Adaptive output tracking control for nonlinear systems with failed actuators and aircraft flight system applications
type: Item
instance of: scholarly article
title: Adaptive output tracking control for nonlinear systems with failed actuators and aircraft flight system applications
zbMATH Open document ID: 1394.93128
DOI: 10.1155/2015/357078
author: Chuanjing Hou
author: Yingwei Zhang
author: Li-Sheng Hu
published in: Mathematical Problems in Engineering
publication date: 2018-08-27T00:00:00Z
review text: Summary: An adaptive failure compensation scheme using output feedback is proposed for a class of nonlinear systems with nonlinearities depending on the unmeasured states of systems. Adaptive high-gain K-filters are presented to suppress the nonlinearities while the proposed backstepping adaptive high-gain controller guarantees the stability of the closed-loop system and small tracking errors. Simulation results verify that the adaptive failure compensation scheme is effective.
Mathematics Subject Classification ID: 93C40
zbMATH DE Number: 6926134
Wikidata QID: Q59118141
MaRDI profile type: Publication
full work available at URL: https://doi.org/10.1155/2015/357078
OpenAlex ID: W1479816163
cites work: Q4828908
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description: scientific article; zbMATH DE number 6926134