Preliminary results of a hybrid thermoelectric propulsion system for a multirotor uas with active rectifying, electronic throttle control and supercapacitors

dc.contributor.author	Fernández Cabanas, Manés
dc.contributor.author	Ballesteros Duque, Salvador
dc.contributor.author	Díaz González, Juan
dc.contributor.author	Pedrayes González, Joaquín Francisco
dc.contributor.author	García Fernández, María
dc.date.accessioned	2022-06-29T08:17:06Z
dc.date.available	2022-06-29T08:17:06Z
dc.date.issued	2021
dc.identifier.citation	Applied sciences (Switzerland), 11(17) (2021); doi:10.3390/app11177899
dc.identifier.issn	2076-3417
dc.identifier.uri	http://hdl.handle.net/10651/63713
dc.language.iso	eng
dc.relation.ispartof	Applied sciences (switzerland)
dc.rights	© 2021 Los autores
dc.rights	CC Reconocimiento 4.0 Internacional
dc.rights.uri	http://creativecommons.org/licenses/by/4.0/
dc.source	Scopus
dc.source.uri	https://www.scopus.com/inward/record.uri?eid=2-s2.0-85114097507&doi=10.3390%2fapp11177899&partnerID=40&md5=2598788832ca6a171723ab655d0aa1a6
dc.title	Preliminary results of a hybrid thermoelectric propulsion system for a multirotor uas with active rectifying, electronic throttle control and supercapacitors
dc.type	journal article
dc.identifier.doi	10.3390/app11177899
dc.relation.publisherversion	http://dx.doi.org/10.3390/app11177899
dc.rights.accessRights	open access
dc.type.hasVersion	VoR

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