Flight management system with integrated tactical commands for use with an aircraft and method of operating same

• US 8,494,766 B2
• Filed: 01/07/2011
• Issued: 07/23/2013
• Est. Priority Date: 01/07/2011
• Status: Active Grant

• Current Assignee: GE Aviation Systems LLC (GE Aerospace)
• Original Assignee: GE Aviation Systems LLC (GE Aerospace)
• Inventors: Walter, Randy Lynn
• Primary Examiner(s): Black, Thomas
• Assistant Examiner(s): LOUIE, WAE LENNY
• Application Number:
  US12/986,838
• Publication Number:
  US 20120179368A1
• Time in Patent Office: 928 Days
• Field of Search: 701/206, 701/465, 701/467, 701/120, 701/122, 340/972, 244/182
• US Class Current: 701/465
• CPC Class Codes: G01C 21/20 Instruments for performing navigational calculations G01C21/24, G01C21/26 take precedence
• CPC Class Codes: G05D 1/101 specially adapted for aircraft
• CPC Class Codes: G08G 5/0034 Assembly of a flight plan
• CPC Class Codes: G08G 5/0039 Modification of a flight plan

Abstract

A flight management system for use in automatically generating a flight path trajectory for an aircraft. The flight path trajectory includes a plurality of waypoints and a plurality of vectors that extend between each waypoint of the plurality of waypoints. The flight management system includes a processor that is configured to calculate a first flight path trajectory including an origin waypoint and a destination waypoint. A tactical command that indicates a change in flight trajectory is received. A second flight path trajectory based at least in part on the tactical command is calculated. The calculated second flight path trajectory includes a departure waypoint along the first flight path trajectory, an intercept waypoint along the first flight path trajectory, and a departure vector from the departure waypoint to the intercept waypoint.

Claims

1. A flight management system for use in automatically generating a flight path trajectory for an aircraft, the flight path trajectory including a plurality of waypoints and a plurality of vectors extending between each waypoint of the plurality of waypoints, said flight management system comprising a processor configured to:

calculate a first flight path trajectory including an origin waypoint and a destination waypoint;

receive a tactical command indicating a change in flight trajectory; and

calculate a second flight path trajectory based at least in part on the tactical command, the calculated second flight path trajectory including a departure waypoint along the first flight path trajectory, an intercept waypoint along the first flight path trajectory, and a departure vector from the departure waypoint to the intercept waypoint, wherein said processor is further configured to calculate the departure vector to meet a required time of arrival (RTA) at a selectable waypoint along the second flight path trajectory.

2. A flight management system in accordance with claim 1, wherein said processor is further configured to:

receive a RTA at a merge waypoint along the first flight path trajectory; and

calculate the second flight path trajectory to meet the RTA at the merge waypoint.

3. A flight management system in accordance with claim 1, wherein the tactical command includes a heading vector command, said processor further configured to calculate the second flight path trajectory including a departure vector that includes maintaining the heading vector for a predefined period of time.

4. A flight management system in accordance with claim 3, wherein said processor is further configured to calculate a period of time to maintain the heading vector to meet a RTA at the destination waypoint.

5. A flight management system in accordance with claim 1, wherein the tactical command includes an altitude vector command, said processor further configured to calculate the departure vector including maintaining the altitude for a predefined period of time.

6. A flight management system in accordance with claim 1, wherein the tactical command includes an airspeed vector command, said processor further configured to calculate the second flight path trajectory based on the tactical airspeed command.

7. A flight management system in accordance with claim 1, wherein the tactical command includes one of a flight path angle command and a vertical speed command.

8. A method of operating an aircraft including a flight management system, the method comprising:

calculating, by the flight management system, a first flight path trajectory including an origin waypoint and a destination waypoint;

receiving, by the aircraft flying in the first flight path trajectory, a tactical command indicating a change in flight trajectory; and

calculating, by the flight management system, a second flight path trajectory based at least in part on the tactical command, the calculated second flight path trajectory including a departure waypoint along the first flight path trajectory, an intercept waypoint along the first flight path trajectory, and a departure vector from the departure waypoint to the intercept waypoint, wherein said processor is further configured to calculate the departure vector to meet a required time of arrival (RTA) at a selectable waypoint along the second flight path trajectory.

9. A method in accordance with claim 8, further comprising:

receiving a RTA at a merge waypoint along the first flight path trajectory; and

calculating the second flight path trajectory to meet the RTA at the merge waypoint.

10. A method in accordance with claim 8, further comprising:

calculating the second flight path trajectory such that the departure vector is within a predefined tactical performance envelope.

11. A method in accordance with claim 8, further comprising:

receiving a tactical command including a heading vector command;

calculating the departure vector to maintain the heading vector command for a predefined period of time.

12. A method in accordance with claim 8, further comprising

receiving a tactical command including an altitude vector command;

and

calculating the departure vector to maintain the altitude vector command for a predefined period of time.

13. A method in accordance with claim 8, further comprising receiving a tactical command including an airspeed vector command;

and

calculating the second flight path trajectory based on the tactical airspeed vector command.

14. A method in accordance with claim 8, further comprising:

receiving a tactical command including a flight path angle command;

calculating the second flight pan trajectory based on the flight path angle command.

15. An aircraft comprising:

a flight management system comprising a processor, said processor configured to;

calculate a first flight path trajectory including an origin waypoint and a destination waypoint;

receive a tactical command indicating a change in flight trajectory; and

calculate a second flight path trajectory based at least in part on the tactical command, the calculated second flight path trajectory including a departure waypoint along the first flight path trajectory, an intercept waypoint along the first flight path trajectory, and a departure vector from the departure waypoint to the intercept waypoint, wherein said processor is further configured to calculate the departure vector to meet a required time of arrival (RTA) at a selectable waypoint along the second flight path trajectory.

16. An aircraft in accordance with claim 15, wherein the tactical command includes a heading vector command, said processor further configured to calculate the second flight path trajectory including a departure vector that includes maintaining the heading vector for a predefined period of time.

17. An aircraft in accordance with claim 15, wherein the tactical command includes an altitude vector command, said processor further configured to calculate the departure vector including maintaining the altitude for a period of time.

18. An aircraft in accordance with claim 15, wherein the tactical command includes an airspeed vector command, said processor further configured to calculate the second flight path trajectory based on the tactical airspeed vector command.

19. An aircraft in accordance with claim 15, wherein the tactical command includes one of a flight path angle and a vertical speed command.