Harmonizing code from independent airborne aircraft identification systems

• US 10,324,178 B2
• Filed: 12/22/2015
• Issued: 06/18/2019
• Est. Priority Date: 05/15/2012
• Status: Active Grant

• Current Assignee: L3Harris Aviation Products, Inc. (L3Harris Technologies, Inc.)
• Original Assignee: L3 Aviation Products, Inc. (L3Harris Technologies, Inc.)
• Inventors: Watson, Gary S., Carlson, Lee R., Getson, Blake R., Bundy, Matthew J., Troxel, James R.
• Primary Examiner(s): Brainard, Timothy A
• Application Number:
  US14/978,831
• Publication Number:
  US 20160109567A1
• Time in Patent Office: 1,274 Days
• Field of Search: 3423574
• CPC Class Codes: G01S 13/784 Coders or decoders therefor; Degarbling systems; Defruiting systems
• 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 13/933 of aircraft or spacecraft
• CPC Class Codes: G01S 19/03 Cooperating elements; Interaction or communication between different cooperating elements or between cooperating elements and receivers

Abstract

An Automatic Dependent Surveillance-Broadcast (ADS-B) system, and method of harmonizing a transponder Squawk code and an ADS-B system, ensures that a Squawk code broadcast by the ADS-B system matches the transponder Squawk code. The transponder Squawk code is transmitted from a transponder positioned onboard an aircraft, and the transmitted transponder Squawk code is received by a device positioned onboard the aircraft in which the transponder is installed. The ADS-B system is updated with the received transmitter squawk code. The squawk code is transmitted using the ADS-B system.

Claims

1. An Automatic Dependent Surveillance-Broadcast (ADS-B) system for positioning in an aircraft comprising:

a transponder decoder comprising an input configured to receive a mode A/C transponder transmission, a decoder decoding the mode A/C transponder transmission, and an output outputting the decoded mode A/C transponder transmission, wherein the mode A/C transponder transmission comprises a squawk code;

a message formatter configured to generate a message based on data received from the transponder decoder output, the message including data identifying the squawk code, wherein the transponder decoder and message formatter are configured to verify that the received mode A/C transponder transmission is a squawk code from the aircraft in which the ADS-B system is installed; and

a wireless transmitter in communication with the message formatter, wherein the wireless transmitter wirelessly broadcasts the message.

2. The ADS-B system of claim 1, wherein the transponder decoder receives the squawk code wirelessly from the transponder.

3. The ADS-B system of claim 1, wherein the transponder decoder also receives altitude information broadcast from the transponder and forwards the altitude information to the message formatter for formatting into the message.

4. The ADS-B system of claim 1, wherein the message formatter verifies that a transponder transmission is a squawk code by determining that the transponder transmission has a value that is not the same value as altitude information for the aircraft.

5. The ADS-B system of claim 1, wherein the transponder decoder verifies that a received transponder transmission is a transponder transmission from the aircraft in which the ADS-B system is installed by analyzing a signal strength of the received transponder transmission, wherein the received transponder transmission is from the aircraft in which the ADS-B system is installed when the signal strength of the received transponder is above a threshold.

6. The ADS-B system of claim 1, wherein the message formatter causes an alternative action if the message formatter cannot verify that the transponder transmission is a squawk code.

7. The ADS-B system of claim 6, wherein the alternative action comprises at least one chosen from (i) providing an indication to a pilot and (ii) sending an interrogation signal to activate the transponder to send a transmission.

8. The ADS-B system of claim 1, wherein the ADS-B system sends an interrogation signal to activate the transponder to send a squawk code.

9. The ADS-B system of claim 8, wherein the wireless transmitter sends the interrogation signal to the transponder.

10. The ADS-B system of claim 8, wherein the interrogation signal is transmitted at an attenuated level.

11. The ADS-B system of claim 1, wherein the message formatter determines that the transponder is not transmitting.

12. The ADS-B system of claim 11, wherein the message formatter distinguishes between the transponder not transmitting because the transponder is not operational and because the transponder is not being interrogated.

13. The ADS-B system of claim 12, wherein the message formatter notifies the pilot.

14. The ADS-B system of claim 1 further comprising a transponder suppression bus input to be coupled to a transponder suppression bus within the aircraft in which the ADS-B system is installed, wherein the transponder suppression bus input responses to a signal when data is transmitted by the transponder onboard the aircraft to distinguish from data transmitted by any transponders off-board the aircraft.

15. The ADS-B system of claim 1, wherein the transponder decoder also receives IDENT information broadcast from the transponder and forwards the IDENT information to the message formatter to be formatted into the message.

16. The ADS-B system of claim 1, wherein the wireless transmitter is a component of a Universal Access Transceiver (UAT).

17. An Automatic Dependent Surveillance-Broadcast (ADS-B) system for positioning in an aircraft comprising:

a transponder decoder comprising an input receiving a mode A/C transponder transmission from a transponder positioned in the aircraft in which the ADS-B system is positioned, a decoder decoding the mode A/C transponder transmission, and an output outputting the decoded mode A/C transponder transmission,

a first transmitter sending an interrogation signal to activate the transponder positioned aboard the aircraft to send the received mode A/C transponder transmissions; and

a second transmitter coupled to the transponder decoder output and configured to wirelessly broadcast the decoded mode A/C transponder transmission data;

wherein the second transmitter and the first transmitter are a combined transmitter that transmits at a lower power level when transmitting the interrogation signal than when transmitting the mode A/C transponder transmission.

