DC FieldValueLanguage
dc.contributor.authorMontel, Mike-
dc.contributor.authorThielecke, Frank-
dc.date.accessioned2020-01-13T11:54:32Z-
dc.date.available2020-01-13T11:54:32Z-
dc.date.issued2020-06-01-
dc.identifier.citationCEAS Aeronautical Journal 11 (2): 461-474 (2020-06-01)de_DE
dc.identifier.issn1869-5590de_DE
dc.identifier.urihttp://hdl.handle.net/11420/4340-
dc.description.abstractIn this paper, a novel high-precision aircraft loads estimator (named EAGLE) will be introduced. EAGLE is based on the hybridization of two state-of-the-art loads estimation methods (a Luenberger observer and the local model network approach) and combines the individual advantages of the underlying methods. The hybrid method features an accurate estimation of structural loads (such as bending moments, shear forces, and torsional moments) due to maneuvers and gusts even for high load events and can be set up for a given flight test database in shortest time. Therefore, the hybrid method provides a cost-efficient setup of an accurate aircraft loads monitoring system. The paper focuses on the introduction of the new loads observer method and its validation by means of an extensive flight test database containing high maneuver and gust load events, which has been acquired using the ultra-light test aircraft UW-9 Sprint.en
dc.language.isoende_DE
dc.relation.ispartofCEAS Aeronautical Journalde_DE
dc.subjectFlight testde_DE
dc.subjectLocal model networkde_DE
dc.subjectLuenberger observerde_DE
dc.subjectModel-based loads estimationde_DE
dc.subjectStructural health monitoringde_DE
dc.subject.ddc000: Allgemeines, Wissenschaftde_DE
dc.titleEfficient and accurate technology for aircraft loads estimationde_DE
dc.typeArticlede_DE
dc.type.diniarticle-
dcterms.DCMITypeText-
tuhh.abstract.englishIn this paper, a novel high-precision aircraft loads estimator (named EAGLE) will be introduced. EAGLE is based on the hybridization of two state-of-the-art loads estimation methods (a Luenberger observer and the local model network approach) and combines the individual advantages of the underlying methods. The hybrid method features an accurate estimation of structural loads (such as bending moments, shear forces, and torsional moments) due to maneuvers and gusts even for high load events and can be set up for a given flight test database in shortest time. Therefore, the hybrid method provides a cost-efficient setup of an accurate aircraft loads monitoring system. The paper focuses on the introduction of the new loads observer method and its validation by means of an extensive flight test database containing high maneuver and gust load events, which has been acquired using the ultra-light test aircraft UW-9 Sprint.de_DE
tuhh.publisher.doi10.1007/s13272-019-00423-z-
tuhh.publication.instituteFlugzeug-Systemtechnik M-7de_DE
tuhh.type.opus(wissenschaftlicher) Artikel-
dc.type.driverarticle-
dc.type.casraiJournal Article-
tuhh.container.issue2de_DE
tuhh.container.volume11de_DE
tuhh.container.startpage461de_DE
tuhh.container.endpage474de_DE
dc.identifier.scopus2-s2.0-85074109680de_DE
local.status.inpresstruede_DE
datacite.resourceTypeJournal Article-
datacite.resourceTypeGeneralText-
item.mappedtypeArticle-
item.fulltextNo Fulltext-
item.creatorGNDMontel, Mike-
item.creatorGNDThielecke, Frank-
item.openairecristypehttp://purl.org/coar/resource_type/c_6501-
item.cerifentitytypePublications-
item.grantfulltextnone-
item.languageiso639-1en-
item.creatorOrcidMontel, Mike-
item.creatorOrcidThielecke, Frank-
item.openairetypeArticle-
crisitem.author.deptFlugzeug-Systemtechnik M-7-
crisitem.author.deptFlugzeug-Systemtechnik M-7-
crisitem.author.orcid0000-0003-4304-4364-
crisitem.author.orcid0000-0002-9755-5381-
crisitem.author.parentorgStudiendekanat Maschinenbau-
crisitem.author.parentorgStudiendekanat Maschinenbau-
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