The design techniques presented are applicable to satellite missions where the dominant environmental torques are well understood and lend themselves to accurate analytical modeling. The techniques were applied to the Particles and Fields subsatellites of the Apollo 15 and 16 spacecraft and the flight results show good agreement with the attitude determination estimates obtained.


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    Title :

    Exploiting environmental torques for attitude control and determination of spin stabilized satellites


    Additional title:

    Das Ausnutzen der Umgebungsdrehmomente fuer die Hoehenregelung und Drallbestimmung stabilisierter Satelliten


    Contributors:
    Gluck, R. (author)

    Published in:

    Israel Journal of Technology ; 12 , 3-4 ; 151-159


    Publication date :

    1974


    Size :

    , 12 Quellen


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English






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