Airport runway collision avoidance system and method

• US 7,479,925 B2
• Filed: 03/23/2005
• Issued: 01/20/2009
• Est. Priority Date: 03/23/2005
• Status: Active Grant

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Schell, Ethan T.
• Primary Examiner(s): Tarcza; Thomas H
• Assistant Examiner(s): Liu; Harry
• Application Number:
  US10/907,172
• Publication Number:
  US 20060214816A1
• Time in Patent Office: 1,399 Days
• Field of Search: 342/455, 342/30, 701/301, 701/16, 340/961, 340/970
• US Class Current: 342/455
• CPC Class Codes: G01S 13/933 of aircraft or spacecraft
• CPC Class Codes: G01S 19/15 Aircraft landing systems
• CPC Class Codes: G08G 5/0008 with other aircraft
• CPC Class Codes: G08G 5/0078 for monitoring traffic from the aircraft radar or analogous systems specially adapted for traffic control G01S13/91
• CPC Class Codes: G08G 5/065 Navigation or guidance aids, e.g. for taxiing or rolling

Abstract

Systems and methods for avoiding runway collisions. In a disclosed embodiment of the invention, a collision avoidance system includes a position-sensing device that is operable to determine a position of the aircraft, and a communications system operable to support two-way communications between the aircraft and other similarly configured aircraft. A collision avoidance processor is coupled to the position-sensing device and the communications system that is configured to generate a message if the aircraft moves into a restricted zone positioned proximate to the airport.

Claims

1. A collision avoidance system for an aircraft, the system comprising:

a position-sensing device operable to determine a position of the aircraft;

a communications system operable to support two-way communications between the aircraft and other aircraft; and

a collision avoidance processor in communication with the position-sensing device and the communications system, the processor being configured to generate an advisory signal if the aircraft is determined to be positioned in a predefined first restricted zone positioned proximate to an airport runway and transmit the generated advisory signal to other similarly configured aircraft via the communications system thereby informing the other aircraft that a current instrument landing system (ILS) landing process may be affected,

wherein the generated signal includes the determined positional information for the aircraft,

wherein the collision avoidance processor receives signals emitted from another aircraft configured to emit signals when the other aircraft is positioned in a second restricted zone, wherein the transmitted signals include the determined positional information for the other aircraft, the collision avoidance processor compares positional information for the other aircraft to the determined positional information for the aircraft, determines if a collision hazard exists based on the comparison, and outputs an alert if it is determined that a collision hazard exists, the determined position information includes previously stored airport information, and the airport information includes at least one of runway information, taxiway information and approach to landing information.

2. The system of claim 1, wherein the position-sensing device comprises a global positioning system (GPS) receiver.

3. The system of claim 2, wherein the position-sensing device is configured to receive navigational and flight plan data is from a flight management computer (FMC).

4. The system of claim 1, wherein the position-sensing device comprises an altitude-sensing device.

5. The system of claim 4, wherein the altitude-sensing device comprises at least one of a pitot-static system and a radio altimeter system.

6. The system of claim 1, further comprising an air-ground logic device coupled with the collision avoidance processor, the air-ground logic device being configured to determine an air-ground state for the aircraft.

7. The system of claim 6, wherein the air-ground logic device comprises at least one of an air-ground logic system that is coupled to a landing gear system of the aircraft, and a radio altimeter system.

17. The system of claim 1, wherein the collision avoidance processor is further configured to generate a landing abort signal if the aircraft is determined to be positioned in a predefined third restricted zone positioned proximate to the airport runway and configured to transmit the generated landing abort signal to the other aircraft so the other aircraft is informed that a current landing process should be aborted.

18. The system of claim 1, wherein the second restricted zone corresponds to a portion of the airport runway on which the other aircraft has landed.

19. The system of claim 1, wherein the aircraft in taxing to the airport runway when in the first restricted zone, and wherein the first restricted zone is an approach zone of the airport runway.

8. A method of collision avoidance for an aircraft, the method comprising

determining position information for the aircraft;

determining if the aircraft is within a first restricted zone proximate to an airport runway based on the position information for the aircraft;

if the aircraft is determined to be within the first restricted zone, transmitting an advisory signal to at least one other aircraft approaching for landing during an instrument landing system (ILS) landing process on the airport runway thereby informing the other aircraft that a current ILS landing process may be affected; and

monitoring for signals emitted from the other aircraft configured to emit signals when positioned in a second restricted zone,

wherein the transmitted signals include the determined position information for the aircraft,

wherein the collision avoidance processor receives signals emitted from the other aircraft configured to emit signals when the other aircraft is positioned in the second restricted zone, wherein the transmitted signals include the determined positional information for the aircraft and the received signals include the determined positional information for the other aircraft, the collision avoidance processor compares positional information for the other aircraft to the determined positional information for the aircraft, determines if a collision hazard exists based on the comparison, and outputs an alert if it is determined that a collision hazard exists, the determined position information includes previously stored airport information, and the airport information includes at least one of runway information, taxiway information and approach to landing information.

9. The method of claim 8, wherein determining position information further comprises receiving position information from a global positioning system (GPS).

10. The method of claim 8, wherein determining position information further comprises periodically updating the position of the aircraft relative to the airport area.

11. The method of claim 8, wherein determining position information further comprises determining an altitude for the aircraft.

12. The method of claim 8, wherein determining if the aircraft is within a restricted zone further comprises detecting if the aircraft is moved across one of a hold short line, a hold short approach line and an ILS hold line adjacent to a runway.

13. The method of claim 8, wherein determining if the aircraft is within a restricted zone further comprises detecting if the aircraft enters an approach zone proximate to the airport.

14. The method of claim 8, wherein determining if the aircraft is within a restricted zone further comprises detecting if the aircraft is on the ground.

15. The method of claim 8, wherein monitoring for signals comprises generating an audible warning message if a signal emitted from another vehicle is received.

16. The method of claim 8, wherein monitoring for signals comprises generating a visual warning message if a signal emitted from another vehicle is received.

20. The method of claim 8, further comprising:

determining if the aircraft is within a third restricted zone proximate to an airport runway based on the position information for the aircraft; and

if the aircraft is determined to be within the third restricted zone, transmitting a landing abort signal to the other aircraft approaching for landing on the airport runway so the other aircraft is informed that a current landing process should be aborted.