Method and system for preventing anti-aircraft warfare engagement with neutral aircraft

• US 8,477,061 B1
• Filed: 06/29/2010
• Issued: 07/02/2013
• Est. Priority Date: 06/29/2010
• Status: Expired due to Fees

• Current Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Original Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Inventors: Pedersen, Richard N.
• Primary Examiner(s): Brainard, Timothy A
• Application Number:
  US12/825,983
• Time in Patent Office: 1,099 Days
• Field of Search: 342 42- 51
• US Class Current: 342/42
• CPC Class Codes: G01S 13/781 Secondary Surveillance Radar [SSR] in general
• CPC Class Codes: G01S 13/933 of aircraft or spacecraft
• CPC Class Codes: G01S 5/0072 Transmission between mobile stations, e.g. anti-collision systems

Abstract

A method and system that prevents engagement with neutral aircraft utilizes secondary surveillance radar (SSR) in conjunction with traffic alert collision avoidance systems (TCAS) conventionally found on various commercial aircraft. The system and method provide for detecting interrogating signals sent out by a TCAS system of an interrogating aircraft searching for another aircraft that may pose a threat for collision. The system and method of the invention provide for a base system generating signals responsive to the interrogation signals such that there is a decreasing time difference between the interrogating signals and the responsive signals. The decreasing time difference indicates to the interrogating aircraft that another aircraft is approaching its airspace urging the neutral aircraft to change course and avoid entering a guarded tactical airspace thus avoiding unnecessary engagement of the aircraft.

Claims

1. A system for preventing engagement with a neutral aircraft, comprising:

a detector that detects SSR (Secondary Surveillance Radar) interrogation signals generated by an aircraft, including detecting frequency of generation of said interrogation signals; and

a transponder that responds to said interrogation signals by generating corresponding response signals such that a time difference between a first time that said aircraft sends out said interrogation signal and receives said corresponding response signal, and a subsequent time that said aircraft sends out said interrogation signal and receives said corresponding response signal, decreases in time.

2. The system as in claim 1, wherein said detector further detects an altitude of said aircraft and said response signals include an indication that a sender is situated at or near said altitude.

3. The system as in claim 1, further comprising a signal generator that generates squitter transmissions to locate aircraft.

4. The system as in claim 3, wherein said signal generator generates Mode S squitter transmissions using a particular address and said detector searches for Mode S interrogation signals generated using said address.

5. The system as in claim 1, wherein said frequency of generation of said interrogation signals includes an initial value of about one every 5 seconds.

6. The system as in claim 1, wherein said time difference decreases in time by increments of about 0.05 seconds.

7. The system as in claim 1, further comprising a computer readable medium with executable instructions that cause said transponder to generate said corresponding response signals with said time difference that decreases in time.

8. The system as in claim 1, wherein said transponder is disposed on a warship that further comprises weapons capable of firing at said aircraft.

9. The system as in claim 1, wherein said corresponding response signals are sent predictively and are initially sent about 0.05 to 0.1 seconds before said interrogation signals are received.

10. The system as in claim 1, wherein said interrogation signals and said response signals each comprise Mode S SSR signals, and said interrogation signals are generated by a TCAS (Traffic Alert and Collision Avoidance System) system of said aircraft.

11. The system as in claim 1, wherein said interrogation signals comprise Mode C SSR signals, and said interrogation signals are generated by a TCAS (Traffic Alert and Collision Avoidance System) system of said aircraft.

12. The system as in claim 1, wherein said corresponding response signals generated by said transponder are visually displayed on an instrument panel in a cockpit of said aircraft.

13. The system as in claim 1, wherein said system further comprises weapons capable of firing at said aircraft and a sub-system for determining if said aircraft is a neutral aircraft.

14. The system as in claim 1, wherein said corresponding response signals are sent predictively before said interrogation signals are received.

15. The system as in claim 1, wherein said time difference is decreased in order to mimic a reduction in distance between the position of said aircraft and the position of said transponder.

16. A method for preventing engagement with a neutral aircraft, said method comprising:

detecting SSR (Secondary Surveillance Radar) interrogation signals generated by an aircraft, including detecting a frequency of generation of said interrogation signals; and

responding to said interrogation signals by generating corresponding response signals such that a time difference between a first time that said aircraft generates one said interrogation signal and receives said corresponding response signal, and a subsequent time that said aircraft sends out said interrogation signal and receives said corresponding response signal, decreases in time.

17. The method as in claim 16, further comprising, prior to said detecting, generating squitter transmission signals to locate said aircraft.

18. The method as in claim 17, wherein said generating squitter transmissions comprises generating Mode S squitter transmissions.

19. The method as in claim 17, wherein said squitter transmission signals use a designated address and said detecting SSR interrogation signals comprises monitoring airspace for Mode S interrogation signals that use said designated address.

20. The method as in claim 16, further comprising detecting an altitude of said aircraft and wherein said responding comprises said response signals indicating that a sender is situated at or near said altitude.

21. The method as in claim 16, wherein said frequency of generation of said interrogation signals decreases in time.

22. The method as in claim 16, wherein said interrogation signals comprise one of Mode S interrogation signals and Mode C interrogation signals.

23. The method as in claim 16, further comprising determining if said aircraft is a neutral aircraft.

24. The method as in claim 16, wherein said generating corresponding response signals comprises providing a visible alert in a display of an instrument panel of said aircraft.

25. The method as in claim 16, wherein said responding comprises predictively responding to said interrogation signals before said interrogation signals are detected, for at least some of said interrogation signals.

26. The method as in claim 16, wherein said detecting a frequency comprises detecting a frequency of once every 5 seconds and said responding comprises initially responding 4.95 seconds after one of said corresponding interrogation signals is sent, then responding at incrementally earlier times after said interrogation signals are sent.

27. The method as in claim 16, wherein said time difference is decreased in order to mimic a reduction in distance between the position of said aircraft and the position of said transponder.