• DocumentCode
    1370987
  • Title

    An extension of the root locus method to obtain closed-loop frequency response of feedback control systems

  • Author

    Jackson, S. Albert

  • Author_Institution
    Cornell University, Ithaca, N. Y.
  • Volume
    73
  • Issue
    4
  • fYear
    1954
  • Firstpage
    176
  • Lastpage
    179
  • Abstract
    THE root locus method for analyzing feedback control systems has become increasingly popular over the last few years. However, the great potentialities of the method have yet to be realized. The method has had the drawback of presenting only the transient response of the system under study. An ideal method of analysis and synthesis would allow the engineer to arrive at both the transient and the steady-state sinusoidal response without any large amount of extra work involved for either. The work would progress in two stages. The first stage would take a relatively short time to complete and would yield approximations to both the closed-loop transient response and the frequency response. At this point, various design features could be compared. The second stage would be an extension of the work done in the first stage ¿ not a more detailed rework of the problem. This second stage of the problem would yield exact and complete transient and sinusoidal solutions.
  • Keywords
    Airplanes; Damping; Engines; Equations; Frequency response; Generators; Transient response;
  • fLanguage
    English
  • Journal_Title
    American Institute of Electrical Engineers, Part II: Applications and Industry, Transactions of the
  • Publisher
    ieee
  • ISSN
    0097-2185
  • Type

    jour

  • DOI
    10.1109/TAI.1954.6371381
  • Filename
    6371381