• DocumentCode
    2908351
  • Title

    Accelerometer assisted high bandwidth control of tip-tilt mirror for precision pointing stability

  • Author

    Ken, Fujiwara ; Susumu, Yasuda ; Nobutaka, Bando ; Shin-ichiro, Sakai ; Atsuo, Tsuiki ; Yoshito, Niwa ; Yoichi, Hatsutori ; Taihei, Yano ; Yoshiyuki, Yamada

  • fYear
    2011
  • fDate
    5-12 March 2011
  • Firstpage
    1
  • Lastpage
    7
  • Abstract
    Pointing stability that defines acceptable displacement of an observation target on the optical detector during the exposure time in a satellite telescope system largely dominates the quality of the image. This research proposes a new control approach to improve pointing stability using a tip-tilt mirror. While conventional control systems for a tip-tilt mirror use feedback error signals obtained from the optical detector, the signal loses enough bandwidth to compensate for high frequency disturbances when pointing at a dark reference guide star. This paper presents a control system subsidiarily using accelerometers to generate high bandwidth feedforward control references to a tip-tilt mirror by properly identifying transfer function between acceleration and pointing displacement. The numerical simulation and experiments using a disturbance source and a tip-tilt mirror verifies feasibility of this method.
  • Keywords
    accelerometers; astronomical telescopes; feedforward; mirrors; stability; acceleration displacement; accelerometer assisted high bandwidth control; bandwidth feedforward control; feedback error signals; numerical simulation; optical detector; pointing displacement; pointing stability; satellite telescope system; tip-tilt mirror; Accelerometers; Adaptive optics; Feedforward neural networks; Mathematical model; Mirrors; Transfer functions; Vibrations;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2011 IEEE
  • Conference_Location
    Big Sky, MT
  • ISSN
    1095-323X
  • Print_ISBN
    978-1-4244-7350-2
  • Type

    conf

  • DOI
    10.1109/AERO.2011.5747383
  • Filename
    5747383