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

dc.contributorUniversidade Estadual Paulista (UNESP)
dc.creatorPereira, Danilo Carlos
dc.creatorBalthazar, José Manoel
dc.creatorChavarette, Fábio Roberto
dc.creatorRafikov, Marat
dc.date2013-09-30T18:14:14Z
dc.date2014-05-20T14:16:08Z
dc.date2016-10-25T17:39:18Z
dc.date2013-09-30T18:14:14Z
dc.date2014-05-20T14:16:08Z
dc.date2016-10-25T17:39:18Z
dc.date2008-01-01
dc.date.accessioned2017-04-05T22:20:43Z
dc.date.available2017-04-05T22:20:43Z
dc.identifierJournal of Computational and Nonlinear Dynamics. New York: Asme-amer Soc Mechanical Eng, v. 3, n. 1, p. 6, 2008.
dc.identifier1555-1423
dc.identifierhttp://hdl.handle.net/11449/24856
dc.identifierhttp://acervodigital.unesp.br/handle/11449/24856
dc.identifier10.1115/1.2802111
dc.identifierWOS:000260001900012
dc.identifierhttp://dx.doi.org/10.1115/1.2802111
dc.identifier.urihttp://repositorioslatinoamericanos.uchile.cl/handle/2250/869816
dc.descriptionIn 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.
dc.languageeng
dc.publisherAsme-amer Soc Mechanical Eng
dc.relationJournal of Computational and Nonlinear Dynamics
dc.rightsinfo:eu-repo/semantics/closedAccess
dc.subjectF-8 aircraft Crusader
dc.subjectbifurcations
dc.subjectoptimal linear control design
dc.titleOn Nonlinear Dynamics and an Optimal Control Design to a Longitudinal Flight
dc.typeOtro


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