• DocumentCode
    1384373
  • Title

    Admittance space stability analysis of power electronic systems

  • Author

    Sudhoff, S.D. ; Glover, S.F. ; Lamm, P.T. ; Schmucker, D.H. ; Delisle, D.E.

  • Author_Institution
    Sch. of Electr. & Comput. Eng., Purdue Univ., West Lafayette, IN, USA
  • Volume
    36
  • Issue
    3
  • fYear
    2000
  • fDate
    7/1/2000 12:00:00 AM
  • Firstpage
    965
  • Lastpage
    973
  • Abstract
    Power electronics based power distribution systems (PEDSs) are becoming increasingly common, particularly in marine and aerospace applications. Stability analysis of this class of systems is crucial due to the potential for negative impedance instability. Existing techniques of stability analysis introduce artificial conservativeness, are sensitive to component grouping, and at the same time do not explicitly address uncertainties and variations in operating point. A new stability criterion, which reduces artificial conservativeness and is also insensitive to component grouping is described. In addition, a means of readily establishing design specifications from an arbitrary stability criterion which specifically includes a provision to incorporate uncertainty, parameter variation, and nonlinearities is set forth. The method is presented in the context of a hardware test system and is experimentally validated.
  • Keywords
    Nyquist stability; electric admittance; electric impedance; nonlinear systems; power distribution; power electronics; Kalman filter; accuracy; admittance space stability analysis; aerospace applications; aircraft body axes; aircraft position; analytic boresighting; analytic calibration; continuous in-flight calibration; design specifications; ground based techniqu; line-of-sight pointing mechanization; line-of-sight sensors; marine applications; negative impedance instability; night test; pointing accuracy; power distribution; residual errors; sensor gimbals; shipboard INS/GPS navigator; stability criterion; surveyed ground targe; target location; Admittance; Aerospace electronics; Hardware; Impedance; Power distribution; Power electronics; Stability analysis; Stability criteria; System testing; Uncertainty;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9251
  • Type

    jour

  • DOI
    10.1109/7.869516
  • Filename
    869516