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dc.contributor.authorGiribet, Juan I.es
dc.contributor.authorPose, Claudio D.es
dc.contributor.authorMas, Ignacioes
dc.date.accessioned2019-08-16T15:01:42Z
dc.date.available2019-08-16T15:01:42Z
dc.date.issued2017
dc.identifier.urihttp://ri.itba.edu.ar/handle/123456789/1716
dc.description.abstract"Recently, it was shown that an hexagon-shaped hexa-rotor micro aerial vehicle with unidirectionally spinning tilted rotors is capable of fault tolerant attitude and altitude control. This result has been theoretically proven and validated by simulations. However, experimental results have never been reported yet. In this work experimental results are presented, and a comparison between a tilted-rotor hexacopter with one in a standard rotor configuration is carried out."es
dc.language.isoenen
dc.subjectACTUADORESes
dc.subjectSISTEMAS DE CONTROLes
dc.subject.otherTOLERANCIA A FALLOSes
dc.subject.otherMICRO VEHICULOS AEREOSes
dc.titleFault tolerant control of an hexacopter with a tilted-rotor configurationen
dc.typePonencias en Congresoses
itba.description.filiationFil: Giribet, Juan I. Universidad de Buenos Aires; Argentina.es
itba.description.filiationFil: Giribet, Juan I. Consejo Nacional de Investigaciones Científicas y Técnicas; Argentina.es
itba.description.filiationFil: Pose, Claudio D. Universidad de Buenos Aires; Argentina.es
itba.description.filiationFil: Mas, Ignacio. Instituto Tecnológico de Buenos Aires; Argentina.es
itba.description.filiationFil: Mas, Ignacio. Consejo Nacional de Investigaciones Científicas y Técnicas; Argentina.es


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