Aircraft flight and brake control system i.e. stick controller, has sensors generating steering control, from movement of handle, acting on aerodynamic surfaces, and spring associated to brake lever to act on brake system of landing gear

摘要

The system has a mobile handle (2) pivoting around steering axes e.g. pitch and roll axes, using a gimbal joint articulation system. The handle has a brake lever (22) to act on a wheel braking system of a landing gear. Sensors generate a steering control e.g. pitch control, from the movement of the handle, acting on an aerodynamic surface situated at the level of a rear part of an aircraft. The brake lever and a position sensor i.e. rotary potentiometer, are mounted on a base (25) of the handle. An effort simulating device e.g. spring, is associated to the lever for acting on the brake system.