BACK-UP THRUST REVERSER ACTUATION SYSTEM CONTROL

A system architecture for a backup thrust reverser actuation system control is provided. The system architecture includes an AC power supply (101, 201) of an aircraft, a power supply (102, 202) and a motor control (103, 203) adapted to control an electric motor (M) of a thrust reverser actuation system. The system architecture further includes a backup power supply (105, 212) adapted to provide power to the electric motor in the event that the power supply fails