Summary form only given substantially as follows: Offers an advanced three axis attitude determination methods by using two-degree-of-freedom star reference sensors. As a result of mathematical analysis, an attitude determination system is presented, which provides onboard realtime attitude information for highly manoeuvrable spacecraft. To solve the problem of Sun/Earth interference, the equations of control for the optical axis of star reference sensors is derived.


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    Titel :

    Three axis attitude determination system by star sensors


    Weitere Titelangaben:

    Drei-Koordinaten-Hoehenbestimmungssystem mit Sternsensoren


    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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