| 摘要 |
An aircraft avionics system (10) for an aircraft, comprising a mission system (2), controlled by an open systems mission computer (OSMC) with a tactical communications system (320) and a tactical navigation system (220); a civil system (1), controlled by a flight management system (FMS) with a civil communications system (310) and a civil navigation system (210), wherein said mission system (2) is logically separated from the civil system (1) through separation of a navigation system (20) of the aircraft into civil navigation system (210) and tactical navigation system (220) and through separation of a communications system (30) of the aircraft (100) into said tactical communications system (320) and said civil communications system (310) and through the independence of the open systems mission computer (OSMC) from the flight management system (FMS), said separation allowing the civil system (1) to operate and be updated independently from the mission system (2). |
