Immunity - Based aircraft failure detection and identification using an integrated hierarchical multi-self strategy

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2009, Pages

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

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: 78049241579     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2009-5878     Document Type: Conference Paper

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