Transient performance of a single-axis rate gyroscope mounted in a spacecraft which is spinning about the spin axis of the gyro is presented. Analytical expressions for various time-domain and frequency-domain specifications as functions of the spin rate of the vehicle are obtained. Numerical results are presented which are useful in selecting the gyro parameters if it is to be used for the measurement of the angular velocity in spinning space vehicles.


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    Title :

    Transient performance of gyro in spinning spacecraft


    Additional title:

    Transientes Verhalten eines Gyroskops in einem rotierenden Raumfahrzeug


    Contributors:
    Singh, S.N. (author) / Iyer, A. (author)

    Published in:

    Publication date :

    1987


    Size :

    5 Seiten, 10 Quellen



    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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