• DocumentCode
    2559270
  • Title

    Surge control and test functions for axial flow compressors

  • Author

    Kang, Wei ; Guoxiang Gu ; Sparks, Andy ; Banda, Siva

  • Author_Institution
    Dept. of Math., Naval Postgraduate Sch., Monterey, CA, USA
  • Volume
    6
  • fYear
    1997
  • fDate
    4-6 Jun 1997
  • Firstpage
    3721
  • Abstract
    The focus of this paper is bifurcation control for axial flow engine compressors. The Moore-Greitzer model is adopted for the analysis. We introduce test functions whose zeros are critical to Hopf bifurcation for the closed-loop system where nonlinear feedback control laws are employed. A test function is also developed to determine the stability of the periodic solutions born at Hopf bifurcation. The analysis based on these test functions leads to a new method of feedback design for control of both stationary and Hopf bifurcation in axial flow compressors. Using the techniques proposed, feedback controllers can be designed to meet several bifurcation control requirements, including elimination of the behavior of surge, coupled with rotating stall
  • Keywords
    aerospace engines; aerospace testing; bifurcation; closed loop systems; compressors; nonlinear control systems; stability; state feedback; transient response; Hopf bifurcation; Moore-Greitzer model; aeroengines; axial flow compressors; bifurcation control; closed-loop system; nonlinear control systems; stability; state feedback; surge control; Bifurcation; Compressors; Ducts; Engines; Feedback control; Hysteresis; Stability; State feedback; Surges; System testing;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference, 1997. Proceedings of the 1997
  • Conference_Location
    Albuquerque, NM
  • ISSN
    0743-1619
  • Print_ISBN
    0-7803-3832-4
  • Type

    conf

  • DOI
    10.1109/ACC.1997.609540
  • Filename
    609540