| 摘要 |
PURPOSE: A flight simulation system for an aircraft, a method for separating a malfunctioned sensor thereof, and an altitude flight alarm simulation method for the aircraft can efficiently provide vital flight data on the flight and navigation of an aircraft to a pilot. CONSTITUTION: A flight simulation system for an aircraft comprises a first sensor device(131), a second sensor device(132), a first automatic flight device, a second automatic flight device, first task computer(121), a second task computer(122), a fist simulation part, a second simulation part, an independent gauge, and a selection switch. When one of the first and second sensor devices is normally operated, the other one is operated in a backup mode. The first and second automatic flight devices make an aircraft automatically fly based on signals detected from the first or second sensor device. The first and second task computers control one of the first and second automatic flight devices with the signals detected from the first or second sensor device. The first simulation part simulates information on the first sensor device and the first automatic flight device. The second simulation part simulates information on the second sensor device and a second automatic flight device. The independent gauge displays flight information which is independent to the first and second sensor devices. The selection switch is operated to ignore the signals transmitted from one of the sensor devices exceeding a predetermined threshold valve. |
