• DocumentCode
    1747159
  • Title

    X2000/IFDP system engineering process for risk management

  • Author

    Hoffman, Tom ; Guiar, Cecilia

  • Author_Institution
    Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
  • Volume
    1
  • fYear
    2001
  • fDate
    2001
  • Abstract
    This paper describes some of the processes employed by the X2000/IFDP system engineering team to manage risk. This paper will describe the difficult system engineering task undertaken by the X2000/IFDP team of trying to develop a technology rich avionics system for a divergent interplanetary mission set. The ability to balance the risks inherent in technology development against the tight requirements of interplanetary missions was the job of the system engineering team. This job posed a unique set of challenges for the team requiring that new processes be developed. Many of the successful processes employed by the X2000/IFDP System Engineering team will be discussed in detail. The bottom line of each of the processes involved early and deep involvement by each of the affected subsystems. This allowed the system design issues to be worked in sufficient detail that the requirements and associated risks could be clearly identified
  • Keywords
    avionics; risk management; space vehicle electronics; systems engineering; X2000/IFDP system engineering process; divergent interplanetary mission set; hardware/software avionics system; risk management; technology development; technology rich avionics system; Aerospace electronics; Engineering management; Hardware; Laboratories; Paper technology; Propulsion; Risk management; Systems engineering and theory; Technology management; Testing;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2001, IEEE Proceedings.
  • Conference_Location
    Big Sky, MT
  • Print_ISBN
    0-7803-6599-2
  • Type

    conf

  • DOI
    10.1109/AERO.2001.931739
  • Filename
    931739