• DocumentCode
    1370023
  • Title

    Sinusoidal analysis of feedback-control systems containing nonlinear elements

  • Author

    Johnson, E. Calvin

  • Author_Institution
    Bendix Aviation Corporation, Detroit, Mich.
  • Volume
    71
  • Issue
    3
  • fYear
    1952
  • fDate
    7/1/1952 12:00:00 AM
  • Firstpage
    169
  • Lastpage
    181
  • Abstract
    TECHNIQUES commonly used at the present time in the analysis and synthesis of feedback-control systems are largely those of constant-linear system theory. In the usual form, these methods stem from a system characterization in terms of ordinary linear differential equations having real constant coefficients. Fortunately, for many purposes this characterization is satisfactory, and in these cases the properties and behavior of the systems can be studied analytically by application of the large body of available linear theory. Frequently, however, practical control systems contain elements, either unavoidably or by design, which are not linear in the engineering sense of being describable by linear differential equations with constant coefficients.
  • Keywords
    Aircraft; Circuit faults; Equations; Nonlinear systems; Oscillators; Steady-state; Transfer functions;
  • 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.1952.6371220
  • Filename
    6371220