TRAFFIC INFORMATION SERVICES-BROADCAST (TIS-B) AUTOMATIC ADDRESS DETECTION AND COVERAGE INDICATION

• US 20140197980A1
• Filed: 01/11/2013
• Published: 07/17/2014
• Est. Priority Date: 01/11/2013
• Status: Active Grant

• Current Assignee: Garmin International, Inc. (Garmin Limited)
• Original Assignee: Garmin International, Inc. (Garmin Limited)
• Inventors: Schulte, Christopher E.P., Hartley, Timothy G.
• Granted Patent: US 9,182,484 B2
• Time in Patent Office: Days
• US Class Current: 342/37
• CPC Class Codes: G01S 13/765 with exchange of information between interrogator and responder
• CPC Class Codes: G01S 13/781 Secondary Surveillance Radar [SSR] in general
• CPC Class Codes: G01S 13/825 with exchange of information between interrogator and responder
• CPC Class Codes: G01S 13/91 for traffic control G01S13/93 takes precedence
• CPC Class Codes: G01S 13/93 for anti-collision purposes
• CPC Class Codes: G01S 13/933 of aircraft or spacecraft
• CPC Class Codes: G08G 5/0004 Transmission of traffic-related information to or from an aircraft airborne radio transmission systems in general H04B7/185; airborne wireless networks H04W84/06
• CPC Class Codes: G08G 5/0008 with other aircraft
• CPC Class Codes: G08G 5/0013 with a ground station
• CPC Class Codes: G08G 5/0021 located in the aircraft
• CPC Class Codes: G08G 5/0078 for monitoring traffic from the aircraft radar or analogous systems specially adapted for traffic control G01S13/91

Abstract

Techniques are described that allow a system, such as a portable ADS-B-enabled device, to automatically determine whether the aircraft in which the system is employed is included in air traffic information (e.g., TIS-B air traffic information) broadcast by an air traffic control (ATC) ground station. The system includes a receiver assembly to receive a first transmission from a transponder of the aircraft that includes an identification address (e.g., an ICAO address) that identifies the aircraft. The receiver assembly also receives a second transmission from the ATC ground station that includes air traffic information and a client list including identification addresses of aircraft included in the air traffic information. The identification address of the aircraft is retrieved from the first transmission and used to determine whether the aircraft is included in the air traffic information by comparing the identification address with the identification addresses in the client list.

Claims

1. A system configured for operation in an aircraft, the system comprising:

a receiver assembly operable to receive a first transmission from a transponder associated with the aircraft, the first transmission including an identification address configured to identify the aircraft, and to receive a second transmission from an air traffic control ground station, the second transmission including air traffic information and a client list including identification addresses of aircraft included in the air traffic information; and

a processing system operable to;

retrieve the identification address associated with the first transmission; and

determine whether the aircraft is included in the air traffic information by comparing the identification address of the aircraft with the identification addresses in the client list.

2. The system as recited in claim 1, further comprising a global navigation satellite system receiver operable to determine a position of the aircraft, wherein the processing system is operable to distinguish the first transmission from transmissions received from transponders of other aircraft based on the determined position of the aircraft.

3. The system as recited in claim 1, wherein the processing system is operable to distinguish the first transmission from transmissions from transponders of other aircraft by comparing a power level of the first transmission with power levels of transmission received from transponders of other aircraft.

4. The system as recited in claim 1, wherein the receiver assembly comprises a 1090 MHz receiver configured to receive a Mode S reply transmission.

5. The system as recited in claim 4, wherein the receiver assembly further comprises a 978 MHz receiver.

6. The system as recited in claim 4, wherein the processing system is further configured to determine whether the first transmission includes an indication that the aircraft is capable of receiving ADS-B information.

7. The system as recited in claim 1, wherein the transponder of the aircraft is further configured to transmit pressure altitude information for the aircraft, and wherein the receiver assembly is configured to receive the transmitted pressure altitude information for decoding by the processing system.

8. The system as recited in claim 1, wherein the first transmission comprises a Mode S transmission and the identification address comprises an ICAO address, and wherein the traffic information comprises TIS-B traffic information.

9. A method comprising:

receiving a Mode S transmission from a transponder of an aircraft, the Mode S transmission including an ICAO address configured to identify the aircraft;

retrieving the ICAO address from the Mode S transmission;

receiving a TIS-B transmission from the air traffic control ground station, the TIS-B transmission including TIS-B air traffic information and a TIS-B service status list including ICAO addresses of aircraft included in the TIS-B air traffic information;

determining whether the aircraft is included in the TIS-B air traffic information by comparing the ICAO address of the aircraft with the ICAO addresses of the TIS-B service status list; and

causing an indication of whether the aircraft is included in the air traffic information to be displayed by a portable electronic device.

10. The method as recited in claim 9, wherein the receiving of the Mode S transmission from the transponder associated with the aircraft comprises determining a position of the aircraft using a global navigation satellite system receiver and distinguishing the Mode S transmission from the transponder associated with the aircraft from Mode S transmissions received from transponders of other aircraft based on the determined position of the aircraft.

11. The method as recited in claim 10, wherein the receiving of the Mode S transmission from the transponder associated with the aircraft comprises distinguishing the Mode S transmission from the transponder associated with the aircraft from Mode S transmissions received from transponders of other aircraft by comparing a power level of the Mode S transmission of the transponder associated with the aircraft with power levels of the Mode S transmissions received from transponders of the other aircraft.

12. The method as recited in claim 11, further comprising determining whether the Mode S transmission from the transponder includes an indication that the aircraft is capable of receiving ADS-B information.

13. The method as recited in claim 11, further comprising receiving pressure altitude information for the aircraft transmitted by the transponder of the aircraft.

14. A portable ADS-B-enabled device configured for operation in an aircraft, the portable ADS-B-enabled device comprising:

a receiver assembly operable to receive a Mode S transmission from a transponder of the aircraft, the Mode S transmission including an ICAO address configured to identify the aircraft, and to receive a TIS-B transmission from the air traffic control ground station, the TIS-B transmission including TIS-B air traffic information and a TIS-B service status list including ICAO addresses of aircraft included in the TIS-B air traffic information; and

a processing system operable to;

retrieve the ICAO address of the aircraft from the Mode S transmission; and

determine whether the aircraft is included in the TIS-B air traffic information by comparing the ICAO address of the aircraft with the ICAO addresses in the TIS-B service status list.

15. The portable ADS-B-enabled device as recited in claim 14, further comprising a global navigation satellite system receiver operable to determine a position of the aircraft, wherein the processing system is operable to distinguish the Mode S transmission from the transponder associated with the aircraft from Mode S transmissions received from transponders of other aircraft based on the determined position of the aircraft.

16. The portable ADS-B-enabled device as recited in claim 14, wherein the processing system is operable to distinguish the Mode S transmission from the transponder associated with the aircraft from Mode S transmissions from transponders of other aircraft by comparing a power level of the Mode S transmission of the transponder associated with the aircraft with power levels of the Mode S transponders of the other aircraft.

17. The portable ADS-B-enabled device as recited in claim 14, wherein the receiver assembly comprises a 1090 MHz receiver configured to receive a Mode S reply transmission.

18. The portable ADS-B-enabled device as recited in claim 17, wherein the receiver assembly further comprises a 978 MHz receiver.

19. The portable ADS-B-enabled device as recited in claim 14, further comprising a communication module configured for communication with a portable electronic device, the processing system further configured to cause an indication of whether the aircraft is included in the air traffic information to be displayed by a display of the portable electronic device.

20. The portable ADS-B-enabled device as recited in claim 19, wherein the portable electronic device is integrated with at least one of the communication module, the receiver assembly, and the processing system.