DocumentCode :
2468158
Title :
A Poincaré map approach for the exact tracking of a nonlinear non-minimum phase system: the VTOL aircraft
Author :
Consolini, Luca ; Tosques, Mario
Author_Institution :
Dipt. di Ingegneria dell´´Informazione, Parco Area delle Sci., Parma
fYear :
2006
fDate :
13-15 Dec. 2006
Firstpage :
1788
Lastpage :
1793
Abstract :
This article considers the problem of open-loop exact tracking for the VTOL aircraft with respect to the nominal output. It is shown that if the norm of the acceleration of the reference curve is lower than k mg, where g is the gravity acceleration and km sime 0.2688, then there exists a special initial state such that the internal dynamics are bounded. The bounding term is directly proportional to the maximum norm of the acceleration of the reference trajectory
Keywords :
Poincare mapping; acceleration control; aircraft control; nonlinear control systems; open loop systems; position control; tracking; Poincare map approach; VTOL aircraft; gravity acceleration; internal dynamics; nonlinear nonminimum phase system; open-loop exact tracking; reference curve; reference trajectory; Acceleration; Aerospace control; Aircraft; Control nonlinearities; Control systems; Force control; Gravity; Nonlinear control systems; Trajectory; Velocity control;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Decision and Control, 2006 45th IEEE Conference on
Conference_Location :
San Diego, CA
Print_ISBN :
1-4244-0171-2
Type :
conf
DOI :
10.1109/CDC.2006.377775
Filename :
4177244
Link To Document :
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