System and method to modify an aircraft flight trajectory
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
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The present disclosure is related to modifying a trajectory profile for an aircraft.
An aircraft can include a flight management system that generates a trajectory profile for the aircraft based on a flight plan. The flight plan includes multiple waypoints (e.g., intermediate points) between a starting point of a flight (e.g., a take-off position) and a destination point (e.g., a landing position) of the flight. The trajectory profile is intended to produce a continuous and flyable flight path for the aircraft while complying with industry guidelines (e.g., Federal Aviation Administration (FAA) guidelines). Typically, the trajectory profile is generated using algorithms designed to achieve the flight plan. The algorithms convert a flight plan into a trajectory profile which is a flyable, optimized, four-dimensional path (latitude, longitude, altitude and time) through space that the aircraft is predicted to fly. For example, the algorithm is designed to produce the continuous and flyable path for the aircraft from the starting point to the destination point via the waypoints in the flight plan. The flight management system displays the trajectory profile on a screen within a cockpit of the aircraft, and a pilot of the aircraft can maneuver (or use an autopilot to control) the aircraft to fly the trajectory profile to reach the destination point. In an ideal scenario, flight conditions are permissible to enable the pilot to smoothly maneuver the aircraft past each waypoint along the path.
權(quán)利要求
What is claimed is:1. A method comprising:generating, at a processor, a flight plan of an aircraft, the flight plan based on at least one waypoint and a set of operational rules associated with the aircraft; generating, at the processor, an initial trajectory profile based on at least one waypoint and the set of operational rules; identifying, at the processor, an impermissible flight condition associated with the initial trajectory profile, wherein the impermissible flight condition violates at least one operational rule of the set of operational rules; and generating, at the processor using a closed formed calculation based on one or more of a turn center location indicated by the initial trajectory profile, a turn inbound course indicated by the initial trajectory profile, a turn outboard course indicated by the initial trajectory profile, a turn starting location indicated by the initial trajectory profile, a turn ending location indicated by the initial trajectory profile or a turn radius indicated by the initial trajectory profile, a modified trajectory profile by modifying at least one aspect of the initial trajectory profile to remove the impermissible flight condition. 2. The method of claim 1 , further comprising updating at least one other system with the modified trajectory profile. 3. The method of claim 2 , wherein the at least one other system comprises an autopilot system. 4. The method of claim 1 , further comprising initiating display of the modified trajectory profile. 5. The method of claim 1 , wherein modifying at least one aspect of the initial trajectory profile comprises modifying at least one of:a location of a center of a first turn included in the initial trajectory profile; or a location of a center of a second turn included in the initial trajectory profile, the second turn immediately subsequent to the first turn in the initial trajectory profile. 6. The method of claim 5 , wherein the location of the center of the first turn is moved along an axis that is parallel to an inbound course of the first turn, and wherein the location of the center of the second turn is moved along an axis that is parallel to an outbound course of the second turn. 7. The method of claim 1 , wherein modifying the at least one aspect of the initial trajectory profile comprises inserting a straight segment between a first turn of the initial trajectory profile and a second turn of the initial trajectory profile. 8. The method of claim 7 , wherein modifying the at least one aspect of the initial trajectory profile further comprises rotating the straight segment. 9. The method of claim 1 , further comprising performing a course capture routine to modify the at least one aspect of the initial trajectory profile. 10. The method of claim 1 , wherein modifying the at least one aspect of the initial trajectory profile comprises projecting a line segment from an outbound course by a course capture intercept angle. 11. The method of claim 1 , wherein modifying the at least one aspect of the initial trajectory profile comprises:constructing a flight trajectory between a first waypoint of the flight plan and a third waypoint of the flight plan; and bypassing construction of a flight trajectory between the first waypoint and a second waypoint of the flight plan, wherein the second waypoint is subsequent to the first waypoint, and wherein the third waypoint is subsequent to the second waypoint. 12. The method of claim 1 , wherein modifying the at least one aspect of the initial trajectory profile includes modifying a final point of a first turn included in the initial trajectory profile and performing a course capture on an outbound course associated with a second turn included in the initial trajectory profile. 13. The method of claim 1 , wherein modifying the at least one aspect of the initial trajectory profile includes modifying an initial point of a first turn included in the initial trajectory profile. 14. The method of claim 1 , wherein the impermissible flight condition is identified based on a first distance between a first waypoint and a final point of a first turn included in the initial trajectory profile and a second distance between a second waypoint and the first waypoint. 15. The method of claim 1 , wherein the impermissible flight condition is identified based on a first distance between a final point of a first turn included in the initial trajectory profile and a first waypoint and a second distance between an initial point of a second turn included in the initial trajectory profile and the first waypoint. 16. The method of claim 1 , wherein the impermissible flight condition is identified based on a comparison of a bank angle included in the initial trajectory profile and a bank angle determined based on an airspeed of the aircraft. 