A new attitude control actuator, the vibrating mass gyroscope is considered. The actuator transforms the vibratory motion of a single gimbal gyroscope to a positive or negative, fluctuating control torque. The equations of motion for such an actuator are presented. The feasibility of construction of such an actuator is investigated. Possible means of realizing the vibratory motion is proposed.


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    Title :

    Vibrationally excited satellite attitude actuator: A feasibility study


    Contributors:


    Publication date :

    2015-06-01


    Size :

    1148188 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English







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