System and method for ground navigation

• US 9,354,633 B1
• Filed: 10/31/2008
• Issued: 05/31/2016
• Est. Priority Date: 10/31/2008
• Status: Active Grant

• Current Assignee: Rockwell Collins, Inc. (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: Rockwell Collins, Inc. (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Chaigneau, Bertrand, Itcia, Eric, McCusker, Patrick D.
• Primary Examiner(s): Shumate, Victoria P
• Assistant Examiner(s): Reyes, Reginald R
• Application Number:
  US12/263,282
• Time in Patent Office: 2,769 Days
• Field of Search: 701/200
• US Class Current: 1/1
• CPC Class Codes: G01S 13/60 wherein the transmitter and receiver are mounted on the moving object, e.g. for determining ground speed, drift angle, ground track G01S13/64 takes precedence
• CPC Class Codes: G01S 13/87 Combinations of radar systems, e.g. primary radar and secondary radar
• CPC Class Codes: G01S 13/88 Radar or analogous systems specially adapted for specific applications electromagnetic prospecting or detecting of objects, e.g. near-field detection, G01V3/00
• CPC Class Codes: G01S 13/953 mounted on aircraft
• CPC Class Codes: G01S 3/043 Receivers
• CPC Class Codes: G05D 1/0022 characterised by the communication link data switching networks in general H04L12/00
• CPC Class Codes: G05D 1/0083 to help an aircraft pilot in the rolling phase
• CPC Class Codes: G05D 1/0257 using a radar radar systems designed for anti-collision purposes between land vehicles or between land vehicle and fixed obstacles G01S13/931
• CPC Class Codes: Y02A 90/10 Information and communication technologies [ICT] supporting adaptation to climate change, e.g. for weather forecasting or climate simulation

Abstract

A method for determining a heading, velocity, and/or position of an aircraft includes receiving a first radar return at a radar antenna for mounting to a first wing of the aircraft and receiving a second radar return at a radar antenna mounted to a second wing of the aircraft where the first wing and the second wing extend from opposite sides of the aircraft. The method also includes determining a velocity of each wing based on the radar returns using processing electronics and calculating the heading, velocity, and/or position of the aircraft based on the determined wing velocities using the processing electronics.

Claims

1. A navigation system for use on an aircraft for determining a heading, velocity, and/or position of the aircraft, comprising:

a first radar antenna for mounting to a first wing of the aircraft and configured to receive radar returns;

a second radar antenna for mounting to a second wing of the aircraft and configured to receive radar returns, the first wing and second wing extending from opposite sides of the aircraft; and

processing electronics configured to determine a velocity of the first and second wings based on the radar returns, the processing electronics calculating the heading, velocity, and/or position of the aircraft based on the determined wing velocities.

2. The navigation system of claim 1, wherein the radar antennas are configured to be located at or near tips of the first and second wings.

3. The navigation system of claim 1, further comprising:

a global positioning device for mounting to the aircraft and configured to determine the position of the aircraft,

wherein the processing electronics determine the heading, velocity, and/or position of the aircraft based on the wing velocities and the position of the aircraft determined by the global positioning device.

4. The navigation system of claim 3, wherein the processing electronics update the heading, velocity, and/or position of the aircraft using the wing velocities at time periods between updates of the heading, velocity, and/or position based on the position of the aircraft determined by the global positioning device.

5. The navigation system of claim 3, wherein the processing electronics use the heading, velocity, and/or position of the aircraft determined from the wing velocities to override or correct the heading, velocity, and/or position of the aircraft determined from the position of the aircraft determined by the global positioning device.

6. The navigation system of claim 1, wherein the processing electronics use aircraft configuration information to determine the heading, velocity, and/or position of the aircraft.

7. The navigation system of claim 6, wherein the aircraft configuration information comprises at least one of a location of an aircraft center of gravity, a landing gear position, a position of one or both the radar antennas, and a global positioning system position.

8. The navigation system of claim 1, wherein the first and second radar antennas are also used to locate potential obstructions relative to the position of the aircraft.

9. The navigation system of claim 1, wherein the processing electronics calculate the heading of the aircraft based on a difference between the wing velocities, the processing electronics calculate the velocity of the aircraft based on a history of differences between the wing velocities, and the processing electronics calculate the position of the aircraft based on a predetermined starting point of the aircraft and a history of calculated velocities of the aircraft.

10. The navigation system of claim 1, wherein the wing velocities are velocities relative to the ground, velocities relative to each other, velocities relative to weather, velocities relative to terrain, or velocities relative to an obstacle.

11. The navigation system of claim 1, wherein the determined heading, velocity, and/or position of the aircraft is stored in a memory device and/or displayed on an electronic display.

12. The navigation system of claim 1, wherein the aircraft is taxiing or on a runway and the wing velocities are determined relative to the ground.

13. A method for determining a heading, velocity, and/or position of an aircraft, comprising:

receiving a first radar return at a radar antenna for mounting to a first wing of the aircraft;

receiving a second radar return at a radar antenna mounted to a second wing of the aircraft, the first wing and the second wing extending from opposite sides of the aircraft;

determining a velocity of each wing based on the radar returns using processing electronics; and

calculating the heading, velocity, and/or position of the aircraft based on the determined wing velocities using the processing electronics.

14. The method of claim 13, wherein the radar antennas for mounting to the first and second wings are configured to be located at or near tips of the first and second wings.

15. The method of claim 13, further comprising:

determining a position of the aircraft at a global positioning device for mounting on the aircraft,

wherein the processing electronics determine the heading, velocity, and/or position of the aircraft based on the wing velocities and based on the position of the aircraft determined by the global positioning device.

16. The method of claim 15, further comprising:

updating the heading, velocity, and/or position of the aircraft using the wing velocities at time periods between updates of the heading, velocity, and/or position based on the position of the aircraft determined by the global positioning device.

17. The method of claim 13, further comprising:

receiving an aircraft configuration at the processing electronics, the processing electronics using the aircraft configuration to determine the heading, velocity, and/or position of the aircraft,

wherein the aircraft configuration comprises at least one of a location of an aircraft center of gravity, a landing gear position, a position of one or both the radar antennas, and a global positioning system position.

18. The method of claim 17, wherein the processing electronics calculate the heading of the aircraft based on a difference between the wing velocities, the processing electronics calculate the velocity of the aircraft based on a history of differences between the wing velocities, and the processing electronics calculate the position of the aircraft based on a predetermined starting point of the aircraft and a history of calculated velocities of the aircraft.

19. The method of claim 13, wherein the wing velocities are velocities relative to the ground, to each other, to signage, to lighting structures, or to buildings.

20. An apparatus for determining a heading, velocity, and/or position of an aircraft, comprising:

means for receiving a first radar return at a first wing of the aircraft;

means for receiving a second radar return at a second wing of the aircraft, the first wing and the second wing extending from opposite sides of the aircraft;

means for determining a velocity of each wing based on the radar returns; and

means for calculating the heading, velocity, and/or position of the aircraft based on the determined wing velocities.