• DocumentCode
    3546906
  • Title

    Simulation analysis of three-phase bridge rectifier circuit of aviation device

  • Author

    Jin Changjiang ; Liu Ling ; Tang Bin ; Kesong, Chen

  • Author_Institution
    Innovation Base of Sch.-Enterprise Cooperation in Aviation Electron. Technol. in Sichuan, Chengdu, China
  • Volume
    2
  • fYear
    2013
  • fDate
    15-17 Nov. 2013
  • Firstpage
    407
  • Lastpage
    409
  • Abstract
    In recent years, with the upgrading of airborne device, most power source circuit of airborne devices use single-phase bridge and three-phase bridge uncontrolled rectifying circuit. Nonlinear characteristics of the rectifier circuit bring serious harmonic interference to the AC power system of the aircraft. This paper simulate and analyses the three-phase bridge circuit of airborne device power source with the help of Matlab, in order to help the governance of the aircraft AC power system harmonic.
  • Keywords
    aircraft power systems; power system harmonics; rectifying circuits; Matlab; airborne device; aircraft AC power system harmonic; aviation device; harmonic interference; nonlinear characteristics; power source circuit; three-phase bridge rectifier circuit; uncontrolled rectifying circuit; Aircraft; Analytical models; Bridge circuits; Integrated circuit modeling; Power harmonic filters; Power supplies; Rectifiers;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Communications, Circuits and Systems (ICCCAS), 2013 International Conference on
  • Conference_Location
    Chengdu
  • Print_ISBN
    978-1-4799-3050-0
  • Type

    conf

  • DOI
    10.1109/ICCCAS.2013.6765368
  • Filename
    6765368