Flight test of an L 1 adaptive controller on the NASA AirSTAR flight test vehicle

AIAA Guidance, Navigation, and Control Conference

Volumn , Issue , 2010, Pages

  Gregory, Irene M ^a,d   Xargay, Enric ^b,e   Cao, Chengyu ^c,e   Hovakimyan, Naira ^b,e  

^a NASA LANGLEY RESEARCH CENTER   (United States)

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

^c UNIVERSITY OF CONNECTICUT   (United States)

^d Dynamic Systems and Control Branch   (United States)

^e Department of Aerospace Engineering ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ADAPTIVE CONTROL ARCHITECTURE; ADAPTIVE CONTROLLERS; CROSS-COUPLINGS; FLIGHT TEST; FLIGHT-TEST VEHICLES; GENERIC TRANSPORT MODELS; INTEGRAL PART; NASA LANGLEY RESEARCH CENTER;

ADAPTIVE CONTROL SYSTEMS; NASA; TRANSPORT AIRCRAFT;

TESTING;

EID: 84862297063     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2010-8015     Document Type: Conference Paper

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