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dc.contributor.authorVieira, Henrique S.
dc.contributor.authorde Paiva, Ely C.
dc.contributor.authorMoriguchi, Sergio K.
dc.contributor.authorCarvalho, Jose R. H.
dc.date.accessioned2024-10-21T18:47:29Z
dc.date.available2024-10-21T18:47:29Z
dc.date.issued2020
dc.identifier.citationIEEE Trans. Aerosp. Electron. Syst.
dc.identifier.issn1557-9603
dc.identifier.urihttp://dx.doi.org/10.1109/TAES.2020.2975525
dc.identifier.urihttps://repositorio.maua.br/handle/MAUA/1567
dc.description.abstractThis article presents a new kind of vectorial backstepping sliding mode control (BSMC) for the positioning and trajectory tracking of an autonomous robotic airship. Also, a unified framework basis for the design/analysis of vectorial BSMC, as well as sliding mode control and backstepping control for a system in lower triangular block form is derived. The design framework makes the theoretical-based comparative analysis of performances/robustness easier between the three nonlinear control approaches. Simulation results for the positioning and tracking of the autonomous airship illustrate the proposal.en
dc.description.sponsorshipFAPEAMpt_BR
dc.description.sponsorshipCNPq DRONI Projectpt_BR
dc.description.sponsorshipProject INCT-SACpt_BR
dc.description.sponsorshipCNPq(Conselho Nacional de Desenvolvimento Cientifico e Tecnologico (CNPQ))pt_BR
dc.description.sponsorshipFAPESP(Fundacao de Amparo a Pesquisa do Estado de Sao Paulo (FAPESP))pt_BR
dc.description.sponsorshipFapesp BEP(Fundacao de Amparo a Pesquisa do Estado de Sao Paulo (FAPESP))pt_BR
dc.description.sponsorshipFapesp VERDEpt_BR
dc.description.sponsorshipFundacao de Amparo a Pesquisa do Estado de Sao Paulo (FAPESP)(Fundacao de Amparo a Pesquisa do Estado de Sao Paulo (FAPESP))pt_BR
dc.description.sponsorshipFAPEAM
dc.description.sponsorshipCNPq DRONI Project
dc.description.sponsorshipProject INCT-SAC
dc.description.sponsorshipCNPq)
dc.description.sponsorshipFAPESP)
dc.format.extent13.0
dc.languageInglêspt_BR
dc.publisherIEEE-INST ELECTRICAL ELECTRONICS ENGINEERS INCen
dc.relation.ispartofIEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS
dc.rightsAcesso Aberto
dc.sourceWeb of Scienceen
dc.subjectBacksteppingen
dc.subjectAerodynamicsen
dc.subjectAtmospheric modelingen
dc.subjectMathematical modelen
dc.subjectForceen
dc.subjectSliding mode controlen
dc.subjectSimulationen
dc.subjectNonlinear controlen
dc.subjectbackstepping (BS)en
dc.subjectsliding mode control (SMC)en
dc.subjectairshipen
dc.subjectunmanned aerial vehicles (UAVs)en
dc.subjectSTATION-KEEPING CONTROLen
dc.subjectTRAJECTORY TRACKINGen
dc.subjectPOSITIONING CONTROLen
dc.subjectPATH-TRACKINGen
dc.subjectSTABILIZATIONen
dc.subjectTUTORIALen
dc.subjectSYSTEMSen
dc.subjectEngineering, Aerospaceen
dc.subjectEngineering, Electrical & Electronicen
dc.subjectTelecommunicationsen
dc.subject.otherBacksteppingen
dc.subject.otherAerodynamicsen
dc.subject.otherAtmospheric modelingen
dc.subject.otherMathematical modelen
dc.subject.otherForceen
dc.subject.otherSliding mode controlen
dc.subject.otherSimulationen
dc.subject.otherNonlinear controlen
dc.subject.otherbackstepping (BS)en
dc.subject.othersliding mode control (SMC)en
dc.subject.otherairshipen
dc.subject.otherunmanned aerial vehicles (UAVs)en
dc.subject.otherSTATION-KEEPING CONTROLen
dc.subject.otherTRAJECTORY TRACKINGen
dc.subject.otherPOSITIONING CONTROLen
dc.subject.otherPATH-TRACKINGen
dc.subject.otherSTABILIZATIONen
dc.subject.otherTUTORIALen
dc.subject.otherSYSTEMSen
dc.subject.otherEngineering, Aerospaceen
dc.subject.otherEngineering, Electrical & Electronicen
dc.subject.otherTelecommunicationsen
dc.titleUnified Backstepping Sliding Mode Framework for Airship Control Designen
dc.typeArtigo de Periódicopt_BR
dc.identifier.doi10.1109/TAES.2020.2975525
dc.description.affiliationUniversidade Estadual de Campinas
dc.description.affiliationInstituto Maua de Tecnologia
dc.description.affiliationUniversidade Federal de Amazonas
dc.identifier.wosWOS:000556829700056
dc.contributor.orcidHughes Carvalho, Jose Reginaldo/0000-0002-3828-7233
dc.contributor.orcidPaiva, Ely/0000-0002-9205-9688
dc.citation.issue4
dc.citation.epage3258
dc.citation.spage3246
dc.citation.volume56


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