Sliding mode control applied to reconfigurable flight control design

40th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2002, Pages

  Hess, R A ^a   Wells, S R ^a  

^a University of California Davis   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; ANGLE OF ATTACK; CONTROLLERS; DESIGN; FREQUENCY DOMAIN ANALYSIS; SLIDING MODE CONTROL; SUPERSONIC AIRCRAFT;

ASYMPTOTIC OBSERVER; FREQUENCY DOMAINS; HIGH ANGLE OF ATTACK; LIMITED BANDWIDTH; PILOT-INDUCED OSCILLATIONS; RECONFIGURABLE FLIGHT CONTROL; SLIDING MODE CONTROLLER; UNMODELED DYNAMICS;

FLIGHT CONTROL SYSTEMS;

EID: 85085402743     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-245     Document Type: Conference Paper

References (23)

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