DocumentCode :
581584
Title :
Non-fragile adaptive fault-tolerant controller design for an airbreathing hypersonic vehicle
Author :
Haibin, Sun ; Shihua, Li ; Changyin, Sun
fYear :
2012
fDate :
25-27 July 2012
Firstpage :
453
Lastpage :
458
Abstract :
This paper concerns the problem of non-fragile fault-tolerant control for the longitudinal dynamics of an airbreathing hypersonic vehicle under external disturbances. And a corresponding non-fragile adaptive fault-tolerant control scheme is proposed for the longitudinal dynamics. In this approach, two adaptive laws are employed to estimate the minimum value of the actuation effectiveness factor and the upper bound of external disturbances, respectively. For the designers, the real minimum value of the actuation effectiveness factor and the upper bound of external disturbances are not required to be known in advance, then the robustness to the actuator faults and external disturbances is guaranteed. Simulation results are given to show the effectiveness of the proposed method finally.
Keywords :
actuators; adaptive control; aircraft control; control system synthesis; fault tolerance; vehicle dynamics; actuator fault robustness; adaptive laws; airbreathing hypersonic vehicle; longitudinal dynamics; minimum actuation effectiveness factor value; nonfragile adaptive fault-tolerant controller design; robust external disturbance upper bound; Actuators; Educational institutions; Fault tolerance; Fault tolerant systems; Robustness; Upper bound; Vehicles; Airbreathing hypersonic vehicles; adaptive control; fault-tolerant control; non-fragile;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control Conference (CCC), 2012 31st Chinese
Conference_Location :
Hefei
ISSN :
1934-1768
Print_ISBN :
978-1-4673-2581-3
Type :
conf
Filename :
6389972
Link To Document :
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