Civil aviation passive coherent location system and method

• US 20020053982A1
• Filed: 10/22/2001
• Published: 05/09/2002
• Est. Priority Date: 10/20/2000
• Status: Active Grant

• Current Assignee: Leidos Innovations Technology, Inc.
• Original Assignee: Lockheed Martin Integrated Systems Incorporated (Martin Marietta Corporation)
• Inventors: Benner, Robert, Lodwig, Richard, Baugh, Kevin W.
• Granted Patent: US 7,012,552 B2
• Time in Patent Office: Days
• US Class Current: 340/945
• CPC Class Codes: G01S 13/003 Bistatic radar systems; Multistatic radar systems
• CPC Class Codes: G01S 13/933 of aircraft or spacecraft
• CPC Class Codes: G01S 5/12 by co-ordinating position lines of different shape, e.g. hyperbolic, circular, elliptical or radial

Abstract

A civil aviation passive coherent location system and method is disclosed. A receiver subsystem receives reference transmissions from an uncontrolled transmitter. The receiver subsystem also receives scattered transmissions originating from the uncontrolled transmitter and scattered by an airborne object. The received transmissions are compared to determine measurement differentials, such a frequency-difference-of-arrival, a time-difference-of-arrival and an angle of arrival. From the measurement differentials, an object state estimate is determined. A previous state estimate may be updated with the determined state estimate. Processing subsystems determine the measurement differentials and state estimates.

Claims

1. A system for enhancing object state awareness to track a plurality of approaching airborne objects, comprising:

a receiver subsystem to receive reference signals from an uncontrolled transmitter and scattered transmissions originating from the uncontrolled transmitter and scattered by an object of said plurality of approaching airborne objects;

a front-end processing subsystem to determine a radial velocity of the object based on the received transmissions; and

a back-end processing subsystem to determine object state estimates based on the determined radial velocity.

2. The system of claim 1, wherein said scattered transmissions comprise ambient transmissions.

3. The system of claim 1, further comprising initial position information for said object, wherein said initial position information is communicated with said reference signals.

4. The system of claim 1, further comprising an output device to display said object state estimates.

5. The system of claim 1, further comprising a communication link to couple said receiver subsystem, said front-end processing subsystem and said back-end processing subsystem.

6. A passive coherent location system for monitoring a predetermined location within airspace, comprising:

a receiver subsystem to receive scattered transmissions scattered by an object within said airspace and to output digitized signals of said scattered transmissions said scattered transmissions originating from an uncontrolled transmitter;

a front-end processing subsystem to determine a frequency-difference-of-arrival for said digitized signals; and

a back-end processing subsystem to determine positional information for said object in accordance with said frequency-difference-of-arrival.

7. The system of claim 6, further comprising an output device to provide said positional information for said object.

8. The system of claim 6, further comprising a reference signal from said uncontrolled transmitter, said reference signal being used to determine said frequency-difference-of-arrival for said digitized signals.

9. The system of claim 6, further comprising a radial velocity calculation of said object determined from said frequency-difference-of-arrival.

10. The system of claim 6, further comprising an antenna subsystem to detect said scattered transmissions.

11. The system of claim 10, wherein said antenna subsystem comprises a phased array antenna.

12. The system of claim 6, wherein said receiver subsystem comprises an ultrahigh dynamic range receiver.

13. The system of claim 6, further comprising a communication link between said front-end processing subsystem and said back-end processing subsystem.

15. The method of claim 14, further comprising determining an initial state estimate for said object.

16. The method of claim 14, further comprising selecting said uncontrolled transmitter from a plurality of transmitters.

17. The method of claim 14, further comprising determining whether said object is moving.

18. The method of claim 14, further comprising outputting said updated state estimate.

19. The method of claim 14, further comprising terminating said receiving when said object is out-of-range.

20. The method of claim 14, wherein said warning is issued to an air traffic control system.

21. The method of claim 14, wherein said warning is issued to a pilot.

14. A method for determining an updated state estimate for an object, comprising:

receiving a reference transmission from an uncontrolled transmitter and a scattered transmission that originated from said uncontrolled transmitter and that was scattered by the object;

comparing the received transmissions to determine a measurement differential;

updating a previous state estimate based on the determined measurement differential; and

issuing a warning when said object is within a predetermined distance from a ground location.

22. A method for determining an updated state estimate for an object, comprising:

receiving a reference transmission from an uncontrolled transmitter and a scattered transmission that originated from said uncontrolled transmitter and was scattered by the object;

comparing the received transmissions to determine a measurement differential;

updating a previous state estimate based on the measurement differential; and

issuing a warning when said object undertakes an airpath, wherein said airpath intersects with another object.

24. The method of claim 23, further comprising outputting said updated object state estimate.

25. The method of claim 23, wherein said measurement differentials include a frequency-difference-of-arrival.

26. The method of claim 23, wherein said measurement differentials include a time-difference-of-arrival.

27. The method of claim 23, wherein said measurement differentials include an angle of arrival.

23. A method for tracking an object using a civil aviation passive coherent location system, comprising:

selecting a transmitter transmitting a reference transmission;

receiving said reference transmission;

receiving a scattered transmission scattered by an object within an airspace, wherein said scattered transmission is transmitted from said transmitter;

comparing said scattered transmission to said reference transmission to determine measurement differentials; and

updating an object state estimate according to said measurement differentials.

28. A system for determining an updated state estimate for an object, comprising:

means for receiving a reference transmission from an uncontrolled transmitter and a scattered transmission that originated from said uncontrolled transmitter and was scattered by the object;

means for comparing the received transmission to determine a measurement differential;

means for updating a previous state estimate based on the determined measurement differential; and

means for issuing a warning when said object is within a predetermined distance.

29. A system for determining an updated state estimate for an object, comprising:

means for receiving a reference transmission from an uncontrolled transmitter and a scattered transmission that originated from said uncontrolled transmitter and was scattered by the object;

means for comparing the received transmission to determine a measurement differential;

means for updating a previous state estimate based on the measurement differential; and

means for issuing a warning when said object undertakes an airpath, wherein said airpath intersects with another object.

30. A system for tracking an object using a civil aviation passive coherent location system, comprising:

means for selecting a transmitter transmitting a reference transmission;

means for receiving said reference transmission;

means for receiving a scattered transmission scattered by an object within an airspace, wherein said scattered transmission is transmitted from said transmitter;

means for comparing said scattered transmission to said reference transmission to determine measurement differentials; and

means for updating object state estimate according to said measurement differentials.