• DocumentCode
    296860
  • Title

    System fault protection design for the Cassini spacecraft

  • Author

    Slonski, John P.

  • Author_Institution
    Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
  • Volume
    1
  • fYear
    1996
  • fDate
    3-10 Feb 1996
  • Firstpage
    279
  • Abstract
    Fault protection can include a wide range of topics, ranging from fault prevention to autonomous fault detection and recovery. This paper will address a portion of the autonomous fault detection and recovery implemented on board the Cassini spacecraft. Specifically, the topic is system level fault protection design, as opposed to subsystem fault protection design. The design of system fault protection for the Cassini spacecraft will be described at a high level in order to define the guiding principles of the design. This will include examining driving requirements, high level design trades, and major architectural elements, including practical details of their design. Finally, a detailed design description will be given of two Cassini fault protection responses which are likely to be used on most other spacecraft
  • Keywords
    aerospace computing; aerospace control; command and control systems; protection; reliability; special purpose computers; system recovery; Cassini spacecraft; Saturn system exploration; architectural elements; autonomous fault detection and recovery; command and data subsystem; command loss; concurrent faults; driving requirements; fault recovery responsibility allocation; high level design trades; onboard fault detection; prioritisation; spacecraft safing; system fault protection design; system level design; Aerospace electronics; Fault detection; Instruments; NASA; Plasma waves; Probes; Propulsion; Protection; Radioactive materials; Space vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Applications Conference, 1996. Proceedings., 1996 IEEE
  • Conference_Location
    Aspen, CO
  • Print_ISBN
    0-7803-3196-6
  • Type

    conf

  • DOI
    10.1109/AERO.1996.495890
  • Filename
    495890