DocumentCode :
3465842
Title :
Application of Direct Power Control in the Charger for Aircraft Battery
Author :
Lv Rui-qiang ; Zhang Ming-lian ; He Zhong-tang ; Zhao Xu-cheng ; Wang Hui
Author_Institution :
Dept. of Aviation Four Stations, Xuzhou Air Force Coll., Xuzhou, China
fYear :
2010
fDate :
7-9 Nov. 2010
Firstpage :
1
Lastpage :
4
Abstract :
PWM rectifier technology is introduced to the main Power Circuit of the charger for aircraft battery to enhance the charging efficiency of aircraft battery and improve its long term reliability and save its life in this paper. A new strategy of DPC Based on the Space Vector Modulation (SVM) is used in PWM rectifier, Meanwhile, a fuzzy PI controller is designed in DC voltage control loop. The simulation results show that unity power factor is achieved and the proposed method has the advantages of low harmonic distortion of current, excellent dynamic-steady state performances, and particularly the designed fuzzy PI controller can restrain the fluctuation of DC voltage, active power and reactive power effectively when charging startup and charging voltage Changing, and also has excellent robustness.
Keywords :
PI control; aircraft; fuzzy control; power system control; voltage control; DC voltage control loop; DC voltage fluctuation; PWM rectifier technology; SVM; aircraft battery charger; direct power control application; fuzzy PI controller; power circuit; space vector modulation; unity power factor; Batteries; Niobium; Power control; Pulse width modulation; Reactive power; Rectifiers; Voltage control;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
E-Product E-Service and E-Entertainment (ICEEE), 2010 International Conference on
Conference_Location :
Henan
Print_ISBN :
978-1-4244-7159-1
Type :
conf
DOI :
10.1109/ICEEE.2010.5660336
Filename :
5660336
Link To Document :
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