• DocumentCode
    2289417
  • Title

    Strategies for fault-tolerant, space-based computing: Lessons learned from the ARGOS testbed

  • Author

    Lovellette, M.N. ; Wood, K.S. ; Wood, D.L. ; Beall, J.H. ; Shirvani, P.P. ; Oh, N. ; McCluskey, E.J.

  • Author_Institution
    Naval Res. Lab., Washington, DC, USA
  • Volume
    5
  • fYear
    2002
  • fDate
    2002
  • Firstpage
    76458
  • Abstract
    The Advanced Space Computing and Autonomy Testbed on the ARGOS satellite provides the first direct, on orbit comparison of a modem radiation hardened 32 bit processor with a similar COTS processor. This investigation was motivated by the need for higher capability computers for space flight use than could be met with available radiation hardened components. The use of COTS devices for space applications has been suggested to accelerate the development cycle and produce cost effective systems. Software-implemented corrections of radiation-induced SEUs (SIHFT) can provide low-cost solutions for enhancing the reliability of these systems. We have flown two 32-bit single board computers (SBCs) onboard the ARGOS spacecraft. One is full COTS, while the other is RAD-hard. The COTS board has an order of magnitude higher computational throughput than the RAD-hard board, offsetting the performance overhead of the SIHFT techniques used on the COTS board while consuming less power.
  • Keywords
    aerospace computing; artificial satellites; circuit reliability; error detection; fault tolerant computing; performance evaluation; radiation hardening (electronics); space vehicle electronics; 32 bit; ARGOS satellite; ARGOS testbed; Advanced Space Computing/Autonomy Testbed; COTS IDT-3081 board; COTS processor; RH-3000 Rad-hard board; SEU susceptibility; fault-tolerant space-based computing; on orbit comparison; radiation hardened processor; radiation-induced SEUs; reliability; single board computers; single event upset susceptibility; software-implemented corrections; space flight; Acceleration; Application software; Costs; Fault tolerance; Modems; Radiation hardening; Satellites; Single event transient; Space vehicles; Testing;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference Proceedings, 2002. IEEE
  • Print_ISBN
    0-7803-7231-X
  • Type

    conf

  • DOI
    10.1109/AERO.2002.1035377
  • Filename
    1035377