A new algorithm is proposed that smoothly integrates non-linear estimation of the attitude quaternion using Davenport s q-method and estimation of non-attitude states through an extended Kalman filter. The new method is compared to a similar existing algorithm showing its similarities and differences. The validity of the proposed approach is confirmed through numerical simulations.


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    Titel :

    Q-Method Extended Kalman Filter


    Beteiligte:
    Zanetti, Renato (Autor:in) / Ainscough, Thomas (Autor:in) / Christian, John (Autor:in) / Spanos, Pol D. (Autor:in)

    Kongress:

    AAS/AIAA Space Flight Mechanics Winter Meeting ; 2013 ; Springfield, VA, United States


    Erscheinungsdatum :

    01.01.2012


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




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