Electric motor for driving inertial measurement device of aircraft e.g. helicopter, has rotor constituting rotating support on which inertial measurement device and part of electronic processing unit are fixed

摘要

The electric motor (1) has an electronic control unit for controlling rotation speed of a rotor (4), and a rotating support integrated with an inertial measurement device. The rotor is provided with permanent magnets, and constitutes the rotating support on which the inertial measurement device and a part of an electronic processing unit are fixed. An inductive unit electrically supplies the inertial measurement device, and transfer measurements to a fixed electronic unit by the inertial measurement device. Independent claims are also included for the following: (1) an inertial measurement unit (2) a power station comprising an attitude, heading and reference system (3) a method for controlling and adjusting inertial rotation speed of an electric motor.