Systems and methods for targeting objects of interest in denied GPS environments
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
G06F-019/00
G01C-021/20
G01S-017/87
G01S-017/42
출원번호
US-0180266
(2016-06-13)
등록번호
US-10184799
(2019-01-22)
발명자
/ 주소
Guthrie, Richard B.
출원인 / 주소
The Boeing Company
대리인 / 주소
Ostrager Chong Flaherty & Broitman P.C.
인용정보
피인용 횟수 :
0인용 특허 :
5
초록▼
Systems and methods that enable a targeting system operator, with no access to GPS signals, to self-locate using one or two landmarks and then geolocate an object-of-interest (OOI) using its own position and attitude and the range to the OOI. In the absence of GPS signals, the coordinates of the pos
Systems and methods that enable a targeting system operator, with no access to GPS signals, to self-locate using one or two landmarks and then geolocate an object-of-interest (OOI) using its own position and attitude and the range to the OOI. In the absence of GPS signals, the coordinates of the position of the targeting system can be calculated using a self-location algorithm either: (1) based on a measured direction and a measured range to one landmark and known coordinates of the position of the landmark; or (2) via triangulation based on two landmarks with respective known coordinates and respective measured headings. The coordinates of the position of the OOI can then be calculated using a geolocation algorithm based on the calculated coordinates of the position of the targeting system, and a measured direction and a measured range to the OOI. The calculated coordinates of the position of the OOI can then be sent to a weapons programmer by digital or voice message.
대표청구항▼
1. A system for targeting an object of interest, comprising: a rangefinder configured to measure a range along a line-of-sight that intersects an object;an attitude determination unit co-aligned with the rangefinder and configured to measure azimuth and elevation angles of the line-of-sight;a non-tr
1. A system for targeting an object of interest, comprising: a rangefinder configured to measure a range along a line-of-sight that intersects an object;an attitude determination unit co-aligned with the rangefinder and configured to measure azimuth and elevation angles of the line-of-sight;a non-transitory tangible computer-readable storage medium storing coordinates of a position of a first landmark;a computer configured to execute the following operations:calculating coordinates of a position of the range finder based at least in part on measurements of the azimuth and elevation angles of a first line-of-sight that intersects the first landmark received from the attitude determination unit, and the coordinates of the position of the first landmark retrieved from the non-transitory tangible computer-readable storage medium; andcalculating coordinates of a position of an object of interest based on a measurement of a range along a second line-of-sight to the object of interest received from the rangefinder, measurements of the azimuth and elevation angles of the second line-of-sight received from the attitude determination unit, and the calculated coordinates of the position of the apparatus; andwherein the calculated coordinates of the position of the object of interest are communicated for programming a weapon to target the object. 2. The system as recited in claim 1, wherein the computer is configured to calculate the coordinates of the position of the apparatus based also in part on a measurement of a range along the first line-of-sight to the first landmark received from the rangefinder. 3. The system as recited in claim 2, wherein the non-transitory tangible computer-readable storage medium also stores coordinates of a position of a second landmark, and the computer is also configured to calculate the coordinates of the position of the apparatus based on measurements of the azimuth and elevation angles of the first line-of-sight, the coordinates of the position of the first landmark, measurements of the azimuth and elevation angles of a third line-of-sight that intersects the second landmark received from the attitude determination unit, and the coordinates of the position of the second landmark retrieved from the non-transitory tangible computer-readable storage medium. 4. The system as recited in claim 3, wherein the computer is configured to calculate the coordinates of the position of the apparatus by calculating respective directions for two lines in an ECEF frame of reference and then calculating the coordinates of a midpoint of a shortest segment between the two lines. 5. The system as recited in claim 1, wherein the non-transitory tangible computer-readable storage medium also stores coordinates of a position of a second landmark, and the computer is configured to calculate the coordinates of the position of the apparatus based also in part on measurements of the azimuth and elevation angles of a third line-of-sight that intersects the second landmark received from the attitude determination unit and the coordinates of the position of the second landmark retrieved from the non-transitory tangible computer-readable storage medium. 