Aeroelastic dynamic response and control of an airfoil section with control surface nonlinearities

Journal of Sound and Vibration

Volumn 329, Issue 22, 2010, Pages 4756-4771

  Li, Daochun ^a,b   Guo, Shijun ^a   Xiang, Jinwu ^b  

^a CRANFIELD UNIVERSITY   (United Kingdom)

^b BEIHANG UNIVERSITY   (China)

Author keywords

[No Author keywords available]

Indexed keywords

AEROELASTIC DYNAMIC RESPONSE; AEROELASTIC RESPONSE; AEROELASTIC SYSTEM; AIRFOIL SECTION; CONTROL INPUTS; CONTROL LAWS; CONTROL PERFORMANCE; CUBIC NONLINEARITIES; FLUTTER SPEED; FLUTTER SUPPRESSION; FREEPLAY; HIGH FREQUENCY HF; NON-LINEARITY; NONLINEAR EFFECT; NUMERICAL APPROACHES; PHASE RESPONSE; QUASI-PERIODIC; RUNGE-KUTTA ALGORITHMS; SIMULATION RESULT; STATE-DEPENDENT RICCATI EQUATION; SUBDOMAIN; SUBOPTIMAL CONTROL; SWITCHING POINTS;

ACTUATORS; AIRCRAFT CONTROL; AIRFOILS; CLOSED LOOP SYSTEMS; CONTROL SURFACES; DELAY CONTROL SYSTEMS; DYNAMIC RESPONSE; EQUATIONS OF MOTION; FEEDBACK; FLIGHT CONTROL SYSTEMS; FLOW VELOCITY; FLUTTER (AERODYNAMICS); NONLINEAR OPTICS; RICCATI EQUATIONS; STATE FEEDBACK; TIME DELAY;

CONTROL NONLINEARITIES;

EID: 77955429848     PISSN: 0022460X     EISSN: 10958568     Source Type: Journal    
DOI: 10.1016/j.jsv.2010.06.006     Document Type: Article

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