DocumentCode
1913951
Title
Actuator fault compensation for a helicopter model
Author
Yu, Xiac-Hua
Author_Institution
Dept. of Electr. Eng., California Polytech. State Univ., San Luis Obispo, CA, USA
Volume
2
fYear
2003
fDate
23-25 June 2003
Firstpage
1372
Abstract
A fault-tolerant system is the one that can continue its operation without significant impact on performance in the presence of hardware and/or software errors. In this paper, the design of a fault-tolerant flight controller to control UH-60 helicopter is investigated. A 9th-order state space representation of the helicopter model operating at the forward mode with 80 knots is presented; then a fault-tolerant optimal feedback controller is designed and tested.
Keywords
actuators; adaptive control; aircraft control; fault tolerant computing; feedback; helicopters; state-space methods; 9th-order state space representation; UH-60 helicopter; actuator fault compensation; adaptive control; fault-tolerant flight controller; fault-tolerant system; hardware error; helicopter model; optimal feedback controller; software error; Actuators; Control systems; Fault diagnosis; Fault tolerance; Fault tolerant systems; Hardware; Helicopters; Logic testing; NASA; Software performance;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Applications, 2003. CCA 2003. Proceedings of 2003 IEEE Conference on
Print_ISBN
0-7803-7729-X
Type
conf
DOI
10.1109/CCA.2003.1223212
Filename
1223212
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