Distributed and Reconfigurable Architecture for Flight Control System
New airplanes must meet rigorous requirements of aviation safety, operational reliability, high performance and energy efficiency at a low cost. To meet this challenge, we should optimize current system and take advantage of available technology for the next decade. This work is aiming at proposing some evolutions for Flight Control System (FCS) and to build alternative FCS low-cost and safe architectures for the next decade with less hardware and software resources.