• DocumentCode
    490388
  • Title

    A Root-Locus Analysis of Quantitative Feedback Theory

  • Author

    Bossert, David E.

  • Author_Institution
    Capt, Department of Aeronautics, U.S. Air Force Academy, USAFA, CO 80840
  • fYear
    1993
  • fDate
    2-4 June 1993
  • Firstpage
    1698
  • Lastpage
    1702
  • Abstract
    This paper examines the effect of the frequency domain Quantitative Feedback Theory (QFT) technique on the root-locus. Examination of a successful QFT design applied to a business jet provides a case study. Comparison to conventional root-locus design methods helps give understanding of the power of the QFT technique. Also, analyzing the QFT design using the root-locus shows why it is effective, and gives insight into a successful root-locus design.
  • Keywords
    Actuators; Control system synthesis; Damping; Design methodology; Force feedback; Frequency domain analysis; Nonlinear dynamical systems; Robust control; Transfer functions; Uncertainty;
  • 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
    4793167
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=490388