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Stability of gain scheduling control for aircraft with highly nonlinear behavior
FANY MÉNDEZ VERGARA
ILSE CERVANTES CAMACHO
RUBY ANGELICA MENDOZA TORRES
Acceso Abierto
Atribución-NoComercial-SinDerivadas
http://dx.doi.org/10.1155/2014/906367
"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."
Hindawi Publishing Corporation
2014
Artículo
Inglés
Público en general
Fany 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
MATEMÁTICAS
Versión publicada
publishedVersion - Versión publicada
Aparece en las colecciones: Publicaciones Científicas Control y Sistemas Dinámicos

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