IPC분류정보
국가/구분 |
United States(US) Patent
등록
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국제특허분류(IPC7판) |
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출원번호 |
US-0709780
(2010-02-22)
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등록번호 |
US-8355536
(2013-01-15)
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발명자
/ 주소 |
- Agurok, Ilya
- Falicoff, Waqidi
- Alvarez, Roberto
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출원인 / 주소 |
- Light Prescriptions Innovators LLC
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인용정보 |
피인용 횟수 :
0 인용 특허 :
23 |
초록
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A passive electro-optical tracker uses a two-band IR intensity ratio to discriminate high-speed projectiles and obtain a speed estimate from their temperature, as well as determining the trajectory back to the source of fire. In an omnidirectional system a hemispheric imager with an MWIR spectrum sp
A passive electro-optical tracker uses a two-band IR intensity ratio to discriminate high-speed projectiles and obtain a speed estimate from their temperature, as well as determining the trajectory back to the source of fire. In an omnidirectional system a hemispheric imager with an MWIR spectrum splitter forms two CCD images of the environment. Three methods are given to determine the azimuth and range of a projectile, one for clear atmospheric conditions and two for nonhomogeneous atmospheric conditions. The first approach uses the relative intensity of the image of the projectile on the pixels of a CCD camera to determine the azimuthal angle of trajectory with respect to the ground, and its range. The second calculates this angle using a different algorithm. The third uses a least squares optimization over multiple frames based on a triangle representation of the smeared image to yield a real-time trajectory estimate.
대표청구항
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1. A projectile tracking device comprising: detector apparatus for converting into electronic form images in at least two infrared wavebands;optics for projecting onto the detector apparatus an image in the at least two infrared wavebands of a scene across which a projectile passes;first logic opera
1. A projectile tracking device comprising: detector apparatus for converting into electronic form images in at least two infrared wavebands;optics for projecting onto the detector apparatus an image in the at least two infrared wavebands of a scene across which a projectile passes;first logic operative to obtain from the images in electronic form apparent brightnesses of the projectile at the optics in at least two infrared wavebands;second logic operative to estimate the speed of the projectile from the ratio of the two measured apparent brightnesses;third logic operative to obtain from the images in electronic form an azimuth of the projectile from the optics at successive times; andfourth logic operative to estimate the direction of the trajectory of the projectile and the distance to the trajectory in an azimuth plane including a location of the detector apparatus from the measured azimuths in combination with the ratio between the measured apparent brightnesses;wherein at least some of at least one of said first, second, third, and fourth logic comprises a computer connected to receive image data from the detector apparatus and programmed to estimate parameters of the projectile trajectory using at least two of:a method comprising measuring the azimuth of the projectile from the optics at successive times, and estimating the direction of the trajectory and the distance to the trajectory of the projectile from the measured azimuths in combination with the ratios between the measured apparent brightnesses;a method wherein a perpendicular from the optics to the projectile trajectory and hence the direction of the projectile trajectory are estimated by locating the point with zero value of the second derivative with respect to time of the direction to the projectile, further combining the estimated projectile speed with the projectile trajectory direction for calculating distances from the optics to the projectile; anda method further comprising measuring the direction of the projectile from the optics at successive times, and estimating the trajectory of the projectile and the distance to the trajectory from the measured directions in combination with the estimated speed;and to provide a final estimate using a comparison of estimates from at least two said methods of estimating parameters. 2. The tracking device of claim 1, wherein the detector apparatus comprises two photosensitive detector arrays, one for each of the at least two infrared wavebands, common objective optics, and a frequency-selective beam-splitter to direct light of each waveband to an appropriate one of the detector arrays. 3. The tracking device of claim 1, wherein the computer is further programmed to estimate parameters of the projectile trajectory using at least one of: a method comprising measuring the azimuth of the projectile from the optics at successive times, and estimating the direction of the trajectory of the projectile from the measured azimuths in combination with the ratios between the measured apparent brightnesses;a method wherein a perpendicular from the optics to the projectile trajectory and hence the direction of the projectile trajectory are estimated by locating the point with zero value of the second derivative with respect to time of the direction to the projectile, further combining the estimated projectile speed with the projectile trajectory direction for calculating distances from the optics to the projectile; anda method further comprising measuring the direction of the projectile from the optics at successive times, and estimating the trajectory of the projectile from the measured directions in combination with the estimated speed. 4. The tracking device of claim 1, wherein the computer is programmed to estimate the speed by estimating the temperature of the projectile from the ratio of the two measured apparent brightnesses and estimating the speed from the estimated temperature. 5. The tracking device of claim 1, wherein the computer is programmed to combine the estimated projectile speed with the estimated projectile trajectory direction for calculating distances from the optics to the projectile. 6. The tracking device of claim 1, wherein the computer is programmed to estimate a perpendicular from the optics to the projectile trajectory and hence the direction of the projectile trajectory by locating the point with zero value of the second derivative with respect to time of the direction from the optics to the projectile. 7. The tracking device of claim 1, wherein the computer is programmed to choose based on atmospheric conditions between projectile trajectory parameters calculated with at least two of: a method comprising measuring the azimuth of the projectile from the optics at successive times, and estimating the direction of the trajectory of the projectile from the measured azimuths in combination with the ratios between the measured apparent brightnesses;a method comprising estimating a perpendicular from the optics to the projectile trajectory and hence the direction of the projectile trajectory by locating the point with zero value of the second derivative with respect to time of the direction to the projectile, further combining the estimated projectile speed with the projectile trajectory direction for calculating distances from the optics to the projectile; anda method further comprising measuring the direction of the projectile from the optics at successive times, and estimating the trajectory of the projectile from the measured directions in combination with the estimated speed. 