• 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