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On Nonlinear Dynamics and an Optimal Control Design to a Longitudinal Flight

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dc.contributor.authorPereira, Danilo Carlos
dc.contributor.authorBalthazar, José Manoel [UNESP]
dc.contributor.authorChavarette, Fábio Roberto
dc.contributor.authorRafikov, Marat
dc.contributor.institutionUniversidade Estadual de Campinas (UNICAMP)
dc.contributor.institutionUniversidade Estadual Paulista (Unesp)
dc.contributor.institutionUniv Ijui
dc.date.accessioned2013-09-30T18:14:14Z
dc.date.accessioned2014-05-20T14:16:08Z
dc.date.available2013-09-30T18:14:14Z
dc.date.available2014-05-20T14:16:08Z
dc.date.issued2008-01-01
dc.description.abstractIn this work, we analyzed a bifurcational behavior of a longitudinal flight nonlinear dynamics, taking as an example the F-8 aircraft Crusader. We deal with an analysis of high angles of attack in order to stabilize the oscillations; those were close to the critical angle of the aircraft, in the flight conditions, established. We proposed a linear optimal control design applied to the considered nonlinear aircraft model below angle of stall, taking into account regions of Hopf and saddled noddle bifurcations.en
dc.description.affiliationFEM UNICAMP, Dept Mech Design DPM, BR-13083970 Campinas, SP, Brazil
dc.description.affiliationUNESP Rio Claro, BR-13230560 São Paulo, Brazil
dc.description.affiliationUniv Ijui, BR-98700000 Rio Grande do Sul, Brazil
dc.description.affiliationUnespUNESP Rio Claro, BR-13230560 São Paulo, Brazil
dc.format.extent6
dc.identifierhttp://dx.doi.org/10.1115/1.2802111
dc.identifier.citationJournal of Computational and Nonlinear Dynamics. New York: Asme-amer Soc Mechanical Eng, v. 3, n. 1, p. 6, 2008.
dc.identifier.doi10.1115/1.2802111
dc.identifier.issn1555-1423
dc.identifier.lattes5723359885365339
dc.identifier.orcid0000-0002-1203-7586
dc.identifier.urihttp://hdl.handle.net/11449/24856
dc.identifier.wosWOS:000260001900012
dc.language.isoeng
dc.publisherAsme-amer Soc Mechanical Eng
dc.relation.ispartofJournal of Computational and Nonlinear Dynamics
dc.relation.ispartofjcr1.996
dc.relation.ispartofsjr0,791
dc.rights.accessRightsAcesso restrito
dc.sourceWeb of Science
dc.subjectF-8 aircraft Crusaderen
dc.subjectbifurcationsen
dc.subjectoptimal linear control designen
dc.titleOn Nonlinear Dynamics and an Optimal Control Design to a Longitudinal Flighten
dc.typeArtigo
dcterms.licensehttp://journaltool.asme.org/Content/AuthorResources.cfm
dcterms.rightsHolderAsme-amer Soc Mechanical Eng
dspace.entity.typePublication
unesp.author.lattes5723359885365339(3)
unesp.author.orcid0000-0002-1203-7586(3)
unesp.campusUniversidade Estadual Paulista (UNESP), Instituto de Geociências e Ciências Exatas, Rio Claropt
unesp.campusUniversidade Estadual Paulista (UNESP), Faculdade de Engenharia, Ilha Solteirapt
unesp.departmentMatemática - FEISEstatística, Matemática Aplicada e Computação - IGCEpt

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Coleções

Rio Claro - IGCE - Instituto de Geociências e Ciências Exatas
Ilha Solteira - FEIS - Faculdade de Engenharia