Environmental waypoint insertion

Patent metadata

Field	Value
Publication number	US-10024665-B2
Application number	US-201514617156-A
Country	US
Kind code	B2
Filing date	Feb 9, 2015
Priority date	Aug 20, 2010
Publication date	Jul 17, 2018
Grant date	Jul 17, 2018

Abstract

The different advantageous embodiments provide a system and method for suggesting significant environmental waypoints along a trajectory to improve the efficiency of a flight plan. Desired information is identified, wherein the desired information is information needed to perform at least one of completing a flight plan and updating a flight plan. It is determined whether to identify environmental information points.

First claim

What is claimed is:

1. A method of generating flight trajectory environmental information points, the method comprising:
receiving, by a processor unit, an environmental information point from an environmental source, wherein the environmental information point identifies a location of the environmental information point and environmental information for the location;
determining, by the processor unit, whether the location of the environmental information point is along a flight trajectory;
determining, by the processor unit, whether the environmental information identified for the environmental information point is significant; and
inserting, by the processor unit, a waypoint corresponding to the environmental information point into a flight plan in response to a determination that the location of the environmental information point is along the fight trajectory and that the environmental information identified for the environmental information point is significant.

2. The method of claim 1 further comprising:
running a trajectory method, wherein the trajectory method generates a number of pseudo waypoints for the flight plan; and
wherein inserting the waypoint corresponding to the environmental information point into the flight plan comprises associating the environmental information point with a one of the number of pseudo waypoints generated.

3. The method of claim 1 , wherein the environmental information identifies environmental conditions at the location selected from the group of environmental conditions consisting of weather, temperature, pressure, humidity, turbulence, wind speed, and wind direction.

4. The method of claim 1 , wherein determining whether the environmental information identified for the environmental information point is significant comprises determining whether the environmental information identifies an environmental condition that influences the flight prediction cost, time, fuel, or performance causing errors in flight predictions for an aircraft following the flight plan to exceed a threshold value for a configured acceptance.

5. The method of claim 1 , wherein inserting the waypoint corresponding to the environmental information point into the flight plan comprises associating the environmental information point with a pseudo waypoint inserted into the flight plan.

6. The method of claim 1 further comprising:
partitioning a portion of a one of the flight trajectory and the flight plan into a plurality of segments, wherein an end of a segment in the plurality of segments comprises a pseudo waypoint, wherein the pseudo waypoint does not correspond to a waypoint that is already in the flight plan;
and
wherein inserting the waypoint corresponding to the environmental information point into the flight plan comprises associating the environmental information point with the pseudo waypoint.

7. The method of claim 6 , wherein partitioning the portion of the one of the flight trajectory and the flight plan into the plurality of segments comprises partitioning the portion of the one of the flight trajectory and the flight plan into the plurality of segments of approximately equal length.

8. The method of claim 6 , wherein determining whether the location of the environmental information point is along the flight trajectory comprises identifying from a plurality of environmental information points whether the location of the environmental information point is closest to the pseudo waypoint.

9. An apparatus configured to generate a flight plan for a flight trajectory, the apparatus comprising a processor unit configured to:
receive an environmental information point from an environmental source, wherein the environmental information point identifies a location of the environmental information point and environmental information for the location;
determine whether the location of the environmental information point is along the flight trajectory;
determine whether the environmental information identified for the environmental information point is significant; and
insert a waypoint corresponding to the environmental information point into the flight plan in response to a determination that the location of the environmental information point is along the fight trajectory and that the environmental information identified for the environmental information point is significant.

10. The apparatus of claim 9 further comprising a waypoint insertion manager configured to:
run a trajectory method wherein the trajectory method generates a number of pseudo waypoints for the flight plan; and
associate the environmental information point with a one of the number of pseudo waypoints generated to insert the waypoint corresponding to the environmental information point into the flight plan.

11. The apparatus of claim 9 ,
wherein the environmental information identifies environmental conditions at the location selected from the group of environmental conditions consisting of weather, temperature, pressure, humidity, turbulence, wind speed, and wind direction.

12. The apparatus of claim 9 , further comprising an assessment processor configured to determine whether the environmental information identified for the environmental information point is significant by determining whether the environmental information identifies an environmental condition that influences the flight prediction cost, time, fuel or performance causing errors in flight predictions for an aircraft following the flight plan to exceed a threshold value for a configured acceptance.

13. The apparatus of claim 9 , further comprising a waypoint insertion manager configured to associate the environmental information point with a pseudo waypoint inserted into the flight plan to insert the waypoint corresponding to the environmental information point into the flight plan.

14. The apparatus of claim 9 further comprising:
a waypoint insertion manager configured to partition a portion of a one of the flight trajectory and the flight plan into a plurality of segments, wherein an end of a segment in the plurality of segments comprises a pseudo waypoint, wherein the pseudo waypoint does not correspond to a waypoint that is already in the flight plan, and insert the waypoint corresponding to the environmental information point into the flight plan by associating the environmental information point with the pseudo waypoint.

15. The apparatus of claim 14 , wherein the waypoint insertion manager is configured to partition the portion of the one of the flight trajectory and the flight plan into the plurality of segments of approximately equal length.

16. The apparatus of claim 14 , wherein the waypoint insertion manager is configured to determine whether the location of the environmental information point is along the flight trajectory by determining from a plurality of environmental information points whether the location of the environmental information point is closest to the pseudo waypoint.

Assignees

• Boeing Co

Inventors

• Bailey Louis J
• Hale Ryan D

Classifications

• G01C21/20 Primary

  Instruments for performing navigational calculations (G01C21/24, G01C21/26 take precedence) · CPC title

• G08G5/0039

  Physics · mapped topic

• G08G5/0091

  Physics · mapped topic

• G01C21/00 Primary

  Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 (measuring distance traversed on the ground by a vehicle G01C22/00; control of position, course, altitude or attitude of vehicles G05D1/00; traffic control systems for road vehicles involving transmission of navigation instructions to the vehicle G08G1/0968) · CPC title

• G08G5/0034

  Physics · mapped topic