Conception d’une architecture robuste pour l’acquisition de grandeurs physiques dans un système aéronautique critique : application à la mesure de température, pression, couple, et vitesse d’une turbomachine

摘要

The acquisition of physical parameters as such as temperature, pressure, torque, and speed are necessary to flight critical systems in order to reach and ensure safety and availability required. Consequently, it requires implementing high technologies and techniques which are able to work in rugged environments.The aim of our work is to design a new architecture for sensor acquisition systems in order to be integrated onto a flight critical system. The goal of the architecture is to ensure data integrity, system's availability and safety relative to airborne critical systems. The solution adds the fault tolerance ability to the signal conditioning. Consequently, we implement additional functionalities, as such as mathematical model of the signal conditioning, in order to make the acquisition system more intelligent.Our research work is partially based on technical specifications from SYRENA project, which is a typical example of flight critical systems, which is the main thematic of our purpose.