DocumentCode :
231573
Title :
Constant output power control of variable trailing-edge flap wind power system based on feedback linearization
Author :
Zhang Zhen ; Liang Yukun
Author_Institution :
Sch. of Autom. Sci. & Electr. Eng., Beijing Univ. of Aeronaut. & Astronaut., Beijing, China
fYear :
2014
fDate :
28-30 July 2014
Firstpage :
3805
Lastpage :
3810
Abstract :
The variable trailing-edge flap concept is introduced in the blades of the wind power system with trailing-edge flaps. When wind speed exceeds the rated value, the wind turbine could adjust trailing-edge flaps to control rotational speed at the rated value, which realizes the control of constant output power. At first the article presents the nonlinear model of wind turbine system with variable trailing-edge flaps. The nonlinear model of wind power system with trailing-edge flaps is global exactly linearized by differential geometry feedback linearization. In the new linearized model, the feedback controller is designed through pole configuration. The simulation results show that the control strategy is capable of constant output power of wind power system effectively with desirable performances and robustness.
Keywords :
angular velocity control; control system synthesis; differential geometry; feedback; linearisation techniques; power control; power generation control; wind power; wind turbines; constant output power control; differential geometry feedback linearization; feedback controller design; pole configuration; rotational speed control; variable trailing-edge flap wind power system; wind turbine system nonlinear model; Automation; Educational institutions; Electrical engineering; Electronic mail; Wind power generation; Wind turbines; Constant Output Power Control; Feedback Linearization; Variable Trailing-edge Flaps; Wind Power System;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control Conference (CCC), 2014 33rd Chinese
Conference_Location :
Nanjing
Type :
conf
DOI :
10.1109/ChiCC.2014.6895573
Filename :
6895573
Link To Document :
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