Design of Four Node Redundancy for Aircraft Electromechanical Management System
Electromechanical management system is an important component of aircraft,supporting the safe and stable flight of aircraft.Aiming at the high-performance and stable architecture requirements of electromechani-cal management system,this paper proposes a four-node redundancy design.Adopting a distributed fault-tolerant architecture and relying on high-speed bus communication technology,it achieves cross interconnection and infor-mation sharing between different nodes,thereby making targeted redundancy decisions,avoiding failure risks to a certain extent,and ensuring the induction and braking of airborne electromechanical equipment.
NETL
NSTL
万方数据
维普
