• DocumentCode
    1597670
  • Title

    Refined H∞ optimal approach to rotorcraft flight control-a simulation on time responses

  • Author

    Young, Jieh-Shian ; Lin, Chin E.

  • Author_Institution
    Chung San Inst. of Sci. & Technol., Tao-Yuan, Taiwan
  • fYear
    1992
  • Firstpage
    818
  • Abstract
    An approach to refining an H∞-optimal controller for the four-block H∞ control problem is proposed. The H∞ norm of the sublayers can be improved by this approach. A simulation of the rotorcraft flight control on time responses is provided. The simulation results show promising progress both in the frequency domain and in the time domain without inflation of the McMillan degree of the controller
  • Keywords
    aircraft control; control system synthesis; frequency-domain analysis; helicopters; optimal control; time-domain analysis; H∞-optimal controller; McMillan degree; aircraft control; frequency domain; helicopters; rotorcraft flight control; time domain; time responses; Aerospace simulation; Economic indicators; H infinity control; Optimal control; Time factors; Transfer functions; Vents;
  • 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.1992.269742
  • Filename
    269742
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=1597670