• DocumentCode
    1597464
  • Title

    Physical lumping methods for developing linear reduced models for high speed propulsion systems

  • Author

    Immel, S.M. ; Hartley, T.T. ; de Abreu Garcia, J.A.

  • Author_Institution
    Dept. of Electr. Eng., Akron Univ., OH, USA
  • fYear
    1992
  • Firstpage
    866
  • Abstract
    A method that allows the development of both high-order large perturbation models and low-order small perturbation models of high-speed propulsion systems is presented. The large perturbation models have a clear nonlinear state space representation as compared with the usual computational fluid dynamics methods. The small perturbation models are easily obtained, given the propulsion system operating point. This modeling approach should be very useful in control system design and essentially parallels that developed by A. Chicatelli and T. T. Hartley (1990)
  • Keywords
    aerospace propulsion; perturbation techniques; state-space methods; NASA Lewis 40-60 inlet; high speed propulsion systems; linear reduced models; nonlinear state space representation; perturbation models; Computational fluid dynamics; Control system synthesis; Difference equations; Digital simulation; Electric shock; Partial differential equations; Physics; Propulsion; Reduced order systems; State-space methods;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Applications, 1992., First IEEE Conference on
  • Conference_Location
    Dayton, OH
  • Print_ISBN
    0-7803-0047-5
  • Type

    conf

  • DOI
    10.1109/CCA.1992.269734
  • Filename
    269734