A simulation environment for testing and research of neurally augmented fault tolerant control laws based on non-linear dynamic inversion

Collection of Technical Papers - AIAA Modeling and Simulation Technologies Conference

Volumn 1, Issue , 2004, Pages 147-157

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

^a WEST VIRGINIA UNIVERSITY   (United States)

^b UNIVERSITY OF PERUGIA   (Italy)

^c Dept of Mechanical and Aerospace Engineering ^*

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; COMPUTER SIMULATION; CONTROL SYSTEM ANALYSIS; DYNAMICS; ERROR ANALYSIS; FLIGHT DYNAMICS; GRAPHICAL USER INTERFACES; RESEARCH AND DEVELOPMENT MANAGEMENT;

FAULT TOLERANT CONTROL LAWS; INVERSION PARAMETERS; NON-LINEAR DYNAMIC INVERSION; SENSOR FAILURE;

FAULT TOLERANT COMPUTER SYSTEMS;

EID: 19644396280     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2004-4913     Document Type: Conference Paper

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