Hybrid Kalman filter approach for aircraft engine in-flight diagnostics: Sensor fault detection case

Journal of Engineering for Gas Turbines and Power

Volumn 129, Issue 3, 2007, Pages 746-754

  Kobayashi, Takahisa ^a   Simon, Donald L ^b  

^a ASRC Aerospace Corp   (United States)

^b NASA GLENN RESEARCH CENTER   (United States)

Author keywords

Flight safety; In flight fault detection; Kalman filter; On board engine model

Indexed keywords

COMPUTER SIMULATION; FAILURE ANALYSIS; FAULT DETECTION; KALMAN FILTERS; PIECEWISE LINEAR TECHNIQUES;

IN-FLIGHT SENSOR FAULT DETECTION; ON-BOARD ENGINE MODEL;

AIRCRAFT ENGINES;

AIRCRAFT ENGINES; COMPUTER SIMULATION; FAILURE ANALYSIS; FAULT DETECTION; KALMAN FILTERS; PIECEWISE LINEAR TECHNIQUES;

EID: 34848918450     PISSN: 07424795     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.2718572     Document Type: Article

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