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dc.contributor.advisorRivas Rivas, Damiánes
dc.contributor.advisorPérez-Saborid Sánchez-Pastor, Migueles
dc.creatorFranco Espín, Antonioes
dc.date.accessioned2014-11-27T11:46:42Z
dc.date.available2014-11-27T11:46:42Z
dc.date.issued2014es
dc.identifier.citationFranco Espín, A. (2014). Aircraft trajectory optimization using singular optimal control theory. (Tesis Doctoral Inédita). Universidad de Sevilla, Sevilla.
dc.identifier.urihttp://hdl.handle.net/11441/15236
dc.description.abstractThe optimization of aircraft trajectories using the theory of singular optimal control is studied in this thesis. To describe the aircraft motion, a general nonlinear 3-degree-of-freedom point-mass model is adopted, along with realistic aerodynamic and pres
dc.formatapplication/pdfes
dc.language.isoenges
dc.rightsAtribución-NoComercial-SinDerivadas 4.0 España
dc.rights.urihttp://creativecommons.org/licenses/by-nc-nd/4.0/
dc.subjectIngeniería mecánicaes
dc.titleAircraft trajectory optimization using singular optimal control theoryes
dc.typeinfo:eu-repo/semantics/doctoralThesises
dc.rights.accessrightsinfo:eu-repo/semantics/openAccess
dc.contributor.affiliationUniversidad de Sevilla. Departamento de Ingeniería Aeroespacial y Mecánica de Fluidoses
idus.format.extent134 p.es
dc.identifier.idushttps://idus.us.es/xmlui/handle/11441/15236

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Except where otherwise noted, this item's license is described as: Atribución-NoComercial-SinDerivadas 4.0 España