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Stability of gain scheduling control for aircraft with highly nonlinear behavior

dc.contributor.authorMéndez Vergara, Fany
dc.contributor.authorCervantes Camacho, Ilse
dc.contributor.authorMendoza Torres, Ruby Angélica
dc.date.accessioned2018-03-08T17:44:10Z
dc.date.available2018-03-08T17:44:10Z
dc.date.issued2014
dc.identifier.citationFany Mendez-Vergara, Ilse Cervantes, and Angelica Mendoza-Torres, Stability of Gain Scheduling Control for Aircraft with Highly Nonlinear Behavior, Mathematical Problems in Engineering, vol. 2014, Article ID 906367, 12 pages, 2014. doi:10.1155/2014/906367
dc.identifier.urihttp://hdl.handle.net/11627/3407
dc.description.abstract"The main goal of this work is to study the stability properties of an aircraft with nonlinear behavior, controlled using a gain scheduled approach. An output feedback is proposed which is able to guarantee asymptotical stability of the task-coordinates origin and safety of the operation in the entire flight envelope. The results are derived using theory of hybrid and singular perturbed systems. It is demonstrated that both body velocity and orientation asymptotic tracking can be obtained in spite of nonlinearities and uncertainty. The results are illustrated using numerical simulations in F16 jet."
dc.publisherHindawi
dc.rightsAttribution-NonCommercial-NoDerivatives 4.0 Internacional
dc.rights.urihttp://creativecommons.org/licenses/by-nc-nd/4.0/
dc.subject.classificationMATEMÁTICAS
dc.titleStability of gain scheduling control for aircraft with highly nonlinear behavior
dc.typearticle
dc.identifier.doihttp://dx.doi.org/10.1155/2014/906367
dc.rights.accessAcceso Abierto


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Attribution-NonCommercial-NoDerivatives 4.0 Internacional
Except where otherwise noted, this item's license is described as Attribution-NonCommercial-NoDerivatives 4.0 Internacional