• DocumentCode
    1769766
  • Title

    Spacecraft health monitoring and management systems

  • Author

    Tipaldi, Massimo ; Bruenjes, Bernhard

  • Author_Institution
    Compagnia Gen. per lo Spazio, Benevento, Italy
  • fYear
    2014
  • fDate
    29-30 May 2014
  • Firstpage
    68
  • Lastpage
    72
  • Abstract
    Spacecraft health monitoring and management systems (also referred to as FDIR (Fault Detection, Isolation and Recovery) systems)) are addressed since the very beginning of any space mission design and play a relevant role in the definition of their reliability, availability and safety objectives. Their primary purposes are the safety of spacecraft/mission life and the improvement of its service availability. In this paper current technical and programmatic FDIR strategies are presented along with their strong connection with the wider concept of on-board autonomy, which is becoming the key-point in the design of new-generation spacecrafts. Recent projects developed at OHB System AG have brought to light some issues in the current FDIR system design approaches. These findings pave the way for innovative solutions, which can support and not rule out conventional industrial practices.
  • Keywords
    aerospace safety; condition monitoring; fault diagnosis; space vehicles; AG; OHB System; fault detection isolation and recovery system; on-board autonomy; programmatic FDIR strategies; space mission design; spacecraft health management system; spacecraft health monitoring system; spacecraft-mission life safety; Hardware; Mathematical model; Monitoring; Redundancy; Satellites; Software; Space vehicles; FDIR; Packet Utilization Standard; Spacecraft Autonomy; Spacecraft Health Monitoring;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Metrology for Aerospace (MetroAeroSpace), 2014 IEEE
  • Conference_Location
    Benevento
  • Type

    conf

  • DOI
    10.1109/MetroAeroSpace.2014.6865896
  • Filename
    6865896