Mobile ballistic missile detection and defense system
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
F41G-007/30
F41G-007/20
F41G-007/00
G01S-013/00
출원번호
US-0852045
(2004-05-24)
등록번호
US-7348918
(2008-03-25)
발명자
/ 주소
Redano,Richard T.
출원인 / 주소
Lockheed Martin Corporation
대리인 / 주소
Duane Morris, LLP
인용정보
피인용 횟수 :
11인용 특허 :
16
초록▼
The present invention is directed towards a ballistic missile detection and defense system. The system of the present invention comprises a ship based interceptor or antiballistic missile, a missile launch detection and tracking system, and a signal processing system capable of receiving said tracki
The present invention is directed towards a ballistic missile detection and defense system. The system of the present invention comprises a ship based interceptor or antiballistic missile, a missile launch detection and tracking system, and a signal processing system capable of receiving said tracking signal calculating an intercept trajectory for an antiballistic missile to intercept a ballistic missile, and further capable of outputting an intercept trajectory program to an antiballistic missile.
대표청구항▼
What is claimed is: 1. A mobile ballistic missile detection and defense system, comprising: a. a nonland based missile launch detection and tracking system configured to detect a missile launch, track the detected launched missile, and output a tracking signal indicative of the trajectory of the de
What is claimed is: 1. A mobile ballistic missile detection and defense system, comprising: a. a nonland based missile launch detection and tracking system configured to detect a missile launch, track the detected launched missile, and output a tracking signal indicative of the trajectory of the detected launched missile in flight; b. a ship; and c. a signal processing system configured to receive said tracking signal, calculate a nonaligned intercept trajectory for an antiballistic missile to intercept the detected launched missile having a trajectory as described by said tracking signal, and further output a nonaligned intercept trajectory program for guiding an antiballistic missile, wherein said antiballistic missile located on said ship, said antiballistic missile comprising a guidance system configured to receive the nonaligned intercept trajectory program and guide the antiballistic missile along the nonaligned intercept trajectory. 2. The system of claim 1, wherein: a. said missile launch detection and tracking system is a means for detecting the location of the missile launch, tracking the detected launched missile in flight, and outputting the tracking signal indicative of the trajectory of the detected launched missile in flight; and b. said signal processing system is a means for receiving said tracking signal, calculating the nonaligned intercept trajectory for the antiballistic missile to intercept the detected launched missile having a trajectory as described by said tracking signal, and further outputting the nonaligned intercept trajectory program for guiding said antiballistic missile. 3. The system of claim 1, wherein said guidance system is remotely located from the signal processing system. 4. The system of claim 1, wherein said missile launch detection and tracking system is located on a satellite. 5. The system of claim 4, wherein said missile launch detection and tracking system comprises a high resolution imaging system. 6. The system of claim 4, wherein said missile launch detection and tracking system comprises an infrared detection system. 7. The system of claim 1, wherein said missile launch detection and tracking system comprises a radar tracking system. 8. A mobile ballistic missile detection and defense system, comprising: a. a nonland based missile launch detection and tracking system configured to detect the location of a missile launch, track a detected missile in flight, and output a tracking signal indicative of the trajectory of the detected missile in flight; b. a ship; and c. a nonland based signal processing system configured to receive said tracking signal, calculate a nonaligned intercept trajectory for an antiballistic missile to intercept the detected missile having a trajectory as described by said tracking signal, and further output a nonaligned intercept trajectory program for guiding the antiballistic missile, wherein said antiballistic missile located on said ship, said antiballistic missile comprising a guidance system configured to receive the nonaligned intercept trajectory program and guide the antiballistic missile along the nonaligned intercept trajectory. 9. The system of claim 8, wherein said missile launch detection and tracking system is located on a satellite. 10. The system of claim 9, wherein said missile launch detection and tracking system comprises a high resolution imaging system. 11. The system of claim 9, wherein said missile launch detection and tracking system comprises an infrared detection system. 12. The system of claim 8, wherein said missile launch detection and tracking system comprises a radar tracking system. 13. The system of claim 8, wherein said guidance system is remotely located from the signal processing system. 14. The system of claim 8, wherein: a. said missile launch detection and tracking system is a means for detecting the location of the missile launch, tracking the detected missile in flight, and outputting the tracking signal indicative of the trajectory of the detected missile in flight; and b. said signal processing system is a means for receiving said tracking signal, calculating the nonaligned intercept trajectory for the antiballistic missile to intercept the detected missile having a trajectory as described by said tracking signal, and further outputting the nonaligned intercept trajectory program for guiding said antiballistic missile. 15. A mobile ballistic missile detection and defense system, comprising: a. a nonland based missile launch detection and tracking system configured to detect a missile launch, tracking a detected missile in flight, and output a tracking signal indicative of the trajectory of the detected missile in flight; b. a ship; and c. a signal processing system located on said ship configured to receive said tracking signal, calculate a nonaligned intercept trajectory for an antiballistic missile to intercept the detected missile having a trajectory as described by said tracking signal, and further output a nonaligned intercept trajectory program for guiding the antiballistic missile, wherein said antiballistic missile located on said ship, said antiballistic missile comprising a guidance system configured to receive the nonaligned intercept trajectory program and guide the antiballistic missile along the nonaligned intercept trajectory. 16. The system of claim 15, wherein said missile launch detection and tracking system is located on said ship. 17. The system of claim 15, wherein said guidance system is remotely located from the signal processing system. 18. The system of claim 15, wherein: a. said missile launch detection and tracking system is a means for detecting the location of the missile launch, tracking the detected missile in flight, and outputting the tracking signal indicative of the trajectory of the detected missile in flight; and b. said signal processing system is a means for receiving said tracking signal, calculating the nonaligned intercept trajectory for the antiballistic missile to intercept the detected missile having a trajectory as described by said tracking signal, and further outputting the nonaligned intercept trajectory program for guiding said antiballistic missile. 19. The system of claim 15, wherein said ship is an Aegis class cruiser. 20. The system of claim 15, wherein said missile launch detection and tracking system is located on a satellite.
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이 특허에 인용된 특허 (16)
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McIntosh John C., Passive three dimensional track of non-cooperative targets through opportunistic use of global positioning system (GPS) and GLONASS signals.
Luu, Thu-Van T.; Boka, Jeffrey B.; Harcourt, Michael J.; Mookerjee, Purusottam, Burnout time estimation and early thrust termination determination for a boosting target.
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