Automatic closed loop and pilot operated twin-gyro systems are discussed as attitude stabilizers for large space vehicles


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    Title :

    RESULTS OF STUDIES ON A TWIN-GYRO ATTITUDE CONTROL SYSTEM FOR SPACE VEHICLES


    Contributors:

    Publication date :

    1963-08-14


    Type of media :

    Preprint


    Type of material :

    No indication


    Language :

    English




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