Adaptive synthetic jet actuator compensation for a nonlinear aircraft model at low angles of attack

IEEE Transactions on Control Systems Technology

Volumn 16, Issue 5, 2008, Pages 983-995

  Deb, Dipankar ^a   Tao, Gang ^b   Burkholder, Jason O ^c   Smith, Douglas R ^d  

^a Sensitron Semiconductor   (United States)

^b UNIVERSITY OF VIRGINIA   (United States)

^c Barron Associates Inc   (United States)

^d UNIVERSITY OF WYOMING   (United States)

Author keywords

Actuator nonlinearity; Adaptive inverse; Nonlinear aircraft dynamics; Parameter projection; Stability and tracking; Synthetic jet actuators

Indexed keywords

AIRCRAFT; AIRCRAFT MODELS; ANGLE OF ATTACK; FEEDBACK; GAS DYNAMICS; JETS; LEARNING SYSTEMS; STATE FEEDBACK; TECHNOLOGY; WINGS;

ACTUATOR ARRAYS; ACTUATOR NONLINEARITY; ADAPTIVE COMPENSATION; ADAPTIVE INVERSE; ADAPTIVE LAWS; AERODYNAMIC PERFORMANCE; ANGLES OF ATTACK; CLOSED-LOOP STABILITY; CONTROL SURFACES; EXPERIMENTAL DATA; INTERMEDIATE STATES; NEW TECHNOLOGIES; NON-LINEARITIES; NONLINEAR AIRCRAFT DYNAMICS; NONLINEAR AIRCRAFT MODEL; NONLINEAR STATE FEEDBACK CONTROL; PARAMETER PROJECTION; PARAMETERIZED MODELING; STABILITY AND TRACKING; SYNTHETIC JET ACTUATOR; SYNTHETIC JET ACTUATORS; TAILLESS AIRCRAFT;

ACTUATORS;

EID: 49249133457     PISSN: 10636536     EISSN: None     Source Type: Journal    
DOI: 10.1109/TCST.2007.912124     Document Type: Article

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