DocumentCode :
603444
Title :
Nonlinear Controllers Applied to Fixed-Wing UAV
Author :
Espinoza, T. ; Dzul, A. ; Garcia, Luis ; Parada, R.
Author_Institution :
Div. de Estudios de Posgrado e Investig., Inst. Tecnol. de la Laguna, Torreón, Mexico
fYear :
2012
fDate :
19-23 Nov. 2012
Firstpage :
243
Lastpage :
248
Abstract :
This article presents a comparison of controllers which have been applied to a fixed-wing UAV (Unmanned Aerial Vehicle). The comparison is realized between the following nonlinear controllers techniques: sliding modes, nested saturations and back stepping. These controllers are compared and analyzed for altitude, yaw and roll by using simulation tests.
Keywords :
aerospace components; autonomous aerial vehicles; nonlinear control systems; backstepping; fixed wing UAV; nested saturation; nonlinear controller technique; sliding mode controller; unmanned aerial vehicle; backstepping control; fixed-wing UAV; nested saturations control; sliding modes control;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Electronics, Robotics and Automotive Mechanics Conference (CERMA), 2012 IEEE Ninth
Conference_Location :
Cuernavaca
Print_ISBN :
978-1-4673-5096-9
Type :
conf
DOI :
10.1109/CERMA.2012.46
Filename :
6524585
Link To Document :
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