• DocumentCode
    1149763
  • Title

    Implementation of CDFM Generator Control

  • Author

    Ortmeyer, Thomas H. ; Weimer, Joseph A.

  • Author_Institution
    Clarkson University
  • Issue
    4
  • fYear
    1986
  • fDate
    7/1/1986 12:00:00 AM
  • Firstpage
    349
  • Lastpage
    355
  • Abstract
    The control of a cascaded doubly fed machine (CDFM) to be used for aircraft power generation is investigated. The controller employs a resistance simulator in the generator exciter to provide machine damping. Excitation is provided by a six step inverter fed from a controlled rectifier. Delays due to the dc link time constant cause the resistance simulation to be nonideal. An investigation into the ability of resistance simulation to provide damping under these conditions is described. The study includes linearized analysis, simulation, and laboratory tests. Good correlation between these methods was obtained throughout the study. Three control strategies for providing machine damping were investigated, and it is concluded that resistance simulation can be used to provide machine damping under these conditions.
  • Keywords
    Aerospace control; Aircraft; Analytical models; Damping; Delay effects; Inverters; Laboratories; Power generation; Rectifiers; Testing;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9251
  • Type

    jour

  • DOI
    10.1109/TAES.1986.310770
  • Filename
    4104224