The invention relates to a flight management system of an aircraft. The system comprises a core module used for implementing generic functionalities relative to the flight management of the aircraft, a supplementary module used for implementing supplementary functionalities, and an interface used for message exchange between the core module and the supplementary module. The core module has an interfacing functionality so as to interface with an airborne system of the craft including at least one man-machine interface which is called a universal man-machine interface, and the supplementary module also has an interfacing functionality used for accessing a specific man-machine interface connected to the supplementary module.
Avionics system, particularly flight management system of aircraft
03.06.2015
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |