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.
Electromechanical flight control actuator
1976-02-01
Report
No indication
English
Electromechanical flight control actuator
Tema Archive | 1976
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