Optical open loop pointing test method using celestial bodies

Patent metadata

Field	Value
Publication number	US-10795453-B2
Application number	US-201816047072-A
Country	US
Kind code	B2
Filing date	Jul 27, 2018
Priority date	Jul 27, 2018
Publication date	Oct 6, 2020
Grant date	Oct 6, 2020

Abstract

Systems and methods for testing or correcting optical pointing systems are disclosed. An optical pointing system may include an imaging sensor including a field-of-view (FOV) carried by the optical pointing system, at least one collecting device for collecting optical photons and directing the optical photons to the imaging sensor, at least one directing device for directing the at least one collecting device to different pointing vectors, and at least one non-transitory computer-readable storage medium carried by the optical pointing system having instructions encoded thereon that when executed by at least one processor operates to test the optical pointing system by, inter alia, determining a pointing error based, at least in part, on a macro image of a targeted object.

First claim

The invention claimed is:

1. An optical pointing system comprising:
an imaging sensor;
at least one collecting device for collecting optical photons and directing the optical photons to the imaging sensor;
at least one directing device for directing the at least one collecting device to different pointing vectors; and
at least one non-transitory computer-readable storage medium carried by the optical pointing system having instructions encoded thereon that when executed by at least one processor, the instructions cause the at least one processor to:
determine a position of the optical pointing system;
determine an attitude of the optical pointing system;
calculate a position of a celestial object, wherein the celestial object is the sun;
calculate a vector to the celestial object;
point the optical system along the calculated vector;
capture images of at least a portion of the celestial object within a field of view (FOV) of the imaging sensor;
form a macro image of the celestial object based, at least in part, on the captured images of the celestial object being merged together; and
determine a pointing error based, at least in part, on the macro image of the celestial object and the celestial object to test or correct the optical pointing system.

2. The optical pointing system of claim 1 , further comprising:
an inertial navigation system (INS); wherein the instructions further comprise:
determine the position and the attitude of the optical pointing system from the INS.

3. The optical pointing system of claim 2 , wherein the position of the optical pointing system includes latitude, longitude, and altitude information.

4. The optical pointing system of claim 1 , further comprising:
an inertial measurement unit (IMU) carried by the optical pointing system; and
an inertial navigation system (INS) operably connected with the optical pointing system;

wherein the instructions further comprise:
determine the position of the optical pointing system from the INS; and
determine the attitude of the optical pointing system from the IMU and the INS.

5. The optical pointing system of claim 4 , wherein the instructions further comprise:
determine the attitude of the optical system relative to the INS by a transfer alignment function.

6. The optical pointing system of claim 1 , wherein the instructions further comprise:
determine a centroid of the macro image of the celestial object; and
compare the centroid of the macro image to a known center of the celestial object to determine the pointing error.

7. The optical pointing system of claim 1 , wherein the calculated vector is based, at least in part, on an azimuth of the celestial object and an elevation position of the celestial object.

8. The optical pointing system of claim 1 , wherein the calculated vector is based, at least in part, on at least one unit vector.

9. The optical pointing system of claim 1 , wherein the instructions further comprise:
capture the images of the at least a portion of the celestial object with a step-stare scan.

10. The optical pointing system of claim 9 , wherein the step-stare scan is based, at least in part, on the FOV relative to a size of the celestial object.

11. The optical pointing system of claim 1 , wherein the instructions further comprise:
capture the images of the at least a portion of the celestial object with a spiral pattern or a raster scan pattern.

12. The optical pointing system of claim 1 , wherein the celestial body requires a signal to noise ratio of greater than one.

13. The optical pointing system of claim 1 , wherein the instructions further comprise:
form the macro image utilizing binary thresholding based, at least in part, on pointer vector positions.

14. The optical pointing system of claim 13 , wherein the pointer vector positions are based on based on gimbal mirror encoder angles.

15. The optical pointing system of claim 1 , wherein the instructions further comprise:
adjust the optical pointing system based on the pointing error to reduce the pointing error.

16. The optical pointing system of claim 1 , further comprising:
at least one filtering mechanism positioned along an optical path of the optical photons collected by the at least one collecting device.

17. A method for an optical pointing system, comprising:
determining a position of the optical pointing system;
determining an attitude of the optical pointing system;
calculating a position of a celestial object, wherein the celestial object is the sun;
calculating a vector to the celestial object;
pointing the optical system along the calculated vector;
capturing images of at least a portion of the celestial object within a field of view (FOV);
(FOV) of an imaging sensor, wherein the FOV of the imaging sensor is smaller than an angular size of the celestial object;
forming a macro image of the celestial object based, at least in part, on the captured images of the celestial object being merged together; and
determining a pointing error based, at least in part, on the macro image of the celestial object and the celestial object.

18. The method of claim 17 , further comprising:
determining a centroid of the macro image of the celestial object; and
comparing the centroid of the macro image to a center of the celestial object to determine the pointing error.

19. The method of claim 17 , further comprising:
step-stare scanning the celestial object.

20. The method of claim 17 , further comprising:
forming the macro image utilizing binary thresholding based, at least in part, on pointer vector positions.

Assignees

• Bae Sys Inf & Elect Sys Integ

Inventors

• Powers Michael J

Classifications

• G06F3/0346

  with detection of the device orientation or free movement in a three-dimensional [3D] space, e.g. 3D mice, 6-DOF [six degrees of freedom] pointers using gyroscopes, accelerometers or tilt-sensors · CPC title

• G06T2207/30192

  Weather; Meteorology · CPC title

• G06F3/0304 Primary

  Detection arrangements using opto-electronic means (constructional details of pointing devices not related to the detection arrangement using opto-electronic means G06F3/033; optical digitisers G06F3/042) · CPC title

• G06T7/73 Primary

  using feature-based methods · CPC title

• G06T2207/10004

  Still image; Photographic image · CPC title