Development of a detection scheme for aircraft engine failures based on the artificial immune system paradigm

AIAA Guidance, Navigation, and Control Conference

Volumn , Issue , 2010, Pages

  Perhinschi, Mario G ^a,b   Porter, Jaclyn ^a,b   Moncayo, Hever ^a,b   Davis, Jennifer ^a,b   Wayne, W Scott ^a,b  

^a WEST VIRGINIA UNIVERSITY   (United States)

^b Dept of Mechanical and Aerospace Engineering ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ABNORMAL CONDITIONS; AIRCRAFT JET ENGINES; ARTIFICIAL IMMUNE SYSTEM; BURNER FUEL; DETECTION RATES; DETECTION SCHEME; ENGINE FAILURES; FALSE ALARMS; FLIGHT SIMULATION; INTERACTIVE DESIGN; LOW-PRESSURE TURBINES; PRESSURE RATIO; SENSOR FAILURE; SIMULATION ENVIRONMENT; SPOOL SPEED; STATIC PRESSURE; SYSTEM DEVELOPMENT; SYSTEM SIMULATION MODELS; WEST VIRGINIA UNIVERSITIES;

ACTUATORS; AIRCRAFT ENGINES; DATA PROCESSING; FLIGHT SIMULATORS; IMMUNOLOGY; JET ENGINES; MIXERS (MACHINERY); NASA; SENSORS;

AIRCRAFT DETECTION;

EID: 84867777590     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2010-7740     Document Type: Conference Paper

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