Flight path management system
Systems and methods for determining a flight path of an aircraft are provided. In one embodiment, a method can include identifying one or more parameter(s) associated with a moving target. The method can include determining a moving circular flight path associated with the moving target based at least in part on the parameter(s) associated with the moving target. The method can include identifying one or more condition(s) associated with at least one of the aircraft and the moving circular flight path. The method can include determining a flight path of the aircraft from a location of the aircraft to the moving circular flight path based at least in part on the parameter(s) associated with the moving target and the condition(s) associated with at least one of the aircraft and the moving circular flight path.
1. A computer-implemented method of determining a flight path of an aircraft, the method comprising:
identifying, by one or more computing devices associated with an aircraft, parameters associated with a moving target, the parameters including an initial location of the moving target, a track of the moving target, a speed of the moving target, and a reference time associated with the moving target;
determining, by the one or more computing devices, a moving circular flight path associated with the moving target such that the moving target is surrounded by the moving circular flight path based at least in part on the parameters associated with the moving target;
identifying, by the one or more computing devices, one or more conditions associated with at least one of the aircraft and the moving circular flight path, wherein the one or more conditions include predicted conditions, the predicted conditions including a planned speed change; and
determining, by the one or more computing devices, a flight path of the aircraft from a location of the aircraft to the moving circular flight path based at least in part on the parameters associated with the moving target and the one or more conditions associated with at least one of the aircraft and the moving circular flight path, wherein the flight path of the aircraft is determined as a minimum lateral time flight path associated with a minimum time for the aircraft to reach the moving circular path from the location of the aircraft.
2. The computer-implemented method of claim 1 , wherein the flight path comprises a first segment and a second segment, wherein the first segment of the flight path is associated with a first path from the location of the aircraft to within proximity of a circumference of the moving circular flight path, and wherein the second segment is associated with a second path to orient the aircraft to travel in accordance with the moving circular flight path, wherein the second segment comprises a transition turn around an intercept point that joining the moving circular flight path.
3. The computer-implemented method of claim 2 , wherein the first segment includes a substantially straight path.
4. The computer-implemented method of claim 1 , wherein the flight path of the aircraft is determined to decrease a travel time for the aircraft to travel from the current location of the aircraft to the moving circular flight path.
5. The computer-implemented method of claim 1 , wherein the moving circular flight path associated with the moving target moves laterally such that the moving target remains within the moving circular flight path.
6. The computer-implemented method of claim 1 , further comprising:
generating, by the one or more computing devices, an output indicative of the flight path of the aircraft; and
providing for display, by the one or more computing devices, the output indicative of the flight path of the aircraft on a user interface of a display device.
7. The computer-implemented method of claim 1 , further comprising:
receiving, by the one or more computing devices, a set of data indicative of an acceptance of the flight path.
8. The computer-implemented method of claim 1 , further comprising:
implementing, by the one or more computing devices, the flight path such that the aircraft is to travel according to the flight path.
9. The computer-implemented method of claim 1 , wherein determining the flight path of the aircraft from the location of the aircraft to the moving circular flight path comprises:
receiving, by the one or more computing devices, an update to at least one of the parameters and the one or more conditions; and
determining, by the one or more computing devices, the flight path of the aircraft based at least in part on at least one of the updated parameters and the updated conditions.
10. A computing system for determining a flight path of an aircraft, the system comprising:
one or more processors included on an aircraft; and
one or more memory devices included on the aircraft, the one or more memory devices storing instructions that when executed by the one or more processors cause the one or more processors to:
identify a moving target;
identify parameters associated with the moving target, wherein the parameters comprise an initial location of the moving target and a velocity of the moving target;
determine a moving circular flight path associated with the moving target such that the moving target is within the moving circular flight path based at least in part on the one or more parameters associated with the moving target;
identify one or more conditions associated with at least one of the aircraft and the moving circular flight path, wherein the one or more conditions include predicted conditions, the predicted conditions including a planned speed change; and
determine a flight path of the aircraft from a location of the aircraft to the moving circular flight path based at least in part on the parameters associated with the moving target and the one or more conditions associated with at least one of the aircraft and the moving circular flight path, wherein the flight path of the aircraft is determined as a minimum lateral time flight path associated with a minimum time for the aircraft to reach the moving circular path from the location of the aircraft.
11. The system of claim 10 , wherein the flight path of the aircraft is determined to decrease a travel time for the aircraft to travel from the location to the moving circular flight path.
12. The system of claim 10 , wherein the one or more processors are further to:
generate an output indicative of the flight path of the aircraft; and
provide for display the output indicative of the flight path of the aircraft on a user interface of a display device.
13. The system of claim 12 , wherein the one or more processors are further to:
receive a set of data indicative of an acceptance of the flight path via the user interface; and
implement the flight path such that the aircraft is to travel according to the flight path.
14. The system of claim 10 , wherein the flight path comprises a first segment and a second segment, wherein the first segment of the flight path is associated with a first path from the location to a circumference of the moving circular flight path, and wherein the second segment is associated with a second path to orient the aircraft to travel in accordance with the moving circular flight path.
15. An aircraft, comprising:
a flight management system configured to
identify one or more parameters associated with a moving target, including an initial location of the moving target, a track of the moving target, and a speed of the moving target, and a reference time associated with the moving target,
determine a moving circular flight path associated with the moving target such that the moving target is located within the moving circular flight path, wherein the moving circular flight path associated with the target moves such that the target remains within the moving circular flight path,
identify one or more conditions associated with at least one of the aircraft and the moving circular flight path, wherein the one or more conditions include predicted conditions, the predicted conditions including a planned speed change,
determine a flight path of the aircraft from a location of the aircraft to the moving circular flight path based at least in part on the parameters associated with the moving target and the one or more conditions associated with at least one of the aircraft and the moving circular flight path, wherein the flight path of the aircraft is determined as a minimum lateral time flight path associated with a minimum time for the aircraft to reach the moving circular path from the location of the aircraft,
generate an output indicative of the flight path, and
provide for display the output indicative of the flight path of the aircraft; and
a control display system configured to display the output indicative of the flight path of the aircraft for display on a user interface of a display device.
16. The aircraft of claim 15 , wherein the location of the aircraft is a future location of the aircraft.
17. The aircraft of claim 15 , wherein to identify the parameters associated with the moving target, the flight management system is further configured to receive a set of data indicative of the parameters associated with the moving target from one or more remote computing devices that are not included on the aircraft.
18. The aircraft of claim 15 , wherein to determine the moving circular flight path associated with the moving target, the flight management system is further configured to receive a set of data indicative of the moving circular flight path associated with the moving target from one or more remote computing devices that are not included on the aircraft.
19. The aircraft of claim 15 , wherein the flight path of the aircraft is determined to decrease a travel time for the aircraft to travel from the location to the moving circular flight path.