The present invention relates to control electronics, preferably for an electromechanical actuator, preferably for use in a primary flight control system of an aircraft, wherein the control electronics can connect or connects an electric motor, preferably of the electromechanical actuator, to an electrical or electronic load and/or wherein the control electronics can deactivate or deactivates a DC/DC converter supplying electrical power to the electric motor, and to an electromechanical actuator and to a method for damping the movement of an electromechanical actuator.
CONTROL ELECTRONICS, ELECTROMECHANICAL ACTUATOR, AIRCRAFT AND METHOD FOR DAMPING THE MOVEMENT OF AN ELECTROMECHANICAL ACTUATOR
2023-10-05
Patent
Electronic Resource
English
European Patent Office | 2023
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