NASA NTRS · 19760015172
Electromechanical flight control actuator
Abstract
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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1976-02-01. Electromechanical flight control actuator. https://ntrs.nasa.gov/citations/19760015172
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