• DocumentCode
    3209033
  • Title

    A high frequency, multi-module, spacecraft boost regulator

  • Author

    Sable, D.M. ; Ridley, R.B.

  • Author_Institution
    Virginia Power Electron. Center, Virginia Polytech. Inst. & State Univ., Blacksburg, VA, USA
  • fYear
    1988
  • fDate
    30 Oct-2 Nov 1988
  • Firstpage
    227
  • Lastpage
    235
  • Abstract
    The design of a high-frequency, multimodule boost regulator suitable for use as a spacecraft battery discharger is presented. A combination of AC inductor current feedback and current-injection (DC switch current feedback) is used for optimum dynamic performance, overload protection, noise immunity, and current sharing of the modules. By suitable design of the second stage output filter, it is shown that the output impedance characteristic possesses a resonant notch instead of a resonant peak and can ensure system stability over a wide range of complex load conditions. Both the overall loop gain and the outer loop gain must be viewed to fully understand all system dynamics
  • Keywords
    controllers; feedback; space vehicle power plants; AC inductor current feedback; DC switch current feedback; HF multimodule spacecraft boost regulator; current sharing; dynamic performance; noise immunity; outer loop gain; output impedance characteristic; overall loop gain; overload protection; spacecraft battery discharger; stability; Batteries; Feedback; Filters; Frequency; Inductors; Protection; Regulators; Resonance; Space vehicles; Switches;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Telecommunications Energy Conference, 1988. INTELEC '88., 10th International
  • Conference_Location
    San Diego, CA
  • Type

    conf

  • DOI
    10.1109/INTLEC.1988.22354
  • Filename
    22354