• DocumentCode
    1501995
  • Title

    Attitude control — I

  • Author

    Farrior, J. S.

  • Author_Institution
    U.S. Army Ballistic Missile Agency, Huntsville, Ala.
  • Volume
    77
  • Issue
    12
  • fYear
    1958
  • Firstpage
    1084
  • Lastpage
    1086
  • Abstract
    THE PROBLEM of attitude control exists to a certain extent with all kinds of vehicles, missiles, and projectiles. Attitude control is necessary or desirable for at least the following reasons: 1. To provide mental and physical comfort for passengers. 2. To provide proper environment and positioning to allow instrumentation to function. 3. To provide proper alignment for lift surfaces and thrust vectors.
  • Keywords
    Aerospace electronics; Attitude control; Satellites; Space vehicles; Telescopes; Wheels;
  • fLanguage
    English
  • Journal_Title
    Electrical Engineering
  • Publisher
    ieee
  • ISSN
    0095-9197
  • Type

    jour

  • DOI
    10.1109/EE.1958.6445495
  • Filename
    6445495
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=1501995