• DocumentCode
    1501999
  • Title

    Attitude control — II

  • Author

    Roberson, R. E.

  • Author_Institution
    Autonetics Division, North American Aviation, Inc., Downey, Calif.
  • Volume
    77
  • Issue
    12
  • fYear
    1958
  • Firstpage
    1086
  • Lastpage
    1088
  • Abstract
    CONTROLLING THE ATTITUDE of a satellite vehicle should be a simple job. The body behaves as if it were suspended on a frictionless pivot. Control torques can be small. There usually is no need for extreme precision in measurement. And adequate response times are ridiculously low by conventional servo standards.
  • Keywords
    Attitude control; Control systems; Equations; Flywheels; Satellites; Torque; Vehicles;
  • fLanguage
    English
  • Journal_Title
    Electrical Engineering
  • Publisher
    ieee
  • ISSN
    0095-9197
  • Type

    jour

  • DOI
    10.1109/EE.1958.6445496
  • Filename
    6445496
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=1501999