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System and method to modify an aircraft flight trajectory

專利號(hào)
US10867520B2
公開日期
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.

說明書

According to one implementation, modifying the at least one aspect of the initial trajectory profile includes translating a turn center for a second turn within the initial trajectory profile until an end of a first turn within the initial trajectory profile is coincident with a beginning of the second turn. According to another implementation, modifying the at least one aspect of the initial trajectory profile includes translating a turn center for a second turn within the initial trajectory profile along a path parallel to a line between a first waypoint of the flight plan and a second waypoint of the flight plan. According to another implementation, modifying the at least one aspect of the initial trajectory profile includes translating a turn center for a second turn within the initial trajectory profile along a path parallel to a line outbound from a second waypoint of the flight plan. According to another implementation, modifying the at least one aspect of the initial trajectory profile includes adding a co-tangent straight segment at one or more points tangent to a first turn arc and a second turn arc based on a first waypoint overfly transition intercepting a first waypoint outbound course closer to a second waypoint than to a beginning of a second turn.

According to one implementation, the method 3400 includes determining whether at least three bypass waypoints are included in adjacent legs of the flight plan. The method 3400 may also include in response to a determination that at least three bypass waypoints are included in the adjacent legs, determining whether more than two bypass waypoints of the at least three bypass waypoints are located within a particular turn radius. The method 3400 may also include grouping the more than two bypass waypoints based on a centroid of the more than two bypass waypoints.

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