Active defense system against tactical ballistic missiles

• US 5,340,056 A
• Filed: 02/24/1993
• Issued: 08/23/1994
• Est. Priority Date: 02/27/1992
• Status: Expired due to Term

• Current Assignee: Rafael - Armament Development Authority Ltd.
• Original Assignee: State of Israel--Ministry of Defence Armament Development Authority Rafael
• Inventors: Guelman, Moshe, Yavnai, Arie
• Primary Examiner(s): Pihulic, Daniel T.
• Application Number:
  US08/021,871
• Time in Patent Office: 545 Days
• Field of Search: 244/3.15, 244/3.16, 244/76 R, 244/175, 244/194, 244/195, 364/462, 364/516
• US Class Current: 244/3.16
• CPC Class Codes: F41G 7/007 Preparatory measures taken before the launching of the guided missiles
• CPC Class Codes: F41G 7/2206 using a remote control station
• CPC Class Codes: F41G 7/2253 Passive homing systems, i.e. comprising a receiver and do not requiring an active illumination of the target
• CPC Class Codes: F41G 7/2293 using electromagnetic waves other than radio waves

Abstract

An active defense system against ballistic missiles. The system includes a fleet consisting of a plurality of flying platforms fitted with interceptor missiles which loiter over hostile territory. The flying platforms communicate with each other by suitable data links and at least some of them also communicate with a ground station located in friendly territory. The interceptor missiles have electro-optical seeking and tracking capabilities and the data which the missile generates while in captive flight are communicated to a processor of the associated flight platform for autonomous decision whether to launch or not to launch the missile.

Claims

1. An active defence system against tactical ballistic missiles, characterized by a capability of detecting and intercepting launched tactical ballistic missiles and comprising in combination:

i) a ground control station located in a friendly area;

ii) a fleet including a plurality of airborne units with missile interception capability comprising each a programmable, self-propelled air vehicle carrying at least one interceptor missile fitted with electro-optical seeker means with searching and tracking capability during captive flight and homing capability during free flight;

iii) connector means in each air vehicle for connection to each of its carried interceptor missiles;

iv) data link means in each air vehicle for communication with other air vehicles of the fleet and

v) processor means in the air vehicle of each airborne unit for autonomous decision on the transmission of commands on the basis of data from own sensors and own data bases and from other air vehicles of the fleet and from the autonomous detection of a ground launched hostile ballistic missile.

2. A defence system according to claim 1, wherein the fleet includes at lease one air vehicle for central fleet management and supervision in addition to said airborne units with missile interception capability.

3. A defence system according to claim 1, wherein the fleet architecture and said processor means are designed to operate in a decentralized-cooperative mode.

4. A defence system according to claim 1, wherein the fleet architecture and said processor means are designed to operate in a distributed-decentralized mode.

5. A defence system according to claim 1, wherein the fleet architecture and said processor means are designed to operate in a centralized mode.

6. A defence system according to claim 1, wherein the fleet architecture and said processor means are designed to operate in a hierarchical-distributed mode.

7. A defense system according to claim 1, in which said data link comprises means for communicating with said ground control station.

8. A defence system according to claim 1, wherein the air vehicle of an airborne unit comprises electro-optical seeker means additional to the seeker means forming part of the interceptor missile.

9. A defence system according to claim 1, wherein Said electro-optical seeker means is an infra-red device.

10. A defence system according to claim 1, wherein said electro-optical seeker means is a television camera.

11. A defence system according to claim 1, wherein said electro-optical seeker means is a thermal imaging camera.

12. A defence system according to claim 1, wherein all air vehicles are unmanned.

13. A defence system according to claim 1, wherein at least one air vehicle is manned.

14. A defence system according to claim 7, comprising an airborne relay station for data link between air vehicles and the ground control station.

15. A defence system according to claim 1, wherein the air vehicle of each airborne unit is fitted with passive means for protection against hostile radar and/or electro-optical seeking means of hostile air-to-air and ground-to-air missiles.

16. A defence system according to claim 1, wherein the air vehicle of each airborne unit is fitted with active means for protection against hostile radar and/or electro-optical seeking means of hostile air-to-air and ground-to-air missiles.

18. A defence system according to claim 1, wherein the data link between an air vehicle and said ground control station is two-way whereby the system affords surveillance and early warning capability.

17. A programmable, self-propelled air vehicle including processor means, data link means, means for carrying at least one interceptor missile and means for connection with each carried missile, wherein said processor means includes means for calculating a distance to a hostile tactical ballistic target missile solely from measurement data obtained from at least one airborne unit indicating an angle and angle rate of a line of sight towards the target missile.

19. An air vehicle according to claim 17, being of the unmanned type.

20. An air vehicle according to claim 17, being of the manned type.

21. An air vehicle according to claim 17, fitted with electro-optical seeker means.

22. An air vehicle according to claim 21, wherein said electro-optional seeker means comprise further identification and detection means for the performance of functions additional to seeking and tracking of hostile ballistic missiles.

23. An air vehicle according to claim 22, wherein said further identification and detection means serve for Friend-or-Foe identification and electronic and electro-optical counter-measure detection.

24. An air vehicle according to claim 17, fitted with passive means for protection against hostile radar and electro-optical seeking means of hostile air-to-air and ground-to-air missiles.

25. An air vehicle according to claim 17, fitted with active means for protection against hostile radar and electro-optical seeking means of hostile air-to-air and ground-to-air missiles.

26. An airborne unit comprising an air vehicle according to claim 17, carrying at least one interceptor missile with electro-optical seeker means, connector means being provided for connection between the air vehicle and said at least one interceptor missile.