High lift system architecture for aircraft

A high lift system architecture for an aircraft, comprising:

• an actuation arrangement configured to move at least one moveable surface of the aircraft between a stowed configuration and a deployed configuration;
• a sensor configured to generate an analog sensed signal representative of a configuration of the moveable surface;
• a flight control computer;
• and
• an actuation control device connected to the actuation arrangement, the sensor, and the flight control computer;
• wherein the actuation control device comprises:
• an acquisition module configured acquire the analog sensed signal from the sensor;
• a processing module configured to process the analog sensed signal and generate an analog controlling signal based on the processed analog sensed signal;
• a conversion module configured to convert the analog sensed signal into a digitalized monitoring signal;
• a control module configured to control the actuation arrangement based on the generated analog controlling signal;
• and,
• a communication module configured to communicate the digitalized monitoring signal to the flight control computer.