17. The method of claim 1 , wherein the impermissible flight condition is identified based on an incomplete turn within the initial trajectory profile. 18. The method of claim 1 , wherein the impermissible flight condition is identified based on an angle of a first turn of the initial trajectory profile. 19. The method of claim 1 , further comprising:determining whether at least three bypass waypoints are included in adjacent legs of the flight plan; 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; and grouping the more than two bypass waypoints based on a centroid of the more than two bypass waypoints. 20. The method of claim 1 , wherein the impermissible flight condition is identified based on:a flight time associated with the initial trajectory profile exceeding a particular flight time; or a flight distance associated with the initial trajectory profile exceeding a particular flight distance. 21. The method of claim 1 , wherein the impermissible flight condition is identified based on a turn radius of a particular turn within the initial trajectory profile being greater than a threshold radius associated with capturing a hold. 22. The method of claim 1 , wherein modifying the at least one aspect of the initial trajectory profile comprises 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. 23. The method of claim 1 , wherein modifying the at least one aspect of the initial trajectory profile comprises 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. 24. The method of claim 1 , wherein modifying the at least one aspect of the initial trajectory profile comprises 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. 25. The method of claim 1 , wherein modifying the at least one aspect of the initial trajectory profile comprises 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. 26. An aircraft comprising:a memory storing a set of operational rules associated with the aircraft; and a flight management system coupled to the memory and configured to:generate a flight plan based on at least one waypoint and the set of operational rules; generate an initial trajectory profile based on at least one waypoint and the set of operational rules; identify an impermissible flight condition associated with the initial trajectory profile, wherein the impermissible flight condition violates at least one operational rule of the set of operational rules; and use a closed formed calculation based on one or more of a turn center location indicated by the initial trajectory profile, a turn inbound course indicated by the initial trajectory profile, a turn outboard course indicated by the initial trajectory profile, a turn starting location indicated by the initial trajectory profile, a turn ending location indicated by the initial trajectory profile or a turn radius indicated by the initial trajectory profile to generate a modified trajectory profile by modifying at least one aspect of the initial trajectory profile to remove the impermissible flight condition. 27. The aircraft of claim 26 , wherein the set of operational rules includes rules specified by a manufacturer of the aircraft, rules specified by a government agency, user-entered rules, or a combination thereof. 28. The aircraft of claim 26 , further comprising a display screen configured to display the modified trajectory profile. 29. A non-transitory computer-readable medium storing instructions that, when executed by a processor on-board an aircraft, cause the processor to perform operations comprising:generating a flight plan of the aircraft, the flight plan based on at least one waypoint and a set of operational rules associated with the aircraft; generating an initial trajectory profile based on at least one waypoint and the set of operational rules; identifying an impermissible flight condition associated with the initial trajectory profile, wherein the impermissible flight condition violates at least one operational rule of the set of operational rules; and generating, using a closed formed calculation based on one or more of a turn center location indicated by the initial trajectory profile, a turn inbound course indicated by the initial trajectory profile, a turn outboard course indicated by the initial trajectory profile, a turn starting location indicated by the initial trajectory profile, a turn ending location indicated by the initial trajectory profile or a turn radius indicated by the initial trajectory profile, a modified trajectory profile by modifying at least one aspect of the initial trajectory profile to remove the impermissible flight condition. 30. The non-transitory computer-readable medium of claim 29 , wherein the operations further comprise updating at least one other system with the modified trajectory profile. 31. The non-transitory computer-readable medium of claim 30 , wherein the at least one other system comprises an autopilot system. 32. A method comprising:generating, at a processor, a flight plan of an aircraft, the flight plan based on at least one waypoint and a set of operational rules associated with the aircraft; generating, at the processor, an initial trajectory profile based on at least one waypoint and the set of operational rules; identifying, at the processor, an impermissible flight condition associated with the initial trajectory profile, wherein the impermissible flight condition violates at least one operational rule of the set of operational rules; and generating, at the processor using a closed formed calculation based on one or more of a turn center location indicated by the initial trajectory profile, a turn inbound course indicated by the initial trajectory profile, a turn outboard course indicated by the initial trajectory profile, a turn starting location indicated by the initial trajectory profile, a turn ending location indicated by the initial trajectory profile or a turn radius indicated by the initial trajectory profile, a modified trajectory profile by modifying at least one aspect of the initial trajectory profile to remove the impermissible flight condition, wherein identifying the impermissible flight condition and modifying the at least one aspect of the initial trajectory profile comprises performing at least one flight plan correction with a path capture transition.
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