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Adaptive Output Tracking Control for Nonlinear Systems with Failed Actuators and Aircraft Flight System Applications
Joint Authors
Hou, Chuanjing
Hu, Lisheng
Zhang, Yingwei
Source
Mathematical Problems in Engineering
Issue
Vol. 2015, Issue 2015 (31 Dec. 2015), pp.1-14, 14 p.
Publisher
Hindawi Publishing Corporation
Publication Date
2015-05-21
Country of Publication
Egypt
No. of Pages
14
Main Subjects
Abstract EN
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.
American Psychological Association (APA)
Hou, Chuanjing& Hu, Lisheng& Zhang, Yingwei. 2015. Adaptive Output Tracking Control for Nonlinear Systems with Failed Actuators and Aircraft Flight System Applications. Mathematical Problems in Engineering،Vol. 2015, no. 2015, pp.1-14.
https://search.emarefa.net/detail/BIM-1073589
Modern Language Association (MLA)
Hou, Chuanjing…[et al.]. Adaptive Output Tracking Control for Nonlinear Systems with Failed Actuators and Aircraft Flight System Applications. Mathematical Problems in Engineering No. 2015 (2015), pp.1-14.
https://search.emarefa.net/detail/BIM-1073589
American Medical Association (AMA)
Hou, Chuanjing& Hu, Lisheng& Zhang, Yingwei. Adaptive Output Tracking Control for Nonlinear Systems with Failed Actuators and Aircraft Flight System Applications. Mathematical Problems in Engineering. 2015. Vol. 2015, no. 2015, pp.1-14.
https://search.emarefa.net/detail/BIM-1073589
Data Type
Journal Articles
Language
English
Notes
Includes bibliographical references
Record ID
BIM-1073589