Linear Servo Actuator Control System

Linear Servo Actuator Control System is used to precisely control the linear type servo actuators such as wing flaps, nose wheels and tail flaps in aircraft. The data received from the drive Hall Effect sensor’s position and speed are controlled according to the vector control algorithm and this controller carries out the driving of the motor according to the structure. It can receive commands via the RS-422 communication interface with the flight control computer.

Key Features

  • Nominal Motor Supplies up to 25A
  • 16-32V Supply Voltage Range
  • -40°C to + 55°C Operating Temperature Range
  • Communication protocols RS-422
  • MIL-STD-810G provides high altitude, humidity, acceleration, vibration and shock procedures