• DocumentCode
    3160003
  • Title

    The angular position estimation of the moving spacecraft

  • Author

    Ichikawa, Tsutomu

  • Author_Institution
    Japan Aerosp. Exploration Agency (JAXA), Sagamihara
  • fYear
    2008
  • fDate
    20-22 Aug. 2008
  • Firstpage
    2601
  • Lastpage
    2606
  • Abstract
    The problem of estimating the angular position of a spacecraft moving at a constant velocity using two rotating tracking stations is considered. This reports on an initial phase of analytical studies on the optimal attainable estimation performance and associated receiver design. Perametric dependence of the optimum attainable estimation is also studied.
  • Keywords
    aerospace instrumentation; angular measurement; position measurement; space vehicles; angular position estimation; constant velocity; moving spacecraft; rotating tracking station; Additive noise; Additive white noise; Angular velocity; Delay effects; Equations; Performance analysis; Phase estimation; Propagation delay; Satellite ground stations; Space vehicles; Angular position; Estimation; Spacecraft;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    SICE Annual Conference, 2008
  • Conference_Location
    Tokyo
  • Print_ISBN
    978-4-907764-30-2
  • Electronic_ISBN
    978-4-907764-29-6
  • Type

    conf

  • DOI
    10.1109/SICE.2008.4655105
  • Filename
    4655105
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=3160003