Aircraft guidance to moving target point

Patent metadata

Field	Value
Publication number	US-12293673-B2
Application number	US-202217659070-A
Country	US
Kind code	B2
Filing date	Apr 13, 2022
Priority date	Apr 13, 2022
Publication date	May 6, 2025
Grant date	May 6, 2025

Abstract

A method of guidance for an aircraft includes obtaining relative position data indicative of a direction from a location of the aircraft to a location of a moving target point. The method also includes determining, based on the relative position data, a location of a virtual leader based on projecting the location of the aircraft onto a virtual leader path, where the virtual leader path corresponds to a straight approach path to the location of the moving target point along a desired approach direction. The method further includes determining, based on the location of the virtual leader, a guidance input to cause the aircraft to follow the virtual leader.

First claim

What is claimed is:

1. A method of guidance for an aircraft, the method comprising:
obtaining, at one or more processors of a guidance system, first relative position data indicative of a direction from a first location of the aircraft at a first time to a first location of a moving target point at the first time;
determining, by the one or more processors based on the first relative position data, a first location of a virtual leader based on projecting the first location of the aircraft onto a first virtual leader path, wherein the first virtual leader path corresponds to a straight approach path to the first location of the moving target point along a desired approach direction, the virtual leader distinct from the moving target point;
determining, by the one or more processors based on the first location of the virtual leader, a guidance input to cause the aircraft to follow the virtual leader;
causing, by the one or more processors, the aircraft to follow the virtual leader by providing the guidance input to the aircraft;
determining, by the one or more processors, a second location of the virtual leader based on the first location, the first virtual leader path, and a virtual velocity associated with the virtual leader; and
determining, by the one or more processors based on the second location of the virtual leader, a second guidance input to cause the aircraft to follow the virtual leader;
obtaining, by the one or more processors, second relative position data indicative of a second direction from a second location of the aircraft at a second time to a second location of the moving target point at the second time;
determining, by the one or more processors based on the second relative position data, a third location of the virtual leader based on projecting the second location of the aircraft onto a second virtual leader path; and
determining, by the one or more processors based on the third location of the virtual leader, a third guidance input to cause the aircraft to follow the virtual leader.

2. The method of claim 1 , further comprising determining an initial virtual leader relative direction based on approach criteria associated with an approach of the aircraft to the moving target point.

3. The method of claim 1 , wherein the first relative position data is based on data from one or more sensors onboard the aircraft.

4. The method of claim 3 , wherein the moving target point is onboard a vehicle, and wherein the first relative position data is further based on data from one or more sensors onboard the vehicle.

5. The method of claim 3 , wherein the one or more sensors onboard the aircraft include one or more of a global position system (GPS) receiver, one or more passive electromagnetic sensors, one or more active electromagnetic sensors, or one or more inertial measurement sensors.

6. The method of claim 1 , wherein the moving target point is onboard a vehicle, and wherein the first relative position data is received via transmission from the vehicle and is based on data from one or more sensors onboard the vehicle.

7. The method of claim 6 , wherein the one or more sensors onboard the vehicle include one or more of a global position system (GPS) receiver, one or more passive electromagnetic sensors, one or more active electromagnetic sensors, or one or more inertial measurement sensors.

8. The method of claim 1 , wherein the moving target point corresponds to an aircraft recovery device that is coupled to a vehicle that is in motion.

9. The method of claim 8 , wherein the vehicle corresponds to a watercraft, a second aircraft, or a land craft.

10. The method of claim 8 , wherein the motion of the vehicle is due at least in part to a propulsion system of the vehicle.

11. The method of claim 8 , wherein the motion of the vehicle is due at least in part to external forces applied to the vehicle by its environment.

12. The method of claim 8 , wherein the motion of the vehicle includes periodic or occasional rotation about a first axis of the vehicle, and wherein the direction from the first location of the aircraft to the first location of the moving target point is substantially aligned with the first axis.

13. The method of claim 8 , wherein the motion of the vehicle includes rotation about a first axis of the vehicle and translation along the first axis.

14. The method of claim 8 , wherein the motion of the vehicle is due to movement of the vehicle with respect to an irregular surface.

15. The method of claim 1 , wherein the aircraft corresponds to a fixed wing aircraft.

16. The method of claim 1 , wherein the guidance input includes a bank angle.

17. A system comprising:
an aircraft;
an aircraft recovery device configured to be coupled to a vehicle and configured to recover the aircraft while the vehicle is in motion; and
a guidance system comprising one or more processors, the guidance system configured to:
obtain first relative position data indicative of a direction from a first location of the aircraft at a first time to a first location of a moving target point of the aircraft recovery device at the first time;
determine, based on the first relative position data, a first location of a virtual leader based on projection of first aircraft location information onto a first virtual leader path, wherein the first virtual leader path corresponds to a straight approach path to the first location of the moving target point along a desired approach direction, the virtual leader distinct from the moving target point;
determine, based on the first location of the virtual leader, a guidance input to cause the aircraft to follow the virtual leader;
cause the aircraft to follow the virtual leader by providing the guidance input to the aircraft;
determine a second location of the virtual leader based on the first location, the first virtual leader path, and a virtual velocity associated with the virtual leader;
determine, based on the second location of the virtual leader, a second guidance input to cause the aircraft to follow the virtual leader;
obtain second relative position data indicative of a second direction from a second location of the aircraft at a second time to a second location of the moving target point at the second time;
determine, based on the second relative position data, a third location of the virtual leader based on projecting the second location of the aircraft onto a second virtual leader path; and
determine, based on the third location of the virtual leader, a third guidance input to cause the aircraft to follow the virtual leader.

18. The system of claim 17 , wherein the guidance system is disposed onboard the aircraft.

19. The system of claim 17 , wherein the guidance system is disposed onboard the vehicle.

20. An aircraft comprising:
a guidance system comprising one or more processors, the guidance system configured to:
obtain first relative position data indicative of a direction from a first location of the aircraft at a first time to a first location of a moving target point at the first time;
determine, based on the first relative position data, a first location of a virtual leader based on projection of first aircraft location information onto a first virtual leader path, wherein the first virtual leader path corresponds to a straight approach path to the first location of the moving target point along a desired approach direction, the virtual leader distinct from the moving target point;
determine, based on the first location of the virtual leader, a gu

Assignees

• Boeing Co

Inventors

• Rysdyk Rolf
• Nasroullahi Mohammad Ehsan

Classifications

• G01C21/3438

  Rendezvous; Ride sharing · CPC title

• B64D25/00

  Emergency apparatus or devices, not otherwise provided for · CPC title

• G08G5/54

  for approach or landing · CPC title

• G08G5/26

  Transmission of traffic-related information between aircraft and ground stations · CPC title

• G08G5/21

  located onboard the aircraft · CPC title