International Journal of Control, Automation and Systems 2018; 16(4): 1989-2001
Published online April 3, 2018
https://doi.org/10.1007/s12555-017-0641-x
© The International Journal of Control, Automation, and Systems
This paper proposes a neural-networks(NN)-based adaptive controller for an uncertain nonlinear system with asymptotic stability. While the satisfactory performance of the NN-based adaptive controller is validated well in various uncertain nonlinear systems, the stability is commonly restricted to the uniformly ultimate boundedness( UUB). To improve the UUB of the NN-based adaptive control to the asymptotically stability(AS) with continuous control, the existing NN-based adaptive controller is augmented with a robust-integral-signum-error (RISE) feedback term, and overall closed-loop stability is rigorously analyzed by modifying the typical stability analysis for the RISE feedback control. To demonstrate the effectiveness of the proposed controller, numerical simulations for a fault tolerant flight control with a nonlinear F-16 aircraft model are performed."
Keywords Adaptive control, asymptotic stability, fault tolerant flight control, neural network, RISE feedback.
International Journal of Control, Automation and Systems 2018; 16(4): 1989-2001
Published online August 1, 2018 https://doi.org/10.1007/s12555-017-0641-x
Copyright © The International Journal of Control, Automation, and Systems.
Jongho Shin, Seungkeun Kim*, and Antonios Tsourdos
Chungnam National University
This paper proposes a neural-networks(NN)-based adaptive controller for an uncertain nonlinear system with asymptotic stability. While the satisfactory performance of the NN-based adaptive controller is validated well in various uncertain nonlinear systems, the stability is commonly restricted to the uniformly ultimate boundedness( UUB). To improve the UUB of the NN-based adaptive control to the asymptotically stability(AS) with continuous control, the existing NN-based adaptive controller is augmented with a robust-integral-signum-error (RISE) feedback term, and overall closed-loop stability is rigorously analyzed by modifying the typical stability analysis for the RISE feedback control. To demonstrate the effectiveness of the proposed controller, numerical simulations for a fault tolerant flight control with a nonlinear F-16 aircraft model are performed."
Keywords: Adaptive control, asymptotic stability, fault tolerant flight control, neural network, RISE feedback.
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