Aircraft failure detection and identification using an immunological hierarchical multiself strategy

Journal of Guidance, Control, and Dynamics

Volumn 33, Issue 4, 2010, Pages 1105-1114

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

^a WEST VIRGINIA UNIVERSITY   (United States)

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

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ADAPTIVE CONTROL SYSTEMS; FAILURE (MECHANICAL); FLIGHT ENVELOPES; FLIGHT SIMULATORS; FRACTURE MECHANICS; NEURAL NETWORKS; SUPERSONIC AIRCRAFT;

ABNORMAL CONDITIONS; ADAPTIVE CONTROL LAW; DETECTION AND IDENTIFICATIONS; DEVELOPMENT AND APPLICATIONS; INTEGRATED ARTIFICIAL IMMUNE SYSTEMS; NONLINEAR DYNAMIC INVERSION; SELF CONFIGURATION; STRUCTURAL FAILURE;

AIRCRAFT DETECTION;

EID: 77956371625     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/1.47445     Document Type: Article

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