6. The system as recited in claim 5, wherein the computer is configured to calculate the coordinates of the position of the apparatus by calculating respective directions for two lines in an ECEF frame of reference and then calculating the coordinates of a midpoint of a shortest segment between the two lines. 7. The system as recited in claim 1, wherein the rangefinder is a laser rangefinder and the attitude determination unit is a digital magnetic compass. 8. The system as recited in claim 1, further comprising a GPS antenna and a GPS receiver. 9. A method for targeting an object of interest using a targeting device, comprising: (a) measuring a range to a landmark along a first line-of-sight that intersects the landmark;(b) measuring azimuth and elevation angles of the first line-of-sight;(c) acquiring coordinates of a position of the landmark;(d) calculating coordinates of a position of the targeting device based on the measured range to the landmark, the measured azimuth and elevation angles of the first line-of-sight, and the coordinates of the position of the landmark;(e) measuring a range to an object of interest along a second line-of-sight that intersects the object of interest;(f) measuring azimuth and elevation angles of the second line-of-sight;(g) calculating coordinates of a position of the object of interest based on the measured range to the object of interest, the measured azimuth and elevation angles of the second line-of-sight, and the calculated coordinates of the position of the targeting device; and(h) communicating the calculated coordinates of the object of interest for programming a weapon to target the object. 10. The method as recited in claim 9, wherein steps (a) and (e) are performed using a laser rangefinder. 11. The method as recited in claim 9, wherein steps (b) and (f) are performed using an attitude determination unit. 12. The method as recited in claim 9, wherein step (c) comprises retrieving the coordinates of the position of the landmark from a non-transitory tangible computer-readable storage medium. 13. The method as recited in claim 9, further comprising communicating the calculated coordinates to a weapons programmer by digital or voice message. 14. The method as recited in claim 9, further comprising operating the weapon in accordance with the programming. 15. A method for geolocating an object of interest using a targeting device, comprising: (a) measuring azimuth and elevation angles of a first line-of-sight that intersects a first landmark;(b) acquiring coordinates of a position of the first landmark;(c) measuring azimuth and elevation angles of a second line-of-sight that intersects a second landmark;(d) acquiring coordinates of a position of the second landmark;(e) calculating coordinates of a position of the targeting device based on the measured azimuth and elevation angles of the first and second lines-of-sight, and the coordinates of the positions of the first and second landmarks;(f) measuring a range to an object of interest along a third line-of-sight that intersects the object of interest;(g) measuring azimuth and elevation angles of the third line-of-sight; and(h) calculating coordinates of a position of the object of interest based on the measured range to the object of interest, the measured azimuth and elevation angles of the third line-of-sight, and the calculated coordinates of the position of the targeting device; and(i) communicating the calculated coordinates of the object of interest for programming a weapon to target the object. 16. The method as recited in claim 15, wherein the coordinates of the position of the targeting device are calculated by calculating respective directions for two lines in an ECEF frame of reference and then calculating the coordinates of a midpoint of a shortest segment between the two lines. 17. The method as recited in claim 15, wherein step (f) is performed using a laser rangefinder. 18. The method as recited in claim 15, wherein steps (a), (c) and (g) are performed using an attitude determination unit. 19. The method as recited in claim 15, wherein steps (b) and (d) comprise retrieving the coordinates of the position of the first and second landmarks from a non-transitory tangible computer-readable storage medium. 20. The method as recited in claim 15, further comprising communicating the calculated coordinates to a weapons programmer by digital or voice message.
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이 특허에 인용된 특허 (5)
Alston Steven C. (Bonney Lake WA) Hack Kenneth W. (Seattle WA) Hibbert John A. (Federal Way WA), Automatic turret tracking apparatus for a light air defense system.
Hablani,Hari B., Laser range finder closed-loop pointing technology of relative navigation, attitude determination, pointing and tracking for spacecraft rendezvous.
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