An actuator includes an inverter, a stator, a movable part, a controller, an injector, a current detector, and an estimator. The inverter is driven by a power generated by the axial force of an engine, etc. The stator includes an armature coil driven by the inverter. The movable part applies a driving force to at least one of a rudder surface of a tailplane of the airplane, etc. The controller controls the inverter in accordance with a signal from a maneuvering system. The injector injects a high-frequency signal into the coil. The current detector detects a coil current. The estimator estimates a position of the movable part.
ACTUATOR FOR AIRPLANE, METHOD OF DRIVING ACTUATOR FOR AIRPLANE, AND ACTUATOR SYSTEM FOR AIRPLANE
15.10.2020
Patent
Elektronische Ressource
Englisch
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