• DocumentCode
    2898040
  • Title

    Inertial pseudo star reference unit

  • Author

    Gilmore, J.P. ; Chien, T.T. ; Wingler, R.

  • fYear
    1992
  • fDate
    23-27 Mar 1992
  • Firstpage
    215
  • Abstract
    Summary form only given. The authors present the development of a precision pointing system, the inertial pseudo-star reference unit (IPSRU). The IPSRU implements a collimated light source mounted on an inertially stabilized platform that is configured using a centrally located two-degree-of-freedom (2-DOF) flexure assembly. The platform inertial sensing is achieved through the combined use of a precision, low-noise 2-DOF dry-tuned rotor gyro (DTG) and two angular displacement sensors (ADS). The composite gyro and ADS implementation optimally combines low-frequency gyro measurements with ADS higher frequency sensing to achieve a composite wide band, extremely low noise, and inertial sensing capability. The collimated light beam in effect becomes a jitter-stabilized pseudo-star. In addition, its pointing direction in inertial space can be changed at a precise rate by commands applied via torquing signals to the gyro
  • Keywords
    Bandwidth; Frequency; Jitter; Low-frequency noise; Mirrors; Monitoring; Optical feedback; Optical saturation; Payloads; Telescopes;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Position Location and Navigation Symposium, 1992. Record. 500 Years After Columbus - Navigation Challenges of Tomorrow. IEEE PLANS '92., IEEE
  • Conference_Location
    Monterey, CA
  • Print_ISBN
    0-7803-0468-3
  • Type

    conf

  • DOI
    10.1109/PLANS.1992.185844
  • Filename
    185844