Summary form only given, as follows. Offers an automatic attitude estimation technique for highly manoeuvrable spacecraft. The atitude determination system in composed of an inertial reference unit (IRU), two-degree-of-freedom star reference sensors, and onboard computer. As a result of the study, suitable algorithms for automatic attitude estimation have been developed. The attitude estimation algorithms are based upon Kalman filter combining measurement data from a set of star reference sensors to compensate the drift error of attitude reference frame.


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    Titel :

    Onboard attitude determination system using filter for drift compensation


    Weitere Titelangaben:

    Bordsystem zur Lagebestimmung unter Verwendung eines Filters fuer die Driftkompensation


    Beteiligte:
    Izumida, K. (Autor:in) / Abe, K. (Autor:in) / Takeda, H. (Autor:in)


    Erscheinungsdatum :

    1981


    Format / Umfang :

    1 Seite


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




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