PROCESS AND DEVICE FOR THE CONTROL OF THE RUDDER OF AN AIRCRAFT

摘要

The device has at least two servo-systems, each having at least one electric control input. At least one of the servo-systems, called the mixed servo-system, als o has a mechanical control input, and an electric control system for the servo-syste ms is able to occupy a state corresponding to a fault of an engine in which at lea st two of the servo-systems simultaneously operate the rudder and a state correspondin g to an electric fault, in which the mixed servo-system operates the controlled rudder from the mechanical control input.