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System and method to modify an aircraft flight trajectory

專利號(hào)
US10867520B2
公開(kāi)日期
2020-12-15
申請(qǐng)人
THE BOEING COMPANY(US IL Chicago)
發(fā)明人
Christopher J. Heiberg; Thomas E. Yochum
IPC分類
G08G5/00; B64C13/18; B64C13/16
技術(shù)領(lǐng)域
flight,waypoint,trajectory,profile,turn,aircraft,wpt2,initial,wpt1,waypoints
地域: IL IL Chicago

摘要

A method includes generating a flight plan of an aircraft. The flight plan is based on at least one waypoint and a set of operational rules associated with the aircraft. The method also includes generating an initial trajectory profile based on the at least one waypoint and the set of operational rules. The method further includes identifying an impermissible flight condition associated with the initial trajectory profile. The impermissible flight condition violates at least one operational rule of the set of operational rules. The method further includes generating a modified trajectory profile by modifying at least one aspect of the initial trajectory profile to remove the impermissible flight condition. The modified trajectory profile can be used by a pilot to fly the aircraft, the modified trajectory profile can be used by an autopilot system, or the modified trajectory profile can be displayed.

說(shuō)明書(shū)

According to another implementation of the present disclosure, an aircraft includes a memory storing a set of operational rules associated with the aircraft. The aircraft also includes a flight management system coupled to the memory. The flight management system is configured to generate a flight plan of an aircraft based on at least one waypoint and the set of operational rules. The flight management system is also configured to generate an initial trajectory profile based on the at least one waypoint and the set of operational rules. The flight management system is further configured to identify an impermissible flight condition associated with the initial trajectory profile. The impermissible flight condition violates at least one operational rule of the set of operational rules. The flight management system is also configured to generate a modified trajectory profile by modifying at least one aspect of the initial trajectory profile to remove the impermissible flight condition. The flight management system is also configured to generate data representing the modified trajectory profile in at least one form that accommodates other flight management systems of the aircraft or other pilots to fly the aircraft along the modified trajectory profile.

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