DocumentCode
2220047
Title
Output trajectory tracking for a switched nonlinear non-minimum phase system: The VSTOL aircraft
Author
Benosman, M. ; Lum, K.-Y.
Author_Institution
Nat. Univ. of Singapore, Singapore
fYear
2007
fDate
1-3 Oct. 2007
Firstpage
262
Lastpage
269
Abstract
This work concerns output trajectory tracking for the McDonnell Dougglas YAV68B Harrier VSTOL aircraft. This system can perform three distinct flight modes, and is modelled with a Lagrangian nonlinear hybrid non-minimum phase dynamics. Output tracking is solved using classical input/output linearization scheme associated to an internal dynamics stable inversion for each flight mode dynamics. The performance of the global switched control law is discussed and validated through simulation tests.
Keywords
aircraft control; linearisation techniques; nonlinear control systems; position control; time-varying systems; tracking; VSTOL aircraft; flight mode dynamics; input-output linearization; output trajectory tracking; switched nonlinear nonminimum phase system; Aircraft; Control systems; Dynamic equilibrium; Lagrangian functions; Manipulator dynamics; Nonlinear control systems; Nonlinear dynamical systems; Partial differential equations; Robots; Trajectory;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Applications, 2007. CCA 2007. IEEE International Conference on
Conference_Location
Singapore
Print_ISBN
978-1-4244-0442-1
Electronic_ISBN
978-1-4244-0443-8
Type
conf
DOI
10.1109/CCA.2007.4389241
Filename
4389241
Link To Document