Artificial-immune-system-based aircraft failure evaluation over extended flight envelope

Journal of Guidance, Control, and Dynamics

Volumn 34, Issue 4, 2011, Pages 989-1001

  Moncayo, Hever ^a,b   Perhinschi, Mario G ^a,b   Davis, Jennifer ^a,b  

^a WEST VIRGINIA UNIVERSITY   (United States)

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

Author keywords

[No Author keywords available]

Indexed keywords

ADAPTIVE CONTROL SYSTEMS; FAILURE (MECHANICAL); FLIGHT SIMULATORS; FORECASTING; IMMUNE SYSTEM; NEURAL NETWORKS; SUPERSONIC AIRCRAFT;

ABNORMAL CONDITIONS; ADAPTIVE CONTROL LAW; AIRCRAFT FAILURES; AIRCRAFT SUBSYSTEMS; ARTIFICIAL IMMUNE SYSTEM; FLIGHT SIMULATION; MAGNITUDE EVALUATION; NONLINEAR DYNAMIC INVERSION;

FLIGHT ENVELOPES;

EID: 79959946126     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/1.52748     Document Type: Article

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