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dc.contributor.authorHovenburg, Anthony Reinier
dc.contributor.authorAndrade, Fabio
dc.contributor.authorHann, Richard
dc.contributor.authorRodin, Christopher D
dc.contributor.authorJohansen, Tor Arne
dc.date.accessioned2020-11-13T09:27:56Z
dc.date.available2020-11-13T09:27:56Z
dc.date.created2020-09-07T14:11:28Z
dc.date.issued2020
dc.identifier.citationIEEE Journal on Miniaturization for Air and Space Systems. 2020, 1 (2), 76 - 89en_US
dc.identifier.issn2576-3164
dc.identifier.urihttps://hdl.handle.net/11250/2687721
dc.description.abstractEarlier studies demonstrate that en-route atmospheric parameters, such as winds and icing conditions, significantly affect the safety, and in-flight performance of unmanned aerial systems. Nowadays, the inclusion of meteorological factors is not a common practice in determining the optimal flight path. This study aims to contribute with a practical method that includes meteorological forecast information in order to obtain the most energy efficient path of a fixed-wing aircraft. The particle swarm optimization-based algorithm takes into consideration the aircraft performance, including the effects of en-route winds and the power required for active electro-thermal icing protection systems to mitigate the effects of icing. As a result, the algorithm selects a path that will use the least energy to complete the given mission. In the scenario evaluated with real meteorological data and real aerodynamic parameters, the battery consumption of the optimized path was 52% lower than the standard straight path.en_US
dc.language.isoengen_US
dc.publisherInstitute of Electrical and Electronics Engineers (IEEE)en_US
dc.relation.urihttp://folk.ntnu.no/richahan/Publications/2020_Pathplanning.pdf
dc.titleLong range path planning using an aircraft performance model for battery powered sUAS equipped with icing protection systemen_US
dc.typeJournal articleen_US
dc.description.versionacceptedVersionen_US
dc.source.pagenumber76-89en_US
dc.source.volume1en_US
dc.source.journalIEEE Journal on Miniaturization for Air and Space Systemsen_US
dc.source.issue2en_US
dc.identifier.doi10.1109/JMASS.2020.3003833
dc.identifier.cristin1827812
dc.relation.projectRegionale forskningsfond Midt-Norge: 285248en_US
dc.relation.projectNotur/NorStore: NN9613Ken_US
dc.relation.projectNorges forskningsråd: 237906en_US
dc.relation.projectNorges forskningsråd: 223254en_US
dc.relation.projectEC/H2020/642153en_US
dc.description.localcode© 2020 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.en_US
cristin.ispublishedtrue
cristin.fulltextpostprint
cristin.qualitycode0


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