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dc.contributor.authorWang, Ye-
dc.contributor.authorRamirez-Jaime, A.-
dc.contributor.authorXu, Feng-
dc.contributor.authorPuig, Vicenç-
dc.date.accessioned2018-08-01T09:24:19Z-
dc.date.available2018-08-01T09:24:19Z-
dc.date.issued2017-
dc.identifierdoi: 10.1088/1742-6596/783/1/012025-
dc.identifierissn: 1742-6588-
dc.identifiere-issn: 1742-6596-
dc.identifier.citationJournal of Physics: Conference Series 783: 012025 (2017)-
dc.identifier.urihttp://hdl.handle.net/10261/168115-
dc.descriptionTrabajo presentado a la 13th European Workshop on Advanced Control and Diagnosis (ACD 2016).-
dc.description.abstractThis paper presents a nonlinear model predictive control (NMPC) strategy combined with constraint satisfactions for a quadcopter. The full dynamics of the quadcopter describing the attitude and position are nonlinear, which are quite sensitive to changes of inputs and disturbances. By means of constraint satisfactions, partial nonlinearities and modeling errors of the control-oriented model of full dynamics can be transformed into the inequality constraints. Subsequently, the quadcopter can be controlled by an NMPC controller with the updated constraints generated by constraint satisfactions. Finally, the simulation results applied to a quadcopter simulator are provided to show the eectiveness of the proposed strategy.-
dc.description.sponsorshipThis work has been partially funded by the Spanish Government (MINECO) through the project CICYT ECOCIS (ref. DPI2013-48243-C2-1-R), by MINECO and FEDER through the project CICYT HARCRICS (ref. DPI2014-58104-R), by the Natural Science Foundation of Guangdong (No.2015A030313881), by the National Natural Science Foundation of China (No.61673239) and the Shenzhen Key Lab of Space Robotic Technology and Telescience.-
dc.publisherInstitute of Physics Publishing-
dc.relationinfo:eu-repo/grantAgreement/MINECO/Plan Estatal de Investigación Científica y Técnica y de Innovación 2013-2016/DPI2013-48243-C2-1-R-
dc.relationinfo:eu-repo/grantAgreement/MINECO/Plan Estatal de Investigación Científica y Técnica y de Innovación 2013-2016/DPI2014-58104-R-
dc.relation.isversionofPublisher's version-
dc.rightsopenAccess-
dc.titleNonlinear model predictive control with constraint satisfactions for a quadcopter-
dc.typecomunicación de congreso-
dc.identifier.doi10.1088/1742-6596/783/1/012025-
dc.relation.publisherversionhttps://doi.org/10.1088/1742-6596/783/1/012025-
dc.date.updated2018-08-01T09:24:19Z-
dc.description.versionPeer Reviewed-
dc.language.rfc3066eng-
dc.rights.licensehttp://creativecommons.org/licenses/by/3.0-
dc.contributor.funderEuropean Commission-
dc.contributor.funderComisión Interministerial de Ciencia y Tecnología, CICYT (España)-
dc.contributor.funderMinisterio de Economía y Competitividad (España)-
dc.contributor.funderNational Natural Science Foundation of China-
dc.relation.csic-
dc.identifier.funderhttp://dx.doi.org/10.13039/501100001809es_ES
dc.identifier.funderhttp://dx.doi.org/10.13039/501100000780es_ES
dc.identifier.funderhttp://dx.doi.org/10.13039/501100007273es_ES
dc.identifier.funderhttp://dx.doi.org/10.13039/501100003329es_ES
dc.type.coarhttp://purl.org/coar/resource_type/c_5794es_ES
item.cerifentitytypePublications-
item.openairecristypehttp://purl.org/coar/resource_type/c_18cf-
item.grantfulltextopen-
item.openairetypecomunicación de congreso-
item.fulltextWith Fulltext-
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