An integrated inertial stellar attitude sensor for an aerospace vehicle includes a star camera system, a gyroscope system, a controller system for synchronously integrating an output of said star camera system and an output of said gyroscope system into a stream of data, and a flight computer responsive to said stream of data for determining from the star camera system output and the gyroscope system output the attitude of the aerospace vehicle.


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    Titel :

    Integrated Inertial Stellar Attitude Sensor


    Beteiligte:
    T. M. Brady (Autor:in) / A. S. Kourepenis (Autor:in) / W. F. Wyman (Autor:in)

    Erscheinungsdatum :

    2003


    Format / Umfang :

    36 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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