Optical navigation system and method for performing self-calibration on the system using a calibration cover
View Patent ↗An optical navigation system and method for performing self-calibration on the system uses captured frames of image data of an interior surface of a calibration cover of the system to detect a performance-related change of the system. In response to the detected performance-related change, a predefined procedure is then initiated.
1. An optical navigation system comprising:
a housing including an aperture;
a calibration cover having an interior surface, the calibration cover being configured to be positioned to cover the aperture of the housing;
an image sensor having an array of photosensitive elements configured to capture frames of image data of the interior surface of the calibration cover when the interior surface of the calibration cover is positioned in the field of view of the image sensor and to capture frames of image data of a navigation surface when the calibration cover is not positioned in the field of view of the image sensor; and
a self-calibration module operably connected to the image sensor, the self-calibration module being configured to detect a performance-related change of the system using the frames of image data of the interior surface of the calibration cover, the self-calibration module being further configured to initiate a predefined procedure in response to the performance-related change of the system.
2. The system of claim 1 wherein the self-calibration module is configured to detect fixed pattern noise in the frames of image data of the interior surface of the calibration cover that is attributable to contaminating particles on some of the components of the system.
3. The system of claim 1 wherein the self-calibration module is configured to determine the light emitting power of a light source of the system using the frames of image data of the interior surface of the calibration cover.
4. The system of claim 1 wherein the self-calibration module is configured to determine optical characteristics of the system with respect to an image capturing operation of the system using the frames of image data of the interior surface.
5. The system of claim 1 wherein the self-calibration module is configured to compare displacement measurements derived using the frames of image data of the interior surface of the calibration cover with known distances on the interior surface to determine the accuracy of the system.
6. The system of claim 1 wherein the predefined procedure includes changing at least one operating parameter of the system.
7. The system of claim 1 wherein the predefined procedure includes notifying a user of the performance-related change of the system.
8. The system of claim 1 wherein the interior surface of the calibration cover is at least partially coated with white