Aircraft landing systems and methods

Patent metadata

Field	Value
Publication number	US-11851206-B2
Application number	US-202117644963-A
Country	US
Kind code	B2
Filing date	Dec 17, 2021
Priority date	Dec 17, 2021
Publication date	Dec 26, 2023
Grant date	Dec 26, 2023

Abstract

A computer-implemented method of navigating a vertical take-off and landing (“VTOL”) vehicle near a landing zone, may comprise receiving data related to a first radar signal reflected from at least one corner reflector; determining whether the received data is consistent with a predefined target landing zone; upon determining that the received data is consistent with the predefined target landing zone, determining a location of the VTOL vehicle relative to the predefined target landing zone, using a second radar signal reflected from at least one corner reflector; and determining whether the location of the VTOL vehicle is consistent with a predefined landing position.

First claim

What is claimed is:

1. A computer-implemented method of navigating a vertical take-off and landing (“VTOL”) vehicle near a landing zone, the method comprising:
receiving data related to a first radar signal reflected from at least one corner reflector;
determining whether the received data is consistent with a predefined target landing zone;
upon determining that the received data is consistent with the predefined target landing zone, determining a location of the VTOL vehicle relative to the predefined target landing zone, using a second radar signal reflected from at least one corner reflector;
determining whether the location of the VTOL vehicle is consistent with a predefined landing position; and
upon determining that the location of the VTOL vehicle is inconsistent with the predefined landing position, automatically repositioning the VTOL.

2. The computer-implemented method of claim 1 , wherein the first radar signal is reflected from at least three corner reflectors, wherein the corner reflectors are arranged in a triangular array.

3. The computer-implemented method of claim 2 , wherein the first radar signal is reflected from exactly three corner reflectors.

4. The computer-implemented method of claim 1 , further comprising:
upon determining that the location of the VTOL vehicle is consistent with the predefined landing position, automatically landing the VTOL.

5. The computer-implemented method of claim 1 , further comprising:
upon determining that the location of the VTOL vehicle is consistent with the predefined landing position, providing a visual or auditory indicator to an operator of the VTOL vehicle.

6. The computer-implemented method of claim 1 , wherein the determining whether the received data is consistent with the predefined target landing zone includes comparing the received data to a library of landing zone profiles.

7. The computer-implemented method of claim 6 , wherein the determining whether the received data is consistent with the predefined target landing zone includes determining at least one of a maximum reflection, radar cross-section, a size, or a color of the at least one corner reflector.

8. A computer-implemented method of navigating a VTOL vehicle near a landing zone, the method comprising:
receiving data related to a radar signal reflected from at least three corner reflectors on a predefined target landing zone;
using the received data, determining whether a location of the VTOL vehicle is consistent with a predefined landing position, wherein the determining includes comparing the received data to a predefined profile in a library having a plurality of profiles of a plurality of landing positions; and
upon determining that the location of the VTOL vehicle is consistent with the predefined landing position, automatically landing the VTOL vehicle or providing a visual or auditory indicator to an operator of the VTOL vehicle.

9. The computer-implemented method of claim 8 , wherein the three corner reflectors define a triangle.

10. The computer-implemented method of claim 8 , wherein the determining whether the location of the VTOL vehicle is consistent with the predefined landing position also includes analyzing a visual indicator.

11. The computer-implemented method of claim 8 , wherein the predefined profile includes at least one of a shape, size, or color of the at least three corner reflectors.

12. The computer-implemented method of claim 8 , wherein the received data is related to the radar signal reflected from exactly three corner reflectors.

13. A system for vehicle landing, the system comprising:
a first corner reflector;
a second corner reflector; and
a third corner reflector, wherein the first corner reflector, the second corner reflector, and the third corner reflector are arranged in a triangular shape on a single landing zone for a vertical take-off and landing (“VTOL”) vehicle, wherein the first corner reflector has a first radar cross section (“RCS”), wherein the second corner reflector has a second RCS, wherein the first RCS differs from the second RCS, wherein the third corner reflector has a third RCS, and wherein the third RCS differs from the first RCS and the second RCS.

14. The system of claim 13 , wherein a center point of the landing zone is within the triangular shape.

15. The system of claim 13 , wherein each of the first corner reflector, the second corner reflector, and the third corner reflector has a trihedral shape.

16. The system of claim 13 , wherein the triangular shape is at least one of an equilateral shape, an isosceles shape, or a scalene shape.

17. The system of claim 13 , wherein the triangular shape is a first triangular shape, and wherein the landing zone is a first landing zone, the system further comprising:
a fourth corner reflector;
a fifth corner reflector; and
a sixth corner reflector, wherein the fourth corner reflector, the fifth corner reflector, and the sixth corner reflector are arranged in a second triangular shape on a second landing zone.

18. The system of claim 13 , wherein the first corner reflector and the second corner reflector are separated by a first distance, wherein the third corner reflector is separated from a midpoint between the first corner reflector and the second corner reflector by a second distance, wherein the second distance is greater than the first distance.

19. The system of claim 13 , wherein the first corner reflector includes a 5 dBsm trihedral corner reflector, a 10 dBsm trihedral corner reflector, or a 15 dBsm trihedral corner reflector.

20. The system of claim 13 , wherein the system includes exactly three corner reflectors.

Assignees

• Honeywell Int Inc

Inventors

• Pos Marc
• Surace Lawrence

Classifications

• G08G5/54

  for approach or landing · CPC title

• G08G5/21

  located onboard the aircraft · CPC title

• G08G5/74

  for monitoring terrain · CPC title

• B64D45/04 Primary

  Landing aids; Safety measures to prevent collision with earth's surface · CPC title

• B64F1/18

  Visual or acoustic landing aids · CPC title