18. The ADS-B system of claim 17, wherein the transponder decoder input comprises an antenna to wirelessly detect the mode A/C transponder transmission.

19. The ADS-B system of claim 17, wherein the decoded mode A/C transponder transmission is wirelessly broadcast using a Universal Access Transceiver (UAT).

20. The ADS-B system of claim 17 further comprising a message formatter to verify that a received transponder transmission is a squawk code.

21. The ADS-B system of claim 20, wherein the message formatter verifies that a received transponder transmission is a squawk code by determining that the received transponder transmission does not have a same value as pressure altitude information for the aircraft.

22. The ADS-B system of claim 20, wherein the first transmitter sends the interrogation signal to activate the transponder if the message formatter cannot verify that the received transponder transmission is a squawk code.

23. The ADS-B system of claim 20, wherein the message formatter determines that the transponder is not transmitting.

24. The ADS-B system of claim 23, wherein the message formatter distinguishes between the transponder not transmitting because the transponder is not operational and not transmitting, and because the transponder is not being interrogated.

25. The ADS-B system of claim 24, wherein the message formatter notifies the pilot.

26. The ADS-B system of claim 18, wherein the antenna sends the interrogation signal to the transponder.

27. An Automatic Dependent Surveillance-Broadcast (ADS-B) system for positioning in an aircraft having a transponder comprising:

a transponder decoder comprising a directional coupler receiving a transponder transmission via at least one antenna, a decoder decoding the transponder transmission, and an output outputting the decoded transponder transmission, wherein the transponder transmission comprises a squawk code;

a logic device generating a message based on data received from the transponder decoder output, the message including data identifying the squawk code, wherein the transponder transmission is received in response to transmitting an interrogation signal from the logic device via the at least one antenna, wherein the transponder decoder and the logic device are configured to verify the received transponder transmission is a squawk code from the aircraft in which the ADS-B is installed; and

a wireless transmitter in communication with the logic device, wherein the wireless transmitter wirelessly broadcasts the message via the directional coupler and the at least one antenna.

28. The ADS-B system of claim 27, wherein the at least one antenna comprises a first antenna for receiving the transponder transmission and for transmitting the message;

and a second antenna for transmitting the interrogation signal.

29. The ADS-B system of claim 27, wherein the at least one antenna is a single antenna.

30. The ADS-B system of claim 29, wherein the directional coupler provides an attenuated path to the logic device.

31. The ADS-B system of claim 30, wherein the decoder receives the transponder transmission via the attenuated path of the directional coupler, and wherein the decoder comprises a detector eliminating a carrier signal of the transponder transmission to produce a digital pulse stream as the decoded transponder transmission.

32. The ADS-B system of claim 27, wherein the directional coupler provides a low-loss path to the wireless transmitter, wherein the wireless transmitter transmissions take place at 978 MHz.

33. The ADS-B system of claim 27, wherein the interrogation signal is transmitted at an attenuated level.

34. The ADS-B system of claim 27, wherein the interrogation signal comprises 970 MHz and 1030 MHz modulated pulses.

35. The ADS-B system of claim 27, wherein the message is wirelessly broadcast using a Universal Access Transceiver (UAT).

36. The ADS-B system of claim 27, wherein the transponder transmission comprises 1090 MHz modulated pulses.

37. A method of automatically harmonizing a transponder squawk code and an Automatic Dependent Surveillance-Broadcast (ADS-B) system such that a squawk code broadcast by the ADS-B system matches the transponder squawk code, the method comprising:

transmitting the transponder squawk code from a transponder positioned onboard an aircraft in which the ADS-B system is installed;

receiving, with the ADS-B system, transponder squawk codes that include the transmitted transponder squawk code transmitted by the transponder;

verifying that the received transponder squawk code is a squawk code from the transponder positioned onboard the aircraft;

updating the ADS-B system with the received transponder squawk code; and

broadcasting, with the ADS-B system, the squawk code.

38. The method of claim 37, wherein the receiving the transmitted transponder squawk code is performed wirelessly using an antenna of the ADS-B system.

39. The method of claim 37 further comprising receiving a signal from a transponder suppression bus, wherein the transponder suppression bus input receives a signal when data is transmitted by the transponder onboard the aircraft to distinguish from data transmitted by any transponders off-board the aircraft.

40. The method of claim 37 further comprising receiving altitude information broadcast from the transponder positioned onboard the aircraft.

41. The method of claim 40 further comprising determining that a transponder transmission is a squawk code by determining that the transponder transmission has a value that is not the same value as the received altitude information for the aircraft.

42. The method of claim 41 further comprising taking alternative action if it cannot be determined that the transponder transmission is a squawk code.

43. The method of claim 42, wherein the alternative action is chosen from (i) providing an indication to a pilot and (ii) sending an interrogation signal to activate the transponder to send a transmission.

44. The method of claim 41 further comprising determining that the transponder is not transmitting.

45. The method of claim 44, wherein the determining that the transponder is not transmitting comprises distinguishing between the transponder not transmitting because the transponder is not operational and because the transponder is not being interrogated.

46. The method of claim 37 further comprising sending an interrogation signal with an antenna of the ADS-B system to activate the transponder to send the squawk code.