• DocumentCode
    3494175
  • Title

    A model-based thruster leakage monitor for the Cassini spacecraft

  • Author

    Lee, Allan Y. ; Brown, M. Jay

  • Author_Institution
    Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
  • Volume
    2
  • fYear
    1998
  • fDate
    21-26 Jun 1998
  • Firstpage
    902
  • Abstract
    The Cassini spacecraft uses thrusters to maintain three-axis attitude control and to perform many other functions. If one of the thrusters leaks, the opposing thrusters will be fired excessively to maintain the commanded attitude. Obviously, the draining of hydrazine and the excessive firings of thrusters must be stopped quickly. A set of three model-based leakage detection monitors has been designed and implemented in the flight software to protect Cassini against the occurrence of this unlikely event. Test results indicate that this design can detect thruster leakage quickly and robustly. Once the leak is detected, the on-board fault protection logic will activate remedial actions which include the swapping of thruster branches
  • Keywords
    aerospace propulsion; attitude control; computerised monitoring; fault diagnosis; space vehicles; Cassini spacecraft; fault protection; flight software; model-based leakage detection; monitoring; three-axis attitude control; thrusters; Event detection; Fault detection; Leak detection; Logic; Monitoring; Propellants; Protection; Robustness; Space vehicles; Testing;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    American Control Conference, 1998. Proceedings of the 1998
  • Conference_Location
    Philadelphia, PA
  • ISSN
    0743-1619
  • Print_ISBN
    0-7803-4530-4
  • Type

    conf

  • DOI
    10.1109/ACC.1998.703537
  • Filename
    703537