• DocumentCode
    858509
  • Title

    Fundamental theory of automatic linear feedback control systems

  • Author

    Horowitz, Isaac M.

  • Author_Institution
    Hughes Aircraft Company, Culver City, CA, USA
  • Volume
    4
  • Issue
    3
  • fYear
    1959
  • fDate
    12/1/1959 12:00:00 AM
  • Firstpage
    5
  • Lastpage
    19
  • Abstract
    The reasons for using feedback are reviewed. The beneficial aspects of feedback are quantitatively expressed in sensitivity functions and noise transmission functions. The physical constraints on the controlled process (or plant) determine the maximum number of independent functions realizable. Any configuration with the same number of degrees of freedom may be used. With this approach the study of conditional feedback, model feedback, combined positive and negative feedback, etc. is of secondary interest. The benefits of feedback are paid for in gain-bandwidth of active elements over and above what is needed to physically do the job. The minimum price that must be paid is independent of configuration. The system with two degrees of freedom is studied in detail. Two methods are presented for the precise design of a system that will be as insensitive as may be desired to large parameter variations. One method uses root-locus techniques and is suitable for systems with a small number of dominant poles and zeros. The second method is based on frequency response and can be used for systems of any complexity. Numerical examples are given.
  • Keywords
    Aerospace control; Aircraft; Automatic control; Control system synthesis; Control systems; Costs; Feedback control; Laboratories; Linear feedback control systems; Negative feedback;
  • fLanguage
    English
  • Journal_Title
    Automatic Control, IRE Transactions on
  • Publisher
    ieee
  • ISSN
    0096-199X
  • Type

    jour

  • DOI
    10.1109/TAC.1959.1104893
  • Filename
    1104893