• DocumentCode
    3102782
  • Title

    Control of a Matrix Converter-based AC Power Supply for Aircrafts under Unbalanced Conditions

  • Author

    Arévalo, Saúl López ; Zanchetta, Pericle ; Wheeler, Patrick W.

  • Author_Institution
    Univ. of Nottingham, Nottingham
  • fYear
    2007
  • fDate
    5-8 Nov. 2007
  • Firstpage
    1823
  • Lastpage
    1828
  • Abstract
    This paper deals with the design, control and implementation of a 10 kVA three-phase ground power supply unit (GPU) for aircraft servicing. Instead of a classical back to back converter configuration, a 3-phase to 3-phase direct AC-AC (matrix) converter has been used as the power conditioning core of the power supply, working in conjunction with input and output LC filters. An optimized control system in the ABC frame employing a repetitive controller has been successfully implemented taking into account both the transient and steady state performance targets together with the system effectiveness under extreme unbalanced conditions. Extensive simulations prove the efficiency of the designed system in meeting the international standards requirements.
  • Keywords
    AC-AC power convertors; aircraft control; aircraft power systems; matrix convertors; optimal control; predictive control; AC power supply; aircraft servicing; direct AC-AC converter; matrix converter; optimized control system; output LC filters; repetitive controller; three-phase ground power supply unit; Aerospace control; Aerospace electronics; Aircraft propulsion; Bandwidth; Control systems; Matrix converters; Military aircraft; Power supplies; Switching frequency; Voltage control;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Industrial Electronics Society, 2007. IECON 2007. 33rd Annual Conference of the IEEE
  • Conference_Location
    Taipei
  • ISSN
    1553-572X
  • Print_ISBN
    1-4244-0783-4
  • Type

    conf

  • DOI
    10.1109/IECON.2007.4460406
  • Filename
    4460406