• DocumentCode
    1218321
  • Title

    Embedded Model Control: Submicroradian Horizontality of the Nanobalance Thrust-Stand

  • Author

    Canuto, Enrico ; Musso, Fabio ; Ospina, José

  • Author_Institution
    Dipt. di Autom. e Inf., Politec. di Torino, Turin
  • Volume
    55
  • Issue
    9
  • fYear
    2008
  • Firstpage
    3435
  • Lastpage
    3446
  • Abstract
    Pendulum tilt, with respect to local gravity, is affected by the tilt and lateral acceleration of the supporting structure. A differential pendulum, such as the Nanobalance thrust-stand, would be immune only in the ideal case of perfectly balanced pendulums. In the actual case, the equivalent tilt must be zeroed in the measuring bandwidth by an active control system. This paper outlines requirements, technology, modeling, and robust control strategies to ensure instrument horizontality, achieving submicroradian accuracy in a frequency band from 0.1 mHz to 1 Hz. Control strategies, including the coordination of slow and fast motors, have been designed and implemented following the embedded model control methodology. The results of commissioning tests are given and discussed, pointing out the limits of the available technology.
  • Keywords
    aerospace instrumentation; attitude control; control system synthesis; pendulums; robust control; active control system; differential pendulum; embedded model control; lateral acceleration; local gravity; nanobalance thrust-stand; submicroradian accuracy; submicroradian horizontality; Digital control; Not given.; embedded model; horizontality; microradian; thrust-stand;
  • fLanguage
    English
  • Journal_Title
    Industrial Electronics, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0278-0046
  • Type

    jour

  • DOI
    10.1109/TIE.2008.925332
  • Filename
    4519971