pThe actuator (10) has an electric motor (13) whose stator comprises an exciter member (17) provided with exciters (17a, 17b), where each exciter drives the movement of a rotor (13b) relative to the stator when the exciter is electrically powered. An inductive type angular position sensor has a transmitter member (20) with transmitters (20a, 20b) that cause transmission of signals (S1, S2) representing a rotor position by receivers (21a, 21b) when the transmitters are electrically powered, respectively. The transmitters and the exciters are electrically powered independently from each other. Independent claims are also included for the following: (1) a brake for an aircraft (2) a braking device for an aircraft, comprising a brake./p[EP2475077A1]
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