A three-axis attitude reconstitution scheme for spin stabilized sounding rockets is presented, using star transit pulse intormation from a single slit all solid state star sensor. The method, based on Kalman filtering and smoothing, gives accuracies in the arcminute range and has been successfully tested on four different missions in the Swedish sounding rocket program.


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    Titel :

    High-Accuracy Sounding Rocket Attitude Estimation Using Star Sensor Data


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    01.11.1978


    Format / Umfang :

    1855004 byte




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch






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