• DocumentCode
    1147891
  • Title

    Auto Reconfiguration of Reaction Wheels in IRS

  • Author

    Goel, P.S. ; Agrawal, V.K. ; Krishnan, A. ; Upadhyaya, J.S.

  • Author_Institution
    Indian Space and Research Organization Satellite Centre Airport Road Bangalore-560 017 India
  • Issue
    1
  • fYear
    1985
  • Firstpage
    160
  • Lastpage
    163
  • Abstract
    The Indian remote sensing satellite (IRS) employs four reaction wheels for attitude control. The fourth, a skew wheel, provides redundancy to the failure of any of the orthogonal wheels. To avoid attitude loss before the redundant skew wheel takes over due to failure of any of the orthogonal wheels, an automatic reconfiguration scheme has been developed and implemented through a microprocessor. The details of reconfiguration logic and the computer simulation results are presented.
  • Keywords
    Computer errors; Computer simulation; Ground support; Microprocessors; Payloads; Redundancy; Remote sensing; Satellite ground stations; Space vehicles; Wheels;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9251
  • Type

    jour

  • DOI
    10.1109/TAES.1985.310550
  • Filename
    4104029