DocumentCode
391275
Title
Control design for the PVTOL aircraft with arbitrary bounds on the acceleration
Author
Castillo, P. ; Lozano, R. ; Fantoni, I. ; Dzul, A.
Author_Institution
Univ. de Technol. de Compiegne, France
Volume
2
fYear
2002
fDate
10-13 Dec. 2002
Firstpage
1717
Abstract
In this paper, a simple control algorithm for the PVTOL aircraft is proposed. The control strategy takes into the account input constraints and does not have any singularities. The control design is such that the acceleration satisfies arbitrary bounds. The stability analysis is proved by using very simple arguments. Satisfactory behavior is shown in simulations.
Keywords
aircraft control; nonlinear control systems; stability; PVTOL aircraft; aircraft control; arbitrary bounds; control algorithm; control design; input constraints; nonlinear systems stabilization; stability analysis; Acceleration; Aerodynamics; Aerospace control; Aircraft propulsion; Analytical models; Control design; Engines; Force control; Stability analysis; State feedback;
fLanguage
English
Publisher
ieee
Conference_Titel
Decision and Control, 2002, Proceedings of the 41st IEEE Conference on
ISSN
0191-2216
Print_ISBN
0-7803-7516-5
Type
conf
DOI
10.1109/CDC.2002.1184768
Filename
1184768
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