Spot leading target laser guidance for engaging moving targets
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
F41G-007/30
F42B-015/01
F41G-007/00
F42B-015/00
출원번호
US-0783681
(2010-05-20)
등록번호
US-8237095
(2012-08-07)
발명자
/ 주소
Glaros, Louis N.
Eddins, William B.
Gaylord, Charles
Kincheloe, Michael
출원인 / 주소
Lockheed Martin Corporation
대리인 / 주소
Jetter & Associates, P.A.
인용정보
피인용 횟수 :
0인용 특허 :
25
초록▼
A laser lead designator for guiding a laser guided weapon (LGW) to strike a moving target includes a laser source for providing a laser beam and a controller coupled to receive a position and a velocity of the moving target. The controller provides a control signal for pointing the laser beam a spec
A laser lead designator for guiding a laser guided weapon (LGW) to strike a moving target includes a laser source for providing a laser beam and a controller coupled to receive a position and a velocity of the moving target. The controller provides a control signal for pointing the laser beam a specified lead distance ahead of the position of the moving target to position a laser spot on a ground location ahead of the moving target. The lead distance compensates for an impact shortfall value that is a function of at least one shortfall parameter including a speed of the moving target so that the LGW shortfalls the laser spot on the moving target. The laser designator is separate from the LGW.
대표청구항▼
1. A laser lead designator for guiding a laser guided weapon (LGW) to strike a moving target, comprising: a laser source for providing a laser beam, anda controller coupled to receive a position and a velocity of said moving target for providing a control signal for pointing said laser beam a specif
1. A laser lead designator for guiding a laser guided weapon (LGW) to strike a moving target, comprising: a laser source for providing a laser beam, anda controller coupled to receive a position and a velocity of said moving target for providing a control signal for pointing said laser beam a specified lead distance ahead of said position of said moving target to position a resulting laser spot on a ground location ahead of said moving target to compensate for an impact shortfall value that is a function of at least one shortfall parameter including a speed of said moving target so that said LGW shortfalls said laser spot on said moving target,wherein said laser designator is separate from said LGW. 2. The laser lead designator of claim 1, wherein said specified lead distance is provided by a look-up table accessible by said controller. 3. The laser lead designator of claim 1, wherein said at least one shortfall parameter includes an engagement geometry and a maneuverability of said LGW. 4. The laser lead designator of claim 1, wherein said lead distance is adjusted to account for wind. 5. The laser lead designator of claim 1, further comprising a target tracker for determining said position and said velocity of said moving target, wherein said laser lead designator comprises an integrated laser lead designator and target tracker system. 6. The laser lead designator of claim 5, wherein said target tracker comprises a passive ranging tracker. 7. The laser lead designator of claim 5, wherein said target tracker comprises a laser ranger that implements target state estimation (TSE). 8. A laser guided weapon delivery system, comprising a laser guided weapon (LGW), anda laser lead designator for guiding said LGW to strike a moving target, comprising:a laser source for providing a laser beam;a target tracker for determining a position and a velocity of said moving target, anda controller coupled to receive said position and said velocity of said moving target for providing a control signal for pointing said laser beam a specified lead distance ahead of said position of said moving target to position a resulting laser spot on a ground location ahead of said moving target to compensate for an impact shortfall value that is a function of at least one shortfall parameter including a speed of said moving target so that said LGW shortfalls said laser spot on said moving target,wherein said laser designator is separate from said LGW. 9. The system of claim 8, wherein said specified lead distance is provided by a look-up table accessible by said controller. 10. The system of claim 8, wherein said at least one shortfall parameter includes an engagement geometry and a maneuverability of said LGW. 11. The system of claim 8, wherein said lead distance is adjusted to account for wind. 12. The system of claim 8, wherein said target tracker comprises a passive ranging tracker. 13. The system of claim 8, wherein said target tracker comprises a laser ranger that implements target state estimation (TSE). 14. The system of claim 8, wherein said LGW comprises a laser guided bomb (LGB) or a laser guided missile (LGM). 15. The system of claim 8, wherein said laser lead designator and said target tracker are co-located to provide an integrated laser lead designator and target tracker system. 16. A method for guiding a laser guided weapon (LGW) to strike a moving target, comprising: tracking said moving target for determining a position and a velocity of said moving target;releasing said LGW toward said moving target;obtaining an impact shortfall value for said LGW relative to said moving target, wherein said impact shortfall value is a function of at least one shortfall parameter including a speed of said moving target;commanding a laser lead designator comprising a laser source for generating a laser beam that is separate from said LGW to point said laser beam a specified lead distance ahead of said position of said moving target to position a resulting laser spot on a ground location ahead of said moving target to compensate for said impact shortfall value, andrepeating said tracking, said obtaining and said commanding a plurality of times to update said specified lead distance, wherein said LGW adjusts its flight-path to follow radiation emanating from said laser spot,wherein at a terminal time said LGW runs out of maneuver space so that said LGW shortfalls said laser spot on said moving target. 17. The method of claim 16, wherein said specified lead distance is provided by a look-up table. 18. The method of claim 16, wherein said at least one shortfall parameter includes an engagement geometry and a maneuverability of said LGW. 19. The method of claim 16, wherein said lead distance is adjusted to account for wind. 20. The method of claim 16, wherein said laser lead designator is in an air-based position. 21. The method of claim 16, wherein said laser lead designator is in a ground-based position. 22. The method of claim 16, wherein said tracking comprises passive ranging. 23. The method of claim 16, wherein said tracking includes laser ranging that implements target state estimation (TSE).
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