Dynamic soaring of unmanned aerial vehicle within airliner wake vortex in climb regime

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dc.contributor.authorZikmund, Pavelcs
dc.contributor.authorMatějů, Jiřícs
dc.coverage.issue13cs
dc.coverage.volume231cs
dc.date.issued2017-11-01cs
dc.description.abstractThe paper presents an analysis of an unmanned aerial vehicle gliding in an airliner wake vortex using the dynamic soaring principle. The presented results provide insight into energy balance and controllability of the unmanned aerial vehicle flying in an airliner wake vortex.en
dc.description.abstractThe paper presents an analysis of an unmanned aerial vehicle gliding in an airliner wake vortex using the dynamic soaring principle. The presented results provide insight into energy balance and controllability of the unmanned aerial vehicle flying in an airliner wake vortex.en
dc.formattextcs
dc.format.extent2479-2486cs
dc.format.mimetypeapplication/pdfcs
dc.identifier.citationPROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING. 2017, vol. 231, issue 13, p. 2479-2486.en
dc.identifier.doi10.1177/0954410016667147cs
dc.identifier.issn0954-4100cs
dc.identifier.orcid0000-0002-5793-8628cs
dc.identifier.orcid0000-0001-9242-4676cs
dc.identifier.other128483cs
dc.identifier.scopus57204492594cs
dc.identifier.urihttp://hdl.handle.net/11012/63674
dc.language.isoencs
dc.publisherSAGEcs
dc.relation.ispartofPROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERINGcs
dc.relation.urihttp://pig.sagepub.com/content/early/2016/09/02/0954410016667147.abstractcs
dc.rights(C) SAGEcs
dc.rights.accessopenAccesscs
dc.rights.sherpahttp://www.sherpa.ac.uk/romeo/issn/0954-4100/cs
dc.subjectDynamic soaringen
dc.subjectFormation flighten
dc.subjectWake vortexen
dc.subjectSelf-sustained flighten
dc.subjectUnmanned aerial vehicleen
dc.subjectDynamic soaring
dc.subjectFormation flight
dc.subjectWake vortex
dc.subjectSelf-sustained flight
dc.subjectUnmanned aerial vehicle
dc.titleDynamic soaring of unmanned aerial vehicle within airliner wake vortex in climb regimeen
dc.title.alternativeDynamic soaring of unmanned aerial vehicle within airliner wake vortex in climb regimeen
dc.type.driverarticleen
dc.type.statusPeer-revieweden
dc.type.versionacceptedVersionen
sync.item.dbidVAV-128483en
sync.item.dbtypeVAVen
sync.item.insts2025.10.14 14:52:09en
sync.item.modts2025.10.14 10:11:49en
thesis.grantorVysoké učení technické v Brně. Fakulta strojního inženýrství. Divize letecké a automobilní technikycs
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