Reconfigurable flight control on sliding modes addressing actuator deflection and deflection rate saturation

1998 Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 1998, Pages 127-137

  Shtessel, Y ^a   Buffington, J ^b   Pachter, M ^c   Chandler, P ^b   Banda, S ^b  

^a UNIVERSITY OF ALABAMA IN HUNTSVILLE   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

^c AIR FORCE INSTITUTE OF TECHNOLOGY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; AIRCRAFT CONTROL; AIRCRAFT DETECTION; BOUNDARY LAYERS; DAMAGE DETECTION; DEFLECTION (STRUCTURES); FLIGHT DYNAMICS; SLIDING MODE CONTROL; SUPERSONIC AIRCRAFT;

AIRCRAFT FLIGHT CONTROL; CONTINUOUS SLIDING MODES; CONTROL STRATEGIES; MULTIPLE TIME SCALE; NONLINEAR FLIGHT DYNAMICS; RECONFIGURABLE FLIGHT CONTROL; SLIDING MODE CONTROLLER; TRACKING PERFORMANCE;

CONTROLLERS;

EID: 84959120804     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-4112     Document Type: Conference Paper

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