Smart Active Inceptors System definition for Tilt Rotor application

The present activity involves the design, development and validation of smart fly-by-wire active inceptors system for the future generation cockpit of a civil tiltrotor. The design will be focused at exploring and assessing mechanical designs which enhance piloting effectiveness for tilt rotor application, at improving functionalities capitalising on active features, and at optimising weight, dimensions and integration within novel distributed fly-by-wire Flight Control System Please refer to the full topic descriptions document published in this call.