• DocumentCode
    1176693
  • Title

    Space Control System Utilizing Digital Logic Techniques for Optimum Response

  • Author

    Bailey, Ray W.

  • Author_Institution
    North American Aviation, Inc. Columbus, Ohio
  • Issue
    4
  • fYear
    1966
  • fDate
    7/1/1966 12:00:00 AM
  • Firstpage
    638
  • Lastpage
    647
  • Abstract
    The objective of this paper is to discuss a new space control system utilizing ??SUBORDINATE OR?? logic blocks. This technique retains the highly efficient stabilization characteristics of the ??TRIGGER LOGIC?? system and adds the capability of optimum response to maneuver commands. Modification and incorporation of the command signal into the control logic is shown so that optimum response results. Optimum herein means getting into the new commanded limit cycle box in minimum time with the least fuel possible expended. The use of elementary digital logic blocks is emphasized for designing a simple nonlinear control system. Such usage precludes the problem of summing small and large analog signals, and also provides more flexibility in control logic design.
  • Keywords
    Communication system control; Control systems; Digital control; Displacement control; Fuels; Limit-cycles; Logic circuits; Logic design; Space missions; Space vehicles;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9251
  • Type

    jour

  • DOI
    10.1109/TAES.1966.4501896
  • Filename
    4501896