Methods and apparatus for obtaining aircraft landing guidance

Patent metadata

Field	Value
Publication number	US-9953541-B2
Application number	US-201615049719-A
Country	US
Kind code	B2
Filing date	Feb 22, 2016
Priority date	Feb 22, 2016
Publication date	Apr 24, 2018
Grant date	Apr 24, 2018

Abstract

A method for receiving data onboard an aircraft is provided. The method obtains a plurality of aircraft transponder messages associated with a particular landing zone; extracts, from each of the plurality of aircraft transponder messages, aircraft position data associated with landing at least one lead aircraft at the particular landing zone; and determines a landing path for use by the aircraft to land at the particular landing zone, based on the extracted aircraft position data.

First claim

What is claimed is:

1. A method for receiving data onboard a second aircraft, the method comprising:
obtaining, by the second aircraft, a plurality of aircraft transponder messages associated with a particular landing zone during flight of the second aircraft;
extracting, from each of the plurality of aircraft transponder messages, lead aircraft position data associated with landing at least one lead aircraft at the particular landing zone, wherein the at least one lead aircraft has landed at the particular landing zone; and
determining a landing path for use by the second aircraft to land at the particular landing zone, based on the extracted aircraft position data, by:
averaging the lead aircraft position data of the at least one lead aircraft; and
determining a mean landing path, based on the averaging, wherein the landing path comprises the mean landing path.

2. The method of claim 1 , wherein obtaining the plurality of aircraft transponder messages further comprises:
receiving the plurality of aircraft transponder messages via aircraft-to-aircraft communication.

3. The method of claim 1 , wherein obtaining the plurality of aircraft transponder messages further comprises:
receiving the plurality of aircraft transponder messages via ground control-to-aircraft communication.

4. The method of claim 1 , further comprising:
identifying a current position for the second aircraft;
calculating a lateral deviation and a vertical deviation between the landing path and the current position; and
presenting flight guidance onboard the second aircraft, based on the lateral deviation and the vertical deviation.

5. The method of claim 1 , further comprising:
selecting, from the plurality of aircraft transponder messages, a subset associated with a particular aircraft type; and
determining the landing path using the subset.

6. The method of claim 1 , further comprising:
selecting, from the plurality of aircraft transponder messages, a subset associated with a particular weight-load balance for the at least one lead aircraft; and
determining the landing path using the subset.

7. The method of claim 1 , further comprising:
selecting, from the plurality of aircraft transponder messages, a subset associated with particular aircraft dimensions; and
determining the landing path using the subset.

8. The method of claim 1 , wherein the second aircraft and the at least one lead aircraft are equipped with Automatic Dependent Surveillance-Broadcast (ADS-B) transponders;
wherein the aircraft transponder messages comprise ADS-B Out messages; and
wherein the second aircraft receives the aircraft transponder messages via ADS-B In.

9. The method of claim 1 , wherein the landing path comprises a series of positions associated with landing the at least one lead aircraft at the particular landing zone, wherein each of the series of positions comprises a latitude, a longitude, and an altitude.

10. A system for receiving data onboard a second aircraft, the system comprising:
a system memory element;
an aircraft transponder, configured to receive a plurality of transponder messages associated with a particular landing zone during flight of the second aircraft; and
at least one processor, communicatively coupled to the system memory element and the aircraft transponder, the at least one processor configured to:
analyze each of the plurality of transponder messages;
identify lead aircraft position data associated with landing at least one lead aircraft at the particular landing zone, based on analyzing each of the plurality of transponder messages, wherein the at least one lead aircraft has landed at the particular landing zone; and
determine a landing path for landing the second aircraft at the particular landing zone, based on the identified lead aircraft position data, by:
calculating an average of the lead aircraft position data of the at least one lead aircraft; and
determining a mean landing path, based on the average, wherein the landing path comprises the mean landing path.

11. The system of claim 10 , wherein the aircraft transponder comprises an Automatic Dependent Surveillance-Broadcast (ADS-B);
wherein the aircraft transponder messages comprise ADS-B Out messages; and
wherein the second aircraft receives the aircraft transponder messages via ADS-B In.

12. The system of claim 10 , wherein the landing path comprises a series of positions associated with landing the at least one lead aircraft at the particular landing zone, wherein each of the series of positions comprises a latitude, a longitude, and an altitude; and
wherein the at least one processor is further configured to:
identify current position for the second aircraft, the current position comprising a current latitude, a current longitude, and a current altitude;
calculate a lateral deviation and a vertical deviation between one of the series of positions of the landing path and the current position; and
present flight guidance onboard the second aircraft, based on the lateral deviation and the vertical deviation.

13. The system of claim 10 , wherein the at least one processor is further configured to:
select, from the plurality of transponder messages, a subset associated with a particular type of aircraft; and
determine the landing path using the subset.

14. A non-transitory, computer-readable medium containing instructions thereon, which, when executed by a processor, perform a method comprising:
receiving, via a transponder onboard a second aircraft, landing path data for a particular landing zone, wherein the landing path data comprises lead aircraft position data included in transponder messages broadcast by at least one lead aircraft that has landed at the particular landing zone, and wherein the transponder messages are received via the transponder during flight of the second aircraft;
identifying a current position of the second aircraft using avionics systems onboard the aircraft; and
determining lateral guidance and vertical guidance for the second aircraft, based on the landing path data and the current position of the second aircraft, by:
averaging the lead aircraft position data of the at least one lead aircraft; and
determining a mean landing path, based on the averaging, wherein lateral guidance and vertical guidance comprise the mean landing path.

15. The non-transitory, computer-readable medium of claim 14 , wherein determining the lateral guidance and the vertical guidance further comprises:
calculating a lateral deviation between a current lateral position of the second aircraft and a required lateral position, wherein the current position comprises the current lateral position, and wherein the landing path data comprises the required lateral position; and
calculating a vertical deviation between a current vertical position of the second aircraft and a required vertical position, wherein the current position comprises the current vertical position, and wherein the landing path data comprises the required vertical position.

16. The non-transitory, computer-readable medium of claim 14 , wherein the lateral guidance and vertical guidance are determined by a flight management system (FMS) onboard the second aircraft.

17. The non-transitory, computer-readable medium of claim 14 , wherein the lateral guidance and vertical guidance are determined using an electronic flight bag (EFB) associated with the second aircraft.

18. The non-transitory, computer-readable medium of claim 14 , wherein the method further comprises:
identifying a subset of

Assignees

• Honeywell Int Inc

Inventors

• Kuttappan Sujith
• Agarwal Jitender Kumar

Classifications

• B64D43/00

  Arrangements or adaptations of instruments · CPC title

• B64D45/04

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

• G01C23/00

  Combined instruments indicating more than one navigational value, e.g. for aircraft; Combined measuring devices for measuring two or more variables of movement, e.g. distance, speed or acceleration · CPC title

• G08G5/025 Primary

  Physics · mapped topic

• G08G5/723

  from the aircraft · CPC title