8. The tracking device of claim 1, wherein the computer is programmed to estimate the size of the projectile from the calculated trajectory and at least one measured apparent brightness. 9. The tracking device of claim 8, wherein the computer is programmed to: determine a distance from the optics to the projectile using the calculated trajectory;calculate an absolute brightness from the measured apparent brightness in at least one waveband and the determined distance to the projectile; andcalculate the estimated size from the calculated absolute brightness and the estimated temperature. 10. The tracking device of claim 1, wherein the computer is programmed to estimate at least one of an origin of the projectile and a hit point of the projectile by extending an observable part of the trajectory and to superimpose the extended trajectory with a local terrain map. 11. A computer comprising a non-transitory computer readable medium encoded with a computer program to carry out a method comprising: measuring apparent brightnesses of a projectile at an observing location in at least two infrared wavebands;estimating a speed of the projectile from the ratio of the two measured apparent brightnesses;measuring an azimuth of the projectile from the observing location at successive times; andestimating the direction of the trajectory of the projectile from the measured azimuths in combination with the ratios between the measured apparent brightnesses using at least two of:a method comprising measuring the azimuth of the projectile from the optics at successive times, and estimating the direction of the trajectory and the distance to the trajectory of the projectile from the measured azimuths in combination with the ratios between the measured apparent brightnesses;a method wherein a perpendicular from the optics to the projectile trajectory and hence the direction of the projectile trajectory are estimated by locating the point with zero value of the second derivative with respect to time of the direction to the projectile, further combining the estimated projectile speed with the projectile trajectory direction for calculating distances from the optics to the projectile; anda method further comprising measuring the direction of the projectile from the optics at successive times, and estimating the trajectory of the projectile and the distance to the trajectory from the measured directions in combination with the estimated speed;and to provide a final estimate using a comparison of estimates from at least two said methods of estimating parameters. 12. A non-transitory computer readable storage medium encoded with a computer program that will cause a processor of a suitable general purpose computer to carry out a method comprising: measuring apparent brightnesses of a projectile at an observing location in at least two infrared wavebands;estimating the speed of the projectile from the ratio of the two measured apparent brightnesses;measuring an azimuth of the projectile from the observing location at successive times; andestimating the direction of the trajectory of the projectile from the measured azimuths in combination with the ratios between the measured apparent brightnesses using at least two of:a method comprising measuring the azimuth of the projectile from the optics at successive times, and estimating the direction of the trajectory and the distance to the trajectory of the projectile from the measured azimuths in combination with the ratios between the measured apparent brightnesses;a method wherein a perpendicular from the optics to the projectile trajectory and hence the direction of the projectile trajectory are estimated by locating the point with zero value of the second derivative with respect to time of the direction to the projectile, further combining the estimated projectile speed with the projectile trajectory direction for calculating distances from the optics to the projectile; anda method further comprising measuring the direction of the projectile from the optics at successive times, and estimating the trajectory of the projectile and the distance to the trajectory from the measured directions in combination with the estimated speed;and to provide a final estimate using a comparison of estimates from at least two said methods of estimating parameters. 13. A method of tracking a projectile in air, comprising: using optics to project onto a detector apparatus an image in at least two infrared wavebands of a scene across which a projectile passes;using the detector apparatus to convert into electronic form images in said at least two infrared wavebands;using first logic to measure apparent brightnesses of the projectile at an observing location in said at least two infrared wavebands;using second logic to estimate the speed of the projectile from the ratio of the two measured apparent brightnesses;using third logic to measure an azimuth of the projectile from the observing location at successive times; andusing fourth logic to estimate the direction of the trajectory of the projectile in an azimuth plane including a location of the optics from the measured azimuths in combination with the ratios between the measured apparent brightnesses using at least two of:a method comprising measuring the azimuth of the projectile from the optics at successive times, and estimating the direction of the trajectory and the distance to the trajectory of the projectile from the measured azimuths in combination with the ratios between the measured apparent brightnesses;a method wherein a perpendicular from the optics to the projectile trajectory and hence the direction of the projectile trajectory are estimated by locating the point with zero value of the second derivative with respect to time of the direction to the projectile, further combining the estimated projectile speed with the projectile trajectory direction for calculating distances from the optics to the projectile; anda method further comprising measuring the direction of the projectile from the optics at successive times, and estimating the trajectory of the projectile and the distance to the trajectory from the measured directions in combination with the estimated speed;and to provide a final estimate using a comparison of estimates from at least two said methods of estimating parameters. 14. The method of claim 13, further comprising combining the estimated projectile speed with the estimated projectile trajectory direction for calculating distances from the observing location to the projectile. 15. The method of claim 13, wherein a perpendicular from the observing location to the projectile trajectory and hence the direction of the projectile trajectory are estimated by locating the point with zero value of the second derivative with respect to time of the direction to the projectile. 16. The method of claim 13, comprising choosing based on atmospheric conditions between projectile trajectory parameters calculated with said at least two methods. 17. The method of claim 13, further comprising estimating the size of the projectile from the calculated trajectory and at least one measured apparent brightness.
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