An adaptive threshold approach for the design of an actuator failure detection and identification scheme

IEEE Transactions on Control Systems Technology

Volumn 14, Issue 3, 2006, Pages 519-525

  Perhinschi, Mario G ^a   Napolitano, Marcello R ^a   Campa, Giampiero ^a   Seanor, Brad ^a   Burken, John ^b   Larson, Richard ^b  

^a West Virginia University   (United States)

^b NASA DRYDEN FLIGHT RESEARCH CENTER   (United States)

Author keywords

Actuator failure detection; Aicraft control; Failure analysis; Flight safety; Neural network

Indexed keywords

ACCIDENT PREVENTION; ADAPTIVE CONTROL SYSTEMS; AIRCRAFT; ALGORITHMS; FAILURE (MECHANICAL); FAILURE ANALYSIS; NEURAL NETWORKS;

ACTUATOR FAILURE DETECTION; ADAPTIVE THRESHOLD APPROACH; AIRCRAFT ACTUATOR; AIRCRAFT CONTROL; FLIGHT SAFETY;

ACTUATORS;

EID: 33646023118     PISSN: 10636536     EISSN: None     Source Type: Journal    
DOI: 10.1109/TCST.2005.860522     Document Type: Article

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