DocumentCode
2196536
Title
Nonlinear tracking control of the VTOL aircraft
Author
Setlur, P. ; Dawson, D. ; Fang, Y. ; Costic, B.
Author_Institution
Dept. of Electr. & Comput. Eng., Clemson Univ., SC, USA
Volume
5
fYear
2001
fDate
2001
Firstpage
4592
Abstract
In this paper, we present a nonlinear tracking controller for the nonminimum-phase, underactuated model of a vertical take off and landing (VTOL) aircraft. Specifically, the controller is designed to ensure that the VTOL aircraft position/orientation tracks a reference signal generator. The controller ensures that the position/orientation tracking error can be exponentially forced into an arbitrarily small neighborhood around zero (i.e., globally uniformly ultimately bounded (GUUB) tracking)
Keywords
aircraft control; control system synthesis; nonlinear control systems; tracking; GUUB tracking; VTOL aircraft; globally uniformly ultimately bounded tracking; nonlinear tracking control; nonminimum-phase underactuated model; reference signal generator tracking; Aerospace control; Aerospace engineering; Aircraft propulsion; Error correction; Force control; Linear approximation; Open loop systems; Optimal control; Signal design; Signal generators;
fLanguage
English
Publisher
ieee
Conference_Titel
Decision and Control, 2001. Proceedings of the 40th IEEE Conference on
Conference_Location
Orlando, FL
Print_ISBN
0-7803-7061-9
Type
conf
DOI
10.1109/.2001.980928
Filename
980928
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