DocumentCode :
184187
Title :
Controller design for blade load reduction using synthetic jets
Author :
Soltani, Mahdi ; Mirzaei, Mohammad
Author_Institution :
Dept. of Energy Technol., Aalborg Univ., Esbjerg, Denmark
fYear :
2014
fDate :
4-6 June 2014
Firstpage :
4440
Lastpage :
4445
Abstract :
As the size of modern wind turbines increase, the blades become longer and more flexible. Consequently, fatigue loads due to the structural vibration become more important and turn to be a constraint on enlarging the size of the new turbines. Thus, it becomes more necessary to use nontraditional actuators to damp structural vibration. This paper, presents the design of a control system that acts on blade synthetic jets to reduce and damp the vibration of the desired blade modes. The design of model-based estimators is addressed. These estimators use the measurements of several accelerometers and strain gauges along the blade and the tower to estimate the contribution of each blade modal state to the vibration of the tower and the blades. The synthetic jet actuators are then controlled, such that the desired vibration modes are damped effectively. Designed estimator and controller are implemented on a FEM-based wind turbine simulation code. The results show significant damping of blade vibration.
Keywords :
accelerometers; actuators; blades; finite element analysis; jets; strain gauges; wind turbines; FEM; accelerometers; blade load reduction; blade modal state; blade modes; controller design; damping; fatigue loads; model-based estimators; nontraditional actuators; strain gauges; structural vibration; synthetic jet actuators; tower; wind turbine simulation code; wind turbines; Accelerometers; Blades; Force; Poles and towers; Strain; Vibrations; Wind turbines; Control applications; Flexible structures; Power systems;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference (ACC), 2014
Conference_Location :
Portland, OR
ISSN :
0743-1619
Print_ISBN :
978-1-4799-3272-6
Type :
conf
DOI :
10.1109/ACC.2014.6858978
Filename :
6858978
Link To Document :
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