• DocumentCode
    2487672
  • Title

    Safing and fault protection for the MESSENGER mission to Mercury

  • Author

    Moore, Robert C.

  • Author_Institution
    Appl. Phys. Lab., Johns Hopkins Univ., Laurel, MD, USA
  • Volume
    2
  • fYear
    2002
  • fDate
    2002
  • Abstract
    The MErcury Surface, Space ENvironment, GEochemistry, and Ranging (MESSENGER) mission is a NASA Discovery-class, deep-space mission to orbit the planet Mercury. Its purpose is to map the planet surface using various scientific instruments and explore the interior of the planet using measurements from instruments such as a magnetometer and observation of planetary libration. This paper discusses the architecture and implementation of the methods by which faults in the MESSENGER spacecraft are detected and the effects of those faults mitigated. The responsibility of the redundant Fault Protection Processors (FPPs) is to detect faults and take autonomous corrective actions that will keep the spacecraft healthy and safe.
  • Keywords
    Mercury (planet); fault diagnosis; protection; space vehicles; MESSENGER deep-space mission; Mercury; fault detection; fault protection; magnetometer; planetary libration; redundant fault protection processor; safing architecture; scientific instrumentation; Extraterrestrial measurements; Fault detection; Instruments; Mercury (planets); NASA; Planetary orbits; Planets; Protection; Space missions; Space vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Digital Avionics Systems Conference, 2002. Proceedings. The 21st
  • Print_ISBN
    0-7803-7367-7
  • Type

    conf

  • DOI
    10.1109/DASC.2002.1052952
  • Filename
    1052952