• DocumentCode
    490268
  • Title

    H∞ control of gasturbine engines for helicopters

  • Author

    Watanabe, Ryo ; Kurosaki, Masahiro ; Kusakawa, Takeshi ; Uchida, Kenko ; Fujita, Masayuki

  • Author_Institution
    Control Systems Engineering Department, Aero-Engine and Space, Operations, Ishikawajima-Harima Heavy Industries Co., Ltd., 229 Tonogaya, Misuho-Machi, Nishitamagun, Tokyo 190-12, Japan
  • fYear
    1993
  • fDate
    2-4 June 1993
  • Firstpage
    1123
  • Lastpage
    1127
  • Abstract
    Engines tests were conducted in order to demonstrate effectiveness and practicability of H∞ control theory to helicopter engines. An engine control algorithm is designed by H∞ control theory, which meets robust stability requirements and nominal performance requirements described in frequency domain. Simulation ad engine test results show that H∞ controllers with feedforward element have better control performance than PI controller with feedforward element, especially, less power turbine speed overshoots are observed in rapid torque decreasing tests.
  • Keywords
    Control systems; Control theory; Engines; Helicopters; Noise measurement; Shafts; Space technology; Testing; Torque control; Turbines;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference, 1993
  • Conference_Location
    San Francisco, CA, USA
  • Print_ISBN
    0-7803-0860-3
  • Type

    conf

  • Filename
    4793041
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=490268