METHOD AND APPARATUS FOR MONITORING COMPLIANCE WITH A NON-TRANSGRESSION ZONE BETWEEN AIRCRAFT APPROACH CORRIDORS

• US 20170084182A1
• Filed: 09/18/2015
• Published: 03/23/2017
• Est. Priority Date: 09/18/2015
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Conway, Sheila R.
• Granted Patent: US 9,818,305 B2
• Time in Patent Office: Days
• CPC Class Codes: G08G 5/0013 with a ground station
• CPC Class Codes: G08G 5/0026 located on the ground
• CPC Class Codes: G08G 5/0043 Traffic management of multiple aircrafts from the ground G08G5/003 takes precedence; data processing specially designed for resource management, e.g. scheduling or allocating time, human or machine resources G06Q10/06
• CPC Class Codes: G08G 5/0082 for monitoring traffic from a ground station radar or analogous systems specially adapted for traffic control G01S13/91
• CPC Class Codes: G08G 5/02 Automatic approach or landing aids, i.e. systems in which flight data of incoming planes are processed to provide landing data landing aids fitted in or to aircraft B64D45/04; visual or acoustic landing aids B64F1/18
• CPC Class Codes: G08G 5/025 Navigation or guidance aids radar or analogous systems specially adapted for landing purposes G01S13/913

Abstract

A method, computing system and computer program product are provided to monitor compliance with a non-transgression zone between aircraft approach corridors, thereby facilitating simultaneous instrument approaches. In the context of a method, a predicted path of an aircraft is determined during a flight based upon at least a representation of a roll angle of the aircraft and a cross-track component of the velocity of the aircraft. The method also includes identifying an instance in which the predicted path of the aircraft during the flight intersects a non-transgression zone. The method further includes causing an alert to be issued in the instance in which the predicted path of the aircraft during the flight intersects the non-transgression zone.

Claims

1. A method for monitoring compliance with a non-transgression zone between aircraft approach corridors, the method comprising:

determining, with processing circuitry, a predicted path of an aircraft during a flight based upon at least a representation of a roll angle of the aircraft and a cross-track component of velocity of the aircraft;

identifying an instance in which the predicted path of the aircraft during the flight intersects the non-transgression zone; and

causing an alert to be issued in the instance in which the predicted path of the aircraft during the flight intersects the non-transgression zone.

2. A method according to claim 1 wherein determining the predicted path of the aircraft comprises determining the representation of the roll angle of the aircraft in real time, and wherein causing the alert to be issued comprises causing the alert to be issued in real time.

3. A method according to claim 1 wherein determining the predicted path is further based upon a current position and heading of the aircraft.

4. A method according to claim 1 wherein determining the predicted path comprises determining a turn rate and a turn radius based upon at least the representation of the roll angle of the aircraft and the cross-track component of the velocity of the aircraft.

5. A method according to claim 1 further comprising receiving the representation of the roll angle of the aircraft and the cross-track component of the velocity of the aircraft from at least one of an Enhanced Surveillance (EHS) surveillance transponder or from an Automatic Dependent Surveillance Broadcast (ADS-B) message.

6. A method according to claim 1 wherein identifying an instance in which the predicted path of the aircraft intersects the non-transgression zone comprises determining, prior to the aircraft reaching a largest cross track position error, whether corrective action has been initiated by the aircraft to avoid intersection with the non-transgression zone.

7. A method according to claim 1 wherein the predicted path of the aircraft is determined by the processing circuitry which is embodied by an air traffic control ground station, by an air traffic control radar system or as an auxiliary function to a display of the air traffic control radar system.

8. A computing system for monitoring compliance with a non-transgression zone between aircraft approach corridors, the computing system comprising processing circuitry configured to:

determine a predicted path of an aircraft during a flight based upon at least a representation of a roll angle of the aircraft and a cross-track component of velocity of the aircraft;

identify an instance in which the predicted path of the aircraft during the flight intersects the non-transgression zone; and

cause an alert to be issued in the instance in which the predicted path of the aircraft during the flight intersects the non-transgression zone.

9. A computing system according to claim 8 wherein the processing circuitry is configured to determine the predicted path of the aircraft by determining the representation of the roll angle of the aircraft in real time, and wherein the processing circuitry is configured to cause the alert to be issued by causing the alert to be issued in real time.

10. A computing system according to claim 8 wherein the processing circuitry is configured to determine the predicted path based further upon a current position and heading of the aircraft.

11. A computing system according to claim 8 wherein the processing circuitry is configured to determine the predicted path by determining a turn rate and a turn radius based upon at least the representation of the roll angle of the aircraft and the cross-track component of the velocity of the aircraft.

12. A computing system according to claim 8 wherein the processing circuitry is further configured to receive the representation of the roll angle of the aircraft and the cross-track component of the velocity of the aircraft from at least one of an Enhanced Surveillance (EHS) surveillance transponder or from an Automatic Dependent Surveillance Broadcast (ADS-B) message.

13. A computing system according to claim 8 wherein the processing circuitry is configured to identify an instance in which the predicted path of the aircraft intersects the non-transgression zone by determining, prior to the aircraft reaching a largest cross track position error, whether corrective action has been initiated by the aircraft to avoid intersection with the non-transgression zone.

14. A computing system according to claim 8 wherein the processing circuitry is embodied by an air traffic control ground station, by an air traffic control radar system or as an auxiliary function to a display of the air traffic control radar system.

15. A computer program product for monitoring compliance with a non-transgression zone between aircraft approach corridors, the computer program product comprising at least one non-transitory computer-readable storage medium having computer-executable program code instructions stored therein, the computer-executable program code instructions comprising program code instructions configured to:

determine a predicted path of an aircraft during a flight based upon at least a representation of a roll angle of the aircraft and a cross-track component of velocity of the aircraft;

identify an instance in which the predicted path of the aircraft during the flight intersects the non-transgression zone; and

cause an alert to be issued in the instance in which the predicted path of the aircraft during the flight intersects the non-transgression zone.

16. A computer program product according to claim 15 wherein the program code instructions configured to determine the predicted path of the aircraft comprise program code instructions configured to determine the representation of the roll angle of the aircraft in real time, and wherein the program code instructions configured to cause the alert to be issued comprise program code instructions configured to cause the alert to be issued in real time.

17. A computer program product according to claim 15 wherein the program code instructions configured to determine the predicted path are further based upon a current position and heading of the aircraft.

18. A computer program product according to claim 15 wherein the program code instructions configured to determine the predicted path comprise program code instructions configured to determine a turn rate and a turn radius based upon at least the representation of the roll angle of the aircraft and the cross-track component of the velocity of the aircraft.

19. A computer program product according to claim 15 wherein the computer-executable program code instructions further comprise program code instructions configured to receive the representation of the roll angle of the aircraft and the cross-track component of the velocity of the aircraft from at least one of an Enhanced Surveillance (EHS) surveillance transponder or from an Automatic Dependent Surveillance Broadcast (ADS-B) message.

20. A computer program product according to claim 15 wherein the program code instructions configured to identify an instance in which the predicted path of the aircraft intersects the non-transgression zone comprise program code instructions configured to determine, prior to the aircraft reaching a largest cross track position error, whether corrective action has been initiated by the aircraft to avoid intersection with the non-transgression zone.