Aircraft failure detection and identification over an extended flight envelope using an artificial immune system

Aeronautical Journal

Volumn 115, Issue 1163, 2011, Pages 43-55

  Moncayo, H ^a   Perhinschi, M G ^a   Davis, J ^a  

^a WEST VIRGINIA UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ADAPTIVE CONTROL SYSTEMS; DEEP NEURAL NETWORKS; FLIGHT ENVELOPES; FLIGHT SIMULATORS; FRACTURE MECHANICS; IMMUNE SYSTEM; NEURAL NETWORKS; SUPERSONIC AIRCRAFT;

ABNORMAL CONDITIONS; ARTIFICIAL IMMUNE SYSTEM; DETECTION AND IDENTIFICATIONS; DIRECT ADAPTIVE CONTROL; INTEGRATED ARTIFICIAL IMMUNE SYSTEMS; NONLINEAR DYNAMIC INVERSION; SELF CONFIGURATION; STRUCTURAL FAILURE;

AIRCRAFT DETECTION;

EID: 79551641337     PISSN: 00019240     EISSN: None     Source Type: Journal    
DOI: 10.1017/S0001924000005352     Document Type: Article

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