Adaptive scan rate space surveillance sensor for super-GEO orbits

Patent metadata

Field	Value
Publication number	US-10167091-B2
Application number	US-201514841590-A
Country	US
Kind code	B2
Filing date	Aug 31, 2015
Priority date	Aug 31, 2015
Publication date	Jan 1, 2019
Grant date	Jan 1, 2019

Abstract

Systems, methods, and apparatus for space surveillance are disclosed herein. In one or more embodiments, the disclosed method involves scanning, by at least one sensor on at least one satellite in super-geostationary earth orbit (super-GEO), a raster scan over a field of regard (FOR). In one or more embodiments, the scanning is at a variable rate, which is dependent upon a target dwell time for detecting a target of interest. In at least one embodiment, the target dwell time is a function of a characteristic brightness of the target.

First claim

We claim:

1. A method for space surveillance, the method comprising:
scanning, by at least one sensor on at least one satellite in super-geostationary earth orbit (super-GEO), a raster scan over a field of regard (FOR),
wherein the scanning is at a variable rate, which is dependent upon a target dwell time for detecting a target of interest,
wherein the target dwell time is a function of a characteristic brightness of the target, and
wherein the field of regard (FOR) of the at least one sensor is a function of a geometry between a sun and the at least one satellite and a function of an angle that the at least one satellite is pointing.

2. The method of claim 1 , wherein the target dwell time is further a function of a range from the at least one sensor to the target of interest and a function of a solar phase angle.

3. The method of claim 1 , wherein the raster scan comprises at least one sweep.

4. The method of claim 3 , wherein the at least one sweep is a continuous sweep.

5. The method of claim 1 , wherein the method further comprises, during the scanning, collecting, by the at least one sensor, image frames over time.

6. The method of claim 5 , wherein the image frames overlap.

7. The method of claim 1 , wherein super-GEO is an orbit has a radius that is larger than a geostationary earth orbit (GEO) radius for a majority of a duration of an orbital cycle.

8. The method of claim 1 , wherein a time required for the raster scan is dependent upon an aperture diameter of the at least one sensor and the target dwell time.

9. The method of claim 8 , wherein the time required for the raster scan is further dependent upon an altitude of the at least one sensor.

10. The method of claim 9 , wherein the time required for the raster scan is further dependent upon an instantaneous field of view (IFOV) of the at least one sensor.

11. The method of claim 5 , wherein the method further comprises comparing a detected brightness level in at least one of the image frames to a detection threshold.

12. The method of claim 11 , wherein the method further comprises determining that the target of interest is present when the detected brightness level in at least one of the image frames exceeds the detection threshold.

13. The method of claim 11 , wherein the method further comprises determining that the target of interest is not present when the detected brightness level in at least one of the image frames does not exceed the detection threshold.

14. The method of claim 1 , wherein when there is two or more of the satellites, the method further comprises one of the satellites scanning at least a portion of a desired scan area where at least one of the sensors of at least one of the other satellites has low performance.

15. A system for space surveillance, the system comprising:
at least one satellite in super-geostationary earth orbit (super-GEO); and
at least one sensor, on the at least one satellite, to scan a raster scan over a field of regard (FOR),
wherein the scanning is at a variable rate, which is dependent upon a target dwell time for detecting a target of interest,
wherein the target dwell time is a function of a characteristic brightness of the target, and
wherein the field of regard (FOR) of the at least one sensor is a function of a geometry between a sun and the at least one satellite and a function of an angle that the at least one satellite is pointing.

16. The system of claim 15 , wherein the target dwell time is further a function of a range from the at least one sensor to the target of interest and a function of a solar phase angle.

17. The system of claim 15 , wherein the raster scan comprises at least one sweep.

18. The system of claim 17 , wherein the at least one sweep is a continuous sweep.

19. The system of claim 15 , wherein the at least one sensor is further configured to collect image frames over time.

20. The system of claim 19 , wherein the image frames overlap.

Assignees

• Boeing Co

Inventors

• Gerwe David R
• Williams Keith R
• Lambert John
• Tarbuck Paul D
• Estrada Edward A

Classifications

• B64G1/1021 Primary

  Earth observation satellites · CPC title

• H04N23/71

  Circuitry for evaluating the brightness variation · CPC title

• G06F18/22

  Matching criteria, e.g. proximity measures · CPC title

• H04N23/698

  for achieving an enlarged field of view, e.g. panoramic image capture · CPC title

• G06T2207/10032

  Satellite or aerial image; Remote sensing · CPC title