Integration of fault tolerant system for sensor and actuator failures within the WVU NASA F-15 simulator

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2003, Pages

  Perhinschi, Mario G ^a   Napolitano, Marcello R ^a   Campa, Giampiero ^a   Fravolini, Mario L ^b  

^a West Virginia University   (United States)

^b UNIVERSITY OF PERUGIA   (Italy)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; CONTROL THEORY; FAULT TOLERANCE; FLIGHT CONTROL SYSTEMS; NASA;

ACTUATOR FAILURES; DETECTION AND IDENTIFICATIONS; FAILURE DETECTION; FAULT TOLERANT SCHEMES; FAULT TOLERANT SYSTEMS; INTELLIGENT FLIGHT CONTROL SYSTEMS; NONLINEAR DYNAMIC INVERSION; SENSOR AND ACTUATORS;

SUPERSONIC AIRCRAFT;

EID: 85088759022     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2003-5644     Document Type: Conference Paper

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