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dc.creatorZufferey, Raphaeles
dc.creatorTormo Barbero, Jesúses
dc.creatorMar Guzmán, M.es
dc.creatorMaldonado, F.J.es
dc.creatorSánchez Laulhe, Ernestoes
dc.creatorGrau, Pedroes
dc.creatorPérez, Martínes
dc.creatorAcosta, José Ángeles
dc.creatorOllero Baturone, Aníbales
dc.date.accessioned2022-10-03T14:31:17Z
dc.date.available2022-10-03T14:31:17Z
dc.date.issued2021
dc.identifier.citationZufferey, R., Tormo Barbero, J., Mar Guzmán, M., Maldonado, F.J., Sánchez Laulhe, E., Grau, P.,...,Ollero Baturone, A. (2021). Design of the High-Payload Flapping Wing Robot E-Flap. IEEE Robotics and Automation Letters, 6 (2), 3097-3104.
dc.identifier.issn2377-3766es
dc.identifier.urihttps://hdl.handle.net/11441/137567
dc.description.abstractAutonomous lightweight flapping-wing robots show potential to become a safe and affordable solution for rapidly deploying robots around humans and in complex environments. The absence of propellers makes such vehicles more resistant to physical contact, permitting flight in cluttered environments, and collaborating with humans. Importantly, the provision of thousands of species of birds that have already mastered the challenging task of flapping flight is a rich source of solutions. However, small wing flapping technology is still in its beginnings, with limited levels of autonomy and physical interaction capability with the environment. One significant limitation to this is the low payload available. Here we show the Eagle-inspired Flapping-wing robot E-Flap, a 510 g novel design capable of a 100% of payload, exceeding the requirement of the computing and sensing package needed to fly with a high degree of autonomy. The concept is extensively characterized, both in a tracked indoor space and in outdoor conditions. We demonstrate flight path angle of up to 50° and velocities from as low as 2 m/s to over 6 m/s. Overall, the robotic platform has been proven to be reliable, having performed over 100 flights. Through mechanical and electronics advances, the E-Flap is a robust vehicle prototype and paves the way towards flapping-wing robots becoming a practical fully autonomous flying solution.es
dc.description.sponsorshipConsejo Europeo de Investigación 788247es
dc.formatapplication/pdfes
dc.format.extent8 p.es
dc.language.isoenges
dc.relation.ispartofIEEE Robotics and Automation Letters, 6 (2), 3097-3104.
dc.rightsAttribution-NonCommercial-NoDerivatives 4.0 Internacional*
dc.rights.urihttp://creativecommons.org/licenses/by-nc-nd/4.0/*
dc.subjectFlapping-wing flightes
dc.subjectPayload-capablees
dc.subjectPrototype designes
dc.subjectUnmanned autonomous vehicleses
dc.titleDesign of the High-Payload Flapping Wing Robot E-Flapes
dc.typeinfo:eu-repo/semantics/articlees
dcterms.identifierhttps://ror.org/03yxnpp24
dc.type.versioninfo:eu-repo/semantics/submittedVersiones
dc.rights.accessRightsinfo:eu-repo/semantics/openAccesses
dc.contributor.affiliationUniversidad de Sevilla. Departamento de Ingeniería de Sistemas y Automáticaes
dc.relation.projectID788247es
dc.identifier.doi10.1109/LRA.2021.3061373es
dc.journaltitleIEEE Robotics and Automation Letterses
dc.publication.volumen6es
dc.publication.issue2es
dc.publication.initialPage3097es
dc.publication.endPage3104es
dc.contributor.funderEuropean Research Council (ERC)es

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