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Journal Articles
Aircraft Engineering and Aerospace Technology: An International Journal (2019) 91 (8): 1122–1132.
Published: 28 May 2019
... electromechanical actuator proposed for the launch vehicle application has a unique configuration which does not require a complex fault detection isolation and reconfiguration logic in the controller. This enhances the system reliability and allows a simplex controller having a lower cost. Bearing Ball screw...

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