• DocumentCode
    381361
  • Title

    Virtual Engineering and Science Team - Reusable autonomy for spacecraft subsystems

  • Author

    Bailin, Sidney C. ; Johnson, Michael A. ; Truszkowski, Walt ; Rilee, Michael L. ; Thompson, Bryan

  • Author_Institution
    Knowledge Evolution Inc., Washington, DC, USA
  • Volume
    5
  • fYear
    2002
  • fDate
    2002
  • Firstpage
    251044
  • Abstract
    Addresses the design, development and evaluation of the Virtual Engineering and Science Team (VEST) tool. VEST supports the efficient and cost-effective realization of on-board subsystem/instrument autonomy and contributes directly to the realization of an intelligent autonomous spacecraft. VEST supports the evolution of a subsystem/instrument model which explicitly represents correct vs. anomalous behavior. From that model, it automatically generates the code needed to support the autonomous operation of what was modeled. VEST facilitates the integration of the efforts of engineers, scientists and software technologists. This integration of efforts will be a significant advance over current development processes. The model, developed through the use of VEST, will be the basis for the physical construction of the subsystem/instrument and the generated code will support its autonomous operation once in space. The close coupling between the model and the code, in the same tool environment, will help ensure the correct and reliable operational control of the subsystem/instrument.
  • Keywords
    aerospace instrumentation; intelligent structures; space vehicles; VEST; Virtual Engineering and Science Team; intelligent autonomous spacecraft; on-board subsystem/instrument autonomy; operational control; physical construction; reusable autonomy; spacecraft subsystems; tool environment; Aerospace engineering; Design engineering; Health and safety; Instruments; Knowledge engineering; Logic; Modems; Space technology; Space vehicles; Voltage;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference Proceedings, 2002. IEEE
  • Print_ISBN
    0-7803-7231-X
  • Type

    conf

  • DOI
    10.1109/AERO.2002.1035440
  • Filename
    1035440