METHOD AND SYSTEM FOR DETECTING AND DECODING AIR TRAFFIC CONTROL REPLY SIGNALS

• US 20080055150A1
• Filed: 09/06/2006
• Published: 03/06/2008
• Est. Priority Date: 09/06/2006
• Status: Abandoned Application

• Current Assignee: Garmin International, Inc. (Garmin Limited)
• Original Assignee: Garmin International, Inc. (Garmin Limited)
• Inventors: Needham, Edward W., Hou, Weiguang
• Application Number:
  US11/470,532
• Publication Number:
  US 20080055150A1
• Time in Patent Office: Days
• US Class Current: 342/40
• CPC Class Codes: G01S 13/782 using multimoding or selective addressing
• CPC Class Codes: G01S 13/784 Coders or decoders therefor; Degarbling systems; Defruiting systems

Abstract

A method and system are provided for detecting an edge of a received signal associated with air traffic control communications. The system includes an A/D converter to convert a received signal to a series of digital data samples and an edge detector module to determine a change rate between the data samples. The change rate represents a change in amplitude between the data samples per unit of time. The edge detector module validates an edge of the received signal based on the change rate between the data samples. A decoder module may derive timing information from the leading/trailing edge pulses and associates the reply message with the framing pulse based on the timing information.

Claims

1. A system for detecting an edge of a received signal associated with air traffic control communications, the system comprising:

an A/D converter to convert a received signal to a series of digital data samples; and

an edge detector module to determine a change rate between the data samples, the edge detector module validating an edge of the received signal based on the change rate between the data samples.

2. The system of claim 1, wherein the edge detector module determines a change rate based on changes in amplitudes of immediately adjacent consecutive data samples and compares the change rate to a change rate threshold.

3. The system of claim 1, wherein the edge detector module determines the change rate based on changes in amplitudes of data samples that are separated from one another by at least one data sample.

4. The system of claim 1, wherein the edge detector module determines a series of the change rates and validates the edge of the received signal when multiple change rates satisfy a detection criteria.

5. The system of claim 1, further comprising a pulse width module for comparing a pulse width of the received signal with a pulse width criteria, wherein a valid edge output is produced when the edge detector module validates the edge of the received signal and the pulse width module determines that the pulse width of the received signal satisfies the pulse width criteria.

6. A method for detecting an edge of a received signal associated with air traffic control communications, the method comprising:

converting a received signal to a series of digital data samples; and

determining a change rate between the data samples;

validating an edge of the received signal based on the change rate between the data samples.

7. The method of claim 6, wherein the determining includes determining a change rate based on changes in amplitudes of immediately adjacent consecutive data samples and compares the change rate to a change rate threshold.

8. The method of claim 6, wherein the determining includes determining the change rate based on changes in amplitudes of data samples that are separated from one another by at least one data sample.

9. The method of claim 6, wherein the determining includes determining a series of the change rates and the validating includes validating the edge of the received signal when multiple consecutive of the change rates satisfy a detection criteria.

10. The method of claim 6, further comprising:

comparing a pulse width of the received signal with a pulse width criteria; and

producing a valid edge output when the edge of the received signal is validated and the pulse width of the received signal satisfies the pulse width criteria.

11. A system for decoding received signals associated with an air traffic control communication, the system comprising:

an A/D converter to convert received signals to a series of digital data samples, the data samples defining reply and framing pulses; and

an edge detector module to detect edges of the reply and framing pulses and, in response thereto, outputting leading edge pulses; and

a decoder deriving timing information from the leading/trailing edge pulses, the decoder associating a reply message with the framing pulses based on the timing information.

12. The system of claim 11, wherein the decoder includes timer counters that are initiated upon receipt of a leading edge pulse of a potential framing pulse, the decoder module determining whether a potential reply message pulse is an actual reply message pulse associated with the potential framing pulse based on a time interval between a leading edge pulses of the potential framing pulse and a leading edge pulse of the potential reply message.

13. The system of claim 11, wherein the decoder includes multiple decoder modules joined in parallel with the edge detector module, each decoder module being assigned to separate overlapping reply messages based upon leading edge pulses of the potential reply messages such that each decoder module tracks reply message pulses and framing pulses within only a single one of the overlapping reply messages.

14. The system of claim 11, wherein the decoder includes a confidence determination module to produce confidence information representing a level of confidence that a reply message is valid.

16. A method for decoding received signals associated with an air traffic control communication, the method comprising:

converting received signals to a series of digital data samples, the data samples defining reply and framing pulses; and

detecting edges of reply messages pulses and framing pulses and, in response thereto, outputting leading/trailing edge pulses; and

deriving timing information from the leading/trailing edge pulses and associating each reply message pulse with an appropriate one of the framing pulse based on the timing information.

17. The method of claim 16, wherein the decoding includes initiating counters upon receipt of a leading edge pulse of a potential framing pulse, and determining whether a potential reply message pulse is an actual reply message pulse associated with the potential framing pulse based on a time interval between a leading edge pulse of the potential framing pulse and a leading edge pulse of the potential reply message.

18. The method of claim 16, further comprising joining multiple decoder modules in parallel, and assigning the decoder modules to separate overlapping reply messages based upon leading edge pulses of the overlapping reply messages such that each decoder module tracks reply message pulses and framing pulses within only a single one of the overlapping reply messages.

19. The method of claim 16, further comprising joining multiple decoder modules in parallel, and activating each of the decoder modules in connection with separate and unique reply messages.

20. The method of claim 16, further comprising producing confidence information representing a level of confidence that a reply message is valid.