System and method for controlling actuators in an aircraft

An actuator control system in an aircraft, said actuator control system comprising at least a first actuator and a second actuator physically distant from each other, each of the first actuator and the second actuator comprising:

• a movement member,
• at least one measurement sensor for measuring an analogue measurement of at least one physical parameter of the movement member, and
• a computing member internally connected to the movement member and configured to be connected to at least one electronic computer of the aircraft,
• said computing member comprising a function for controlling the movement member, configured to transmit an analogue setpoint to the movement member on a basis of a digital command coming from the electronic computer,
• wherein the measurement sensor of the first actuator is connected externally to the computing member of the second actuator,
• said computing member of the second actuator also comprising a monitoring function for monitoring the movement member of the first actuator, configured to transmit a digital state of the movement member of the first actuator to the electronic computer on a basis of the analogue measurement of the measurement sensor of the first actuator.