An extended Kalman filter (EKF) algorithm is implemented on UNIVAC 1100/70. As an example, the longitudinal states, characterizing the short period dynamics of an aircraft are obtained from noisy measured data. This algorithm, with minor modifications and the incorporation of a stiff differential equation solution algorithm, could be implemented for extraction of stability and control derivatives from noisy flight test data.


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    Titel :

    Extended Kalman Filter (EKF) Algorithm


    Beteiligte:
    P. Ramamoorthy (Autor:in)

    Erscheinungsdatum :

    1989


    Format / Umfang :

    13 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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