• DocumentCode
    552540
  • Title

    SCKF for MAV attitude estimation

  • Author

    Li, Chao ; Ge, Quan-bo

  • Author_Institution
    Inst. of Inf. & Control, Hangzhou Dianzi Univ., Hangzhou, China
  • Volume
    3
  • fYear
    2011
  • fDate
    10-13 July 2011
  • Firstpage
    1313
  • Lastpage
    1318
  • Abstract
    In this paper, a novel quaternion-based attitude estimation algorithm with the square-root cubature Kalman filter (SCKF) is proposed to improve the attitude estimation performance for micro air vehicle (MAV). The SCKF is a kind of new effective method to solve nonlinear state estimation, it can directly deal with nonlinear systems, and the QR decomposition in SCKF avoids the square-root operation of the covariance matrix, which ensures the continuity of the filtering process. We use quaternion to represent the attitude, treat the strap down attitude as state update, and adopt the bi-vector method to update the measurement vector. Simulation example shows that the proposed algorithm can get better performance on the estimate accuracy and error robustness than that of extended Kalman filter (EKF) and unscented Kalman filter (UKF).
  • Keywords
    Kalman filters; aircraft control; attitude control; covariance matrices; nonlinear systems; stability; state estimation; MAV attitude estimation; QR decomposition; bivector method; covariance matrix; error robustness; filtering process continuity; measurement vector; microair vehicle; nonlinear state estimation; nonlinear system; quaternion-based attitude estimation algorithm; square-root cubature Kalman filter; square-root operation; state update; strap down attitude; Accuracy; Covariance matrix; Equations; Estimation; Kalman filters; Mathematical model; Quaternions; Attitude estimation; MAV; Quaternion; SCKF;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Machine Learning and Cybernetics (ICMLC), 2011 International Conference on
  • Conference_Location
    Guilin
  • ISSN
    2160-133X
  • Print_ISBN
    978-1-4577-0305-8
  • Type

    conf

  • DOI
    10.1109/ICMLC.2011.6016854
  • Filename
    6016854