• DocumentCode
    1795254
  • Title

    The research of satellite attitude determination algorithm based on federal filter

  • Author

    Jing Yang ; Xiaoman Zhang

  • Author_Institution
    Sch. of Autom. Sci. & Electr. Eng., Beihang Univ., Beijing, China
  • fYear
    2014
  • fDate
    8-10 Aug. 2014
  • Firstpage
    2122
  • Lastpage
    2127
  • Abstract
    In order to obtain satellite attitude with better precision and reliability by using a multi-sensor satellite attitude determination system with uncertain model error, federated filter structure is adopted. The subfilter of federated filter is an improved Nonlinear filter, which is suitable for estimation of nonlinear system with uncertain model error by combining the Predictive filter and second-order divided Difference Filter (NPDF). The proposed method estimate model error and system state estimation by fusion multi-sensor information. The simulation results show that the federated filter with feedback, compared with no feedback, obtained better precision that is similar with that of centralized filter. 5 kinds of information-sharing methods are compared, Frobenius norm of estimated error variance matrix algorithm and variance matrix eigenvalue trace algorithm obtained relatively better estimation precision.
  • Keywords
    attitude measurement; eigenvalues and eigenfunctions; nonlinear filters; sensor fusion; space vehicles; state estimation; Frobenius norm; NPDF; difference filter; estimation precision; federal filter; fusion multisensor information; information-sharing methods; multisensor satellite attitude determination system; nonlinear filter; predictive filter; satellite attitude determination algorithm; system state estimation; uncertain model error; variance matrix eigenvalue trace algorithm; Filtering algorithms; Information filters; Mathematical model; Satellites; Sun; Vectors;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Guidance, Navigation and Control Conference (CGNCC), 2014 IEEE Chinese
  • Conference_Location
    Yantai
  • Print_ISBN
    978-1-4799-4700-3
  • Type

    conf

  • DOI
    10.1109/CGNCC.2014.7007503
  • Filename
    7007503