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


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    Titel :

    Onboard realtime attitude determination system


    Weitere Titelangaben:

    System zur Echtzeithoehenbestimmung an Bord eines Raumfahrzeuges


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


    Erscheinungsdatum :

    1980


    Format / Umfang :

    1 Seite



    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




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