Adaptive control design methodology for nonlinear-in-control systems in aircraft applications

Journal of Guidance, Control, and Dynamics

Volumn 30, Issue 6, 2007, Pages 1770-1782

  Young, Amanda ^a,c   Cao, Chengyu ^a,c   Patel, Vijay ^a,c   Hovakimyan, Naira ^a,c   Lavretsky, Eugene ^b,d  

^a VIRGINIA POLYTECHNIC INSTITUTE AND STATE UNIVERSITY   (United States)

^b BOEING COMPANY   (United States)

^c Department of Aerospace and Ocean Engineering ^*  (United States)

^d Phantom Works   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ADAPTIVE CONTROL SYSTEMS; COMPUTER SIMULATION; FIGHTER AIRCRAFT; LYAPUNOV FUNCTIONS; NONLINEAR CONTROL SYSTEMS; THEOREM PROVING;

ADAPTIVE LAWS; NONLINEAR-IN-CONTROL UNCERTAIN DYNAMICS; TIKHONOV'S THEOREM;

FLIGHT CONTROL SYSTEMS;

EID: 36849046809     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/1.27969     Document Type: Article

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