ℒ1 adaptive control augmentation system for the X-48B aircraft

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2009, Pages

  Leman, Tyler ^a   Xargay, Enric ^a   Dullerud, Geir ^a   Hovakimyan, Naira ^a   Wendel, Thomas ^b  

^a UNIVERSITY OF ILLINOIS AT URBANA CHAMPAIGN   (United States)

^b BOEING COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; AIRCRAFT CONTROL; CONTROL SURFACES; CONTROL SYSTEM ANALYSIS; CONTROLLERS; DELAY CONTROL SYSTEMS; FLIGHT CONTROL SYSTEMS; FLIGHT ENVELOPES;

ADAPTIVE CONTROLLERS; CONTROL SURFACE FAILURE; ENTIRE FLIGHT ENVELOPE; GAIN AND PHASE MARGIN; NON-LINEAR ADAPTIVE CONTROLS; STEADY STATE PERFORMANCE; SYSTEMATIC FRAMEWORK; VERIFICATION-AND-VALIDATION;

ADAPTIVE CONTROL SYSTEMS;

EID: 78049266882     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2009-5619     Document Type: Conference Paper

References (14)

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2. Chengyu Cao and Naira Hovakimyan. Guaranteed Transient Performance with ℒ1 Adaptive Controller for Systems with Unknown Time- Varying Parameters and Bounded Disturbances: Part I. In Proc. of American Control Conference, pages 3925-3930, New York, NY, July 2007.
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