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dc.contributor.authorWang, Ko-Yuanen_US
dc.contributor.authorLee, Pei-Hsuanen_US
dc.contributor.authorHung, Shao-Kangen_US
dc.date.accessioned2017-04-21T06:49:04Z-
dc.date.available2017-04-21T06:49:04Z-
dc.date.issued2015en_US
dc.identifier.isbn978-1-4673-9107-8en_US
dc.identifier.issn2159-6255en_US
dc.identifier.urihttp://hdl.handle.net/11536/135935-
dc.description.abstractA kite-like unmanned aerial vehicle (UAV) is leashed by a taut tether, which supplies electric power from the ground battery. Although working range is restricted, the flight time is extended significantly. Long endurance is a necessary condition for serious UAV missions. In this paper, a payload model of kite-like UAV is developed by measuring electrical and mechanical characteristics of the UAV\'s propulsion unit. After investigating the model, there exits an optimum electric cable selection to achieve maximum payload capacity or highest flying altitude. Simulation results indicate the proper electric cable selection is crucial for kite-like UAV.en_US
dc.language.isoen_USen_US
dc.titleOptimum Electric Cable Selection for Kite-like Unmanned Aerial Vehicleen_US
dc.typeProceedings Paperen_US
dc.identifier.journal2015 IEEE/ASME INTERNATIONAL CONFERENCE ON ADVANCED INTELLIGENT MECHATRONICS (AIM)en_US
dc.citation.spage1537en_US
dc.citation.epage1540en_US
dc.contributor.department機械工程學系zh_TW
dc.contributor.departmentDepartment of Mechanical Engineeringen_US
dc.identifier.wosnumberWOS:000381493900263en_US
dc.citation.woscount0en_US
Appears in Collections:Conferences Paper