An electromechanical actuator that will follow a proportional control command with minimum wasted energy is developed. The feasibility of meeting space vehicle actuator requirements using advanced electromechanical concepts is demonstrated. Recommendations for further development are given.


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    Title :

    Electromechanical flight control actuator


    Publication date :

    1976-02-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English







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