DocumentCode :
44566
Title :
Model predictive control-based non-linear fault tolerant control for air-breathing hypersonic vehicles
Author :
Xiaoxiang Hu ; Karimi, Hamid Reza ; Ligang Wu ; Yang Guo
Author_Institution :
Xi´an Res. Inst. of High-tech, Xi´an, China
Volume :
8
Issue :
13
fYear :
2014
fDate :
September 4 2014
Firstpage :
1147
Lastpage :
1153
Abstract :
In this study, a model predictive control (MPC)-based fault tolerant control (FTC) design method for air-breathing hypersonic vehicles (AHVs) is proposed. The non-linear model of AHVs is recalled and the FTC problem is discussed. The problem is challenging because the relationship between flight dynamics and the control input is not so clear. For the purpose of non-linear FTC, an optimisation-based reference reconfiguration method is given. Through the reconfiguration, a new reference command, which can be realised by the faulty system, is constructed. Actuator saturation has been take into account when constructing the new reference command. An MPC-based controller reconfiguration method is proposed with respect to the new command and system faults. Finally, simulations are given to show the effectiveness of the proposed control method.
Keywords :
actuators; aircraft control; control system synthesis; fault tolerant control; nonlinear control systems; predictive control; AHV; MPC-based FTC design method; MPC-based controller reconfiguration method; actuator saturation; air-breathing hypersonic vehicles; control input; flight dynamics; model predictive control; nonlinear fault tolerant control; optimisation-based reference reconfiguration method; reference command;
fLanguage :
English
Journal_Title :
Control Theory & Applications, IET
Publisher :
iet
ISSN :
1751-8644
Type :
jour
DOI :
10.1049/iet-cta.2013.0986
Filename :
6882891
Link To Document :
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