An Architecture Modeling and Simulation Methods of Integrated Electromechanical Management System

摘要

Airborne integrated electromechanical management system (IEMS) is a safety critical system, ensuring the aircraft normal flight and the normal operation of each function of the plane. This paper analyses IEMS of the current fighter aircraft, EAP, F-22 and F-35, proposes an architecture modeling and simulation method of IEMS. This method establishes a common model of IEMS, forms modeling and simulation process of IEMS, detailed designs monitoring and redundancy management algorithms based Simulink. Finally, we have applied the methodology on a commercial aircraft and verify the feasibility, accuracy and effectiveness of the modeling method.