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dc.contributor.authorGryte, Kristoffer
dc.contributor.authorHann, Richard
dc.contributor.authorAlam, Mushfiqul
dc.contributor.authorRohac, Jan
dc.contributor.authorJohansen, Tor Arne
dc.contributor.authorFossen, Thor I.
dc.date.accessioned2019-03-29T06:35:58Z
dc.date.available2019-03-29T06:35:58Z
dc.date.created2019-01-06T20:25:17Z
dc.date.issued2018
dc.identifier.isbn978-1-5386-1354-2
dc.identifier.urihttp://hdl.handle.net/11250/2592296
dc.description.abstractWith advanced control, estimation and simulation requirements in unmanned aerial systems comes the need for sophisticated aerodynamic models. This paper reviews two common means for establishing such models; numerical design tools and wind tunnel testing, by presenting strengths and potential problems, in a ”lessons learned”-manner. As a case study throughout the paper, a six degrees-of-freedom aerodynamic model of the Skywalker X8 fixed-wing unmanned aerial vehicle is presented.nb_NO
dc.language.isoengnb_NO
dc.publisherInstitute of Electrical and Electronics Engineers (IEEE)nb_NO
dc.relation.ispartof2018 International Conference on Unmanned Aircraft Systems
dc.titleAerodynamic modeling of the Skywalker X8 Fixed-Wing Unmanned Aerial Vehiclenb_NO
dc.typeChapternb_NO
dc.description.versionacceptedVersionnb_NO
dc.identifier.doi10.1109/ICUAS.2018.8453370
dc.identifier.cristin1651112
dc.description.localcode© 2018 IEEE. Personal use of this material is permitted. Permission from IEEE must be obtained for all other uses, in any current or future media, 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 component of this work in other works.nb_NO
cristin.unitcode194,63,25,0
cristin.unitnameInstitutt for teknisk kybernetikk
cristin.ispublishedtrue
cristin.fulltextoriginal
cristin.qualitycode1


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