Please use this identifier to cite or link to this item: https://hdl.handle.net/2440/82166
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Type: Journal article
Title: Robust fault tolerant tracking controller design for a VTOL aircraft
Author: Chadli, M.
Aouaouda, S.
Karimi, H.
Shi, P.
Citation: Journal of the Franklin Institute, 2013; 350(9):2627-2645
Publisher: Pergamon-Elsevier Science Ltd
Issue Date: 2013
ISSN: 0016-0032
1879-2693
Statement of
Responsibility: 
M. Chadli, S. Aouaouda, H.R. Karimi, P. Shi
Abstract: This paper deals with the fault tolerant control (FTC) design for a Vertical Takeoff and Landing (VTOL) aircraft subject to external disturbances and actuator faults. The aim is to synthesize a fault tolerant controller ensuring trajectory tracking for the nonlinear uncertain system represented by a Takagi-Sugeno (T-S) model. In order to design the FTC law, a proportional integral observer (PIO) is adopted which estimate both of the faults and the faulty system states. Based on the Lyapunov theory and ℓ2 optimization, the trajectory tracking performance and the stability of the closed loop system are analyzed. Sufficient conditions are obtained in terms of linear matrix inequalities (LMI). Simulation results show that the proposed controller is robust with respect to uncertainties on the mechanical parameters that characterize the model and secures global convergence. © 2012 The Franklin Institute.
Rights: Copyright © 2012 The Franklin Institute.
DOI: 10.1016/j.jfranklin.2012.09.010
Appears in Collections:Aurora harvest
Electrical and Electronic Engineering publications

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