Systems and methods for determining bearing

• US 20060009909A1
• Filed: 07/12/2004
• Published: 01/12/2006
• Est. Priority Date: 07/12/2004
• Status: Active Grant

• Current Assignee: L3 Technologies, Inc. (L3Harris Technologies, Inc.)
• Original Assignee: Aviation Communication and Surveillance Systems LLC (L3Harris Technologies, Inc.)
• Inventors: Smith, Mark Dean
• Granted Patent: US 8,798,911 B2
• Time in Patent Office: Days
• US Class Current: 701/301
• CPC Class Codes: G01S 13/4454 phase comparisons monopulse, i.e. comparing the echo signals received by an interferometric antenna arrangement
• CPC Class Codes: G01S 13/765 with exchange of information between interrogator and responder
• CPC Class Codes: G01S 13/86 Combinations of radar systems with non-radar systems, e.g. sonar, direction finder
• CPC Class Codes: G01S 13/933 of aircraft or spacecraft
• CPC Class Codes: G01S 3/023 Monitoring or calibrating
• CPC Class Codes: G08G 5/0008 with other aircraft

Abstract

A system determines bearing for situational awareness. The system may include a receiver, a processor, and a memory comprising an engine for performing a method. The method includes receiving signals using directional reception; receiving positional data; calculating a correction amount; and applying the correction amount to subsequent uncorrected bearings to provide corrected bearings. Positional data may be received in any conventional format including data link, ADS-B, and MODE S. Positional data may be determined in the target using a global positioning system. The system may provide a signal to display the corrected bearing and/or provide traffic alerting and collision avoidance advisories.

Claims

1. A method for determining corrected bearings, the method comprising:

a step for determining a first uncorrected bearing in accordance with signals received using directional reception;

a step for calculating a correction amount in accordance with the first uncorrected bearing and received positional data; and

a step for applying the correction amount to subsequently determined uncorrected bearings to provide the corrected bearings.

2. A system for determining corrected bearings, the system comprising:

means for determining a first uncorrected bearing in accordance with signals received using directional reception;

means for calculating a correction amount in accordance with the first uncorrected bearing and received positional data; and

means for applying the correction amount to subsequently determined uncorrected bearings to provide the corrected bearings.

3. A method for situational awareness performed by a system aboard a host vehicle, the method comprising in sequence:

a step for determining a first uncorrected bearing in accordance with a first signal and a direction, the first signal associated with a first target relative to the host vehicle, the first signal in further accordance with directional reception from the direction;

a step for determining a correct-bearing in accordance with received positional data, the data being in accordance with the direction;

a step for determining a correction amount in accordance with the first uncorrected bearing and the correct bearing;

a step for determining a second uncorrected bearing in accordance with a second signal, the second signal associated with a second target relative to the host vehicle, the second signal in further accordance with directional reception from the direction; and

a step for determining a corrected bearing in accordance with the second uncorrected bearing, the correction amount, and the direction.

4. The method of claim 3 wherein:

the method further comprises a step for storing the correction amount in accordance with the direction; and

the step for determining a corrected bearing comprises a step for recalling the correction amount in accordance with the direction.

5. The method of claim 3 wherein the positional data is received from the first target.

6. The method of claim 3 wherein the positional data comprises an ADS-B format.

7. The method of claim 4 wherein recalling the correction amount comprises a step for performing a binary tree search algorithm.

8. The method of claim 3 wherein the method further comprises a step for using the corrected bearing for at least one of traffic alerting and collision avoidance.

9. The method of claim 3 further comprising a step for providing, in accordance with the corrected bearing, a signal for a display.

10. The method of claim 3 wherein the step for determining a correction amount comprises a step for determining an average of a plurality of stored first uncorrected bearings.

11. The method of claim 3 wherein the step for determining the corrected bearing comprises a step for combining the second uncorrected bearing and the correction amount.

12. The method of claim 11 wherein the step for combining comprises a step for computing a sum that includes the correction amount.

13. The method of claim 11 wherein the step for combining comprises a step for computing at least one of a product that includes the correction amount and a quotient that includes the correction amount.

14. The method of claim 3 wherein the host and a second aircraft are members of a formation and the positional data is received from the second aircraft.

27. A memory device comprising instructions for performing the method of any of claims 3 through 26.

28. A system for situational awareness, the system comprising:

a receiver that provides the first signal and the second signal;

a processor coupled to the receiver; and

a memory device, coupled to the processor, comprising instructions for the processor to perform the method of any of claims 3 through 26.

15. A method for situational awareness performed by a system aboard a host vehicle, the method comprising:

a step for determining a first uncorrected bearing in accordance with a first signal and a direction, the first signal associated with a first target relative to the host vehicle, the first signal in further accordance with directional reception from the direction;

a step for determining a first elevation of the first target relative to the host vehicle;

a step for determining a correct bearing in accordance with received positional data, the data being in accordance with the direction and the first elevation;

a step for determining a correction amount in accordance with the first uncorrected bearing and the correct bearing;

a step for determining a second uncorrected bearing in accordance with a second signal, the second signal associated with a second target relative to the host vehicle, the second signal in further accordance with directional reception from the direction;

a step for determining a second elevation of the second target; and

a step for determining a corrected bearing in accordance with the second uncorrected bearing, the correction amount, the direction, and the second elevation.

16. The method of claim 15 wherein:

the method further comprises a step for storing the correction amount in accordance with the direction and the first elevation; and

the step for determining a corrected bearing comprises a step for recalling the correction amount in accordance with the direction and the second elevation.

17. The method of claim 15 wherein the positional data is received from the first target.

18. The method of claim 15 wherein the positional data comprises an ADS-B format.

19. The method of claim 16 wherein the step for recalling the correction amount comprises a step for performing a binary tree search algorithm.

20. The method of claim 15 wherein the method further comprises a step for using the corrected bearing for at least one of traffic alerting and collision avoidance.

21. The method of claim 15 further comprising a step for providing, in accordance with the corrected bearing, a signal for a display.

22. The method of claim 15 wherein the step for determining a correction amount comprises a step for determining an average of a plurality of stored first uncorrected bearings.

23. The method of claim 15 wherein the step for determining the corrected bearing comprises a step for combining the second uncorrected bearing and the correction amount.

24. The method of claim 23 wherein the step for combining comprises a step for calculating a sum that includes the correction amount.

25. The method of claim 23 wherein the step for combining comprises a step for computing at least one of a product that includes the correction amount and a quotient that includes the correction amount.

26. The method of claim 15 wherein the host and a second aircraft are members of a formation and the positional data is received from the second aircraft.