• DocumentCode
    3598551
  • Title

    Using model-based reasoning for autonomous instrument operation

  • Author

    Johnson, Michael A. ; Rile, M.L. ; Truszkowski, Walt

  • Author_Institution
    NASA Goddard Space Flight Center, Greenbelt, MD, USA
  • Volume
    5
  • fYear
    2001
  • fDate
    6/23/1905 12:00:00 AM
  • Firstpage
    2411
  • Abstract
    Model-based reasoning has been applied as an autonomous control strategy on the Low Energy Neutral Atom (LENA) instrument currently flying onboard the Imager for Magnetosphere-to-Aurora Global Exploration (IMAFE) spacecraft. Explicit models of instrument subsystem responses have been constructed and are used to dynamically adapt the instrument to the spacecraft´s environment. These functions are cast as part of a virtual Principal Investigator (VPI) that autonomously monitors and controls the instrument. In the VPI´s current implementation, LENA´s command uplink volume has been decreased significantly from its previous volume; typically, no uplinks are required for operations. This work demonstrates that a model-based approach can be used to enhance science instrument effectiveness. The components of LENA are common in space science instrumentation, and lessons learned by modeling this system may be applied to other instruments. Future work involves the extension of these methods to cover more aspects of LENA operation and the generalization to other space science instrumentation
  • Keywords
    aerospace control; aerospace expert systems; aerospace instrumentation; model-based reasoning; LENA; Low Energy Neutral Atom instrument; Magnetosphere-to-Aurora Global Exploration spacecraft; Virtual Principal Investigator; autonomous instrument operation; model-based reasoning; multiprobe missions; space science instrumentation; Bandwidth; Inference mechanisms; Instruments; Magnetic sensors; Magnetic separation; Magnetosphere; Probes; Space technology; Space vehicles; Sun;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2001, IEEE Proceedings.
  • Print_ISBN
    0-7803-6599-2
  • Type

    conf

  • DOI
    10.1109/AERO.2001.931200
  • Filename
    931200