | 3 | es |
dc.publication.issue | 10 | es |
dc.publication.initialPage | 2188 | es |
dc.publication.endPage | 2201 | es |