Multibody Model of a UAV in Presence of Wind Fields

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dc.contributor.authorDe Simone, M.C.es_ES
dc.contributor.authorRusso, S.es_ES
dc.contributor.authorRivera, Z.B.es_ES
dc.contributor.authorGuida, D.es_ES
dc.date.accessioned6/22/2022 13:33
dc.date.accessioned2022-09-30T17:01:51Z
dc.date.available6/22/2022 13:33
dc.date.available2022-09-30T17:01:51Z
dc.date.issued2017
dc.description.abstractThe aim of this work is the development of a multibody model of a quadrotor helicopter system in presence of wind fields by using Simscape Multibody Environment. The simplified model of the quadrotor is modelled as a non linear system which is under-actuated and strongly coupled. For the dynamics, aerodynamic effect of drag, the thrust due to the rotation of propellers and external wind fields are considered. In particular, a study on the evaluation of the thrust coefficients is conducted. Thrust evaluation, for prescribed trajectories, gives us indications about the type of propellers and motor characteristics to be installed on the UAV. © 2017 IEEE.es_ES
dc.formatapplication/pdfes_ES
dc.identifier.doi10.1109/ICCAIRO.2017.26es_ES
dc.identifier.urihttps://doi.org/10.1109/ICCAIRO.2017.26
dc.language.isoenges_ES
dc.publisherInstitute of Electrical and Electronics Engineers Inc.es_ES
dc.rightsinfo:eu-repo/semantics/closedAccesses_ES
dc.rights.urihttps://creativecommons.org/licenses/by/4.0/es_ES
dc.sourceProceedings - 2017 International Conference on Control, Artificial Intelligence, Robotics and Optimization, ICCAIRO 2017es_ES
dc.titleMultibody Model of a UAV in Presence of Wind Fieldses_ES
dc.typeinfo:eu-repo/semantics/articlees_ES
dc.type.versioninfo:eu-repo/semantics/publishedVersiones_ES
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