Finite-Time Adaptive Fault-Tolerant Control for Airfoil Flutter of Reentry Vehicle
Publication: Journal of Aerospace Engineering
Volume 31, Issue 2
Abstract
This paper presents a finite-time adaptive fault-tolerant control method for a two-dimensional airfoil flutter with parameter uncertainties and external disturbances. Sensor and actuator faults are both considered. Flutter motion equations of an airfoil with cubic hard spring nonlinearity are established based on the trajectory optimization for reentry vehicle. A finite-time adaptive fault-tolerant controller is designed to deal with the airfoil flutter. The stability of the proposed controller is proved theoretically. Numerical simulations are given to demonstrate the effectiveness of the scheme.
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Acknowledgments
This work is supported by the Natural Science Foundation of China (11772187) and the Natural Science Foundation of Shanghai (16ZR1436200).
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Information & Authors
Information
Published In
Journal of Aerospace Engineering
Volume 31 • Issue 2 • March 2018
Copyright
©2017 American Society of Civil Engineers.
History
Received: Dec 2, 2014
Accepted: Jun 28, 2017
Published online: Nov 22, 2017
Published in print: Mar 1, 2018
Discussion open until: Apr 22, 2018
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