Disturbance attenuation in fault detection of gas turbine engines: A discrete robust observer design

IEEE Transactions on Systems, Man and Cybernetics Part C: Applications and Reviews

Volumn 39, Issue 2, 2009, Pages 234-239

  Dai, Xuewu ^a,b   Gao, Zhiwei ^c   Breikin, Tim ^b   Wang, Hong ^b  

^a SOUTHWEST UNIVERSITY   (China)

^b UNIVERSITY OF MANCHESTER   (United Kingdom)

^c TIANJIN UNIVERSITY   (China)

Author keywords

Fast Fourier transformation (FFT); Fault detection; Gas turbine engine (GTE); Robust observer design

Indexed keywords

AIRCRAFT PROPULSION; EIGENVALUES AND EIGENFUNCTIONS; ENGINES; FAST FOURIER TRANSFORMS; FAULT DETECTION; FOURIER ANALYSIS; GAS TURBINES; GASES; TURBOMACHINERY;

ACTUATOR FAULT DETECTIONS; COMPUTATION COMPLEXITY; COMPUTATION RESOURCES; DISTURBANCE ATTENUATIONS; DISTURBANCE FREQUENCIES; EIGEN VALUES; EIGENVALUE OPTIMIZATIONS; EIGENVECTOR ASSIGNMENTS; EXISTING METHODS; FAST FOURIER TRANSFORMATION (FFT); FREE PARAMETERS; FREQUENCY INFORMATIONS; GAS TURBINE ENGINE (GTE); LOCAL OPTIMAL SOLUTIONS; ON-BOARD FAULT DETECTIONS; PERFORMANCE INDEXES; ROBUST OBSERVER DESIGN;

FREQUENCY ESTIMATION;

EID: 63049092691     PISSN: 10946977     EISSN: None     Source Type: Journal    
DOI: 10.1109/TSMCC.2008.2005845     Document Type: Article

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