Stability of Gain Scheduling Control for Aircraft with Highly Nonlinear Behavior
Joint Authors
Mendoza-Torres, Angelica
Camacho, Ilse Cervantes
Mendez-Vergara, Fany
Source
Mathematical Problems in Engineering
Issue
Vol. 2014, Issue 2014 (31 Dec. 2014), pp.1-12, 12 p.
Publisher
Hindawi Publishing Corporation
Publication Date
2014-05-20
Country of Publication
Egypt
No. of Pages
12
Main Subjects
Abstract EN
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.
American Psychological Association (APA)
Mendez-Vergara, Fany& Camacho, Ilse Cervantes& Mendoza-Torres, Angelica. 2014. Stability of Gain Scheduling Control for Aircraft with Highly Nonlinear Behavior. Mathematical Problems in Engineering،Vol. 2014, no. 2014, pp.1-12.
https://search.emarefa.net/detail/BIM-507009
Modern Language Association (MLA)
Mendez-Vergara, Fany…[et al.]. Stability of Gain Scheduling Control for Aircraft with Highly Nonlinear Behavior. Mathematical Problems in Engineering No. 2014 (2014), pp.1-12.
https://search.emarefa.net/detail/BIM-507009
American Medical Association (AMA)
Mendez-Vergara, Fany& Camacho, Ilse Cervantes& Mendoza-Torres, Angelica. Stability of Gain Scheduling Control for Aircraft with Highly Nonlinear Behavior. Mathematical Problems in Engineering. 2014. Vol. 2014, no. 2014, pp.1-12.
https://search.emarefa.net/detail/BIM-507009
Data Type
Journal Articles
Language
English
Notes
Includes bibliographical references
Record ID
BIM-507009
