DocumentCode
2114807
Title
Discrete-time actuator fault estimation design for flight control application
Author
Yee, Jiong-Sang ; Jiang, Bin ; Wang, Jim Liang ; Li, Yan
Author_Institution
Sch. of Electr. & Electron. Eng., Nanyang Technol. Univ., Singapore
Volume
3
fYear
2002
fDate
2-5 Dec. 2002
Firstpage
1287
Abstract
This paper proposes a new discrete-time fault estimation scheme that deals with multiple, simultaneous and abrupt actuator failures. The proposed actuator fault estimation scheme is applied to design a fault-tolerant H∞ flight controller for a combat aircraft in tracking bank-angle and pitch-rate commands with zero lateral acceleration. Simulation results demonstrate good performance using the fault-tolerant H∞ flight controller.
Keywords
H∞ control; actuators; aircraft control; control system synthesis; controllers; discrete time systems; fault diagnosis; fault tolerance; actuator failures; actuator fault estimation scheme; bank angle; discrete time fault estimation scheme; fault tolerant H∞ flight controller; flight control application; pitch rate; zero latent acceleration; Aerospace control; Aerospace electronics; Aerospace engineering; Aircraft; Control systems; Fault detection; Fault tolerance; Hydraulic actuators; State estimation; Testing;
fLanguage
English
Publisher
ieee
Conference_Titel
Control, Automation, Robotics and Vision, 2002. ICARCV 2002. 7th International Conference on
Print_ISBN
981-04-8364-3
Type
conf
DOI
10.1109/ICARCV.2002.1234958
Filename
1234958
Link To Document