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System and method to modify an aircraft flight trajectory

專利號
US10867520B2
公開日期
2020-12-15
申請人
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

Referring to FIG. 17, a diagram of a process 1700 for adjusting a trajectory profile is shown. The process 1700 can be performed by flight management system 202 of FIG. 2. The process 1700 illustrates an example of modifying at least one aspect (e.g., the second segment 262) of the initial trajectory profile 232 by inserting a straight segment between a first turn included in the second segment 262 of the initial trajectory profile 232 and a second turn included in the second segment 262 of the initial trajectory profile. According to the process 1700, the straight segment may be rotated.

For example, after an impermissible flight condition is detected, the flight management system 202 applies one or more correction algorithms to create a smooth and continuous trajectory profile (e.g., the modified trajectory profile 242) for the aircraft 100 based on the flight conditions 250. For the scenario where the S-turn produces a “bi-quad” impermissible flight condition, the flight management system 202 can select an algorithm described with respect to FIG. 17 using a rule-based decision.

According to the process 1700, turn centers are translated and then moved apart. For example, the first turn center (TC1) is moved along a line parallel to its inbound course and the second turn center (TC2) is moved along a line parallel to its outbound course until a straight segment tangent to the two turn arcs reaches a fixed distance. The fixed distance can be set to accomplish a maneuver goal such as being sufficient to achieve a particular roll-anticipation-distance for a particular turn radius and speed of the aircraft 100.

權(quán)利要求

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