• DocumentCode
    870177
  • Title

    Improved strapdown coning algorithms

  • Author

    Jiang, Yeon Fuh ; Lin, Yu Ping

  • Author_Institution
    Nat. Chiao Tung Univ., Hsinchu, Taiwan
  • Volume
    28
  • Issue
    2
  • fYear
    1992
  • fDate
    4/1/1992 12:00:00 AM
  • Firstpage
    484
  • Lastpage
    490
  • Abstract
    Three improved algorithms for strapdown attitude computation utilizing accumulated gyro increments from the previous and current update are developed and evaluated analytically under classical coning motion. The error criterion of Miller is derived directly from the rotation vector concept. The accuracy of updating rotation vector estimation can be improved at least two orders of magnitude as compared with those of conventional algorithms. The proposed algorithm is equivalent to increasing the number of gyro samples used in the conventional method and it requires less computer loading
  • Keywords
    aerospace computing; computerised navigation; computerised signal processing; error analysis; gyroscopes; inertial navigation; Miller; accumulated gyro increments; coning motion; error criterion; rotation vector; strapdown coning algorithms; Algorithm design and analysis; Artificial intelligence; Attitude control; Computer errors; Control engineering; Differential equations; Error correction; Motion analysis; Quaternions; Vehicles;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9251
  • Type

    jour

  • DOI
    10.1109/7.144574
  • Filename
    144574