NDLI: Fault Tolerant Flight Control Law Design with a Model-Following Sliding Mode Controller

Content Provider	IEEE Xplore Digital Library
Author	Yang Zhi-jun Qi Xiao-hui Shan Gan-lin
Copyright Year	2009
Abstract	A sliding mode controller based on model following control is designed for the flight control system with uncertainties and perturbations. With this controller, the controlled plant can track the reference model precisely. It is shown that this scheme provides better performance for the flight control system and the fault tolerant control objective is achieved. The proposed scheme has the advantages of the model following and sliding-mode control. A Proportional-Integral type sliding surface is designed through pole placement method to make the sliding mode have good dynamic characteristics and to eliminate the steady state error. The simple saturation control is adopted to weaken the chattering phenomena. The simulation results show that the flight control system using this controller not only doesn’t require the procedure of fault detection and isolation, but also achieves the model following.
Starting Page	665
Ending Page	668
File Size	262203
Page Count	4
File Format	PDF
ISBN	9780769535838
DOI	10.1109/ICMTMA.2009.526
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2009-04-11
Publisher Place	China
Access Restriction	Subscribed
Rights Holder	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Subject Keyword	State feedback Uncertainty sliding mode control Control systems Steady-state Sliding mode control Aerospace control Fault tolerance model following control fault tolerant flight control Fault tolerant systems Aerospace simulation Control system synthesis
Content Type	Text
Resource Type	Article

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