• DocumentCode
    783141
  • Title

    Estimation of Rodrigues parameters from vector observations

  • Author

    Idan, M.

  • Author_Institution
    Fac. of Aerosp. Eng., Israel Inst. of Technol., Haifa, Israel
  • Volume
    32
  • Issue
    2
  • fYear
    1996
  • fDate
    4/1/1996 12:00:00 AM
  • Firstpage
    578
  • Lastpage
    586
  • Abstract
    A recursive minimum variance algorithm for attitude determination is presented. The attitude is expressed by the Rodrigues vector, where only three parameters are needed to describe orientation. The advantage of using the Rodrigues parameters is computational. Attitude calculations involve only relatively simple algebraic expressions, which is advantageous especially in real-time applications. The efficiency of the derived algorithm is demonstrated using Monte-Carlo computer simulation results and in an initial alignment aerospace application.
  • Keywords
    Monte Carlo methods; attitude control; recursive estimation; vectors; Monte-Carlo computer simulation; Rodrigues parameters; algebraic expressions; alignment aerospace application; attitude determination; orientation; recursive minimum variance algorithm; vector observations; Aerodynamics; Aerospace control; Aerospace engineering; Aircraft; Application software; Equations; Missiles; Parameter estimation; Position measurement; Quaternions; Recursive estimation;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9251
  • Type

    jour

  • DOI
    10.1109/7.489502
  • Filename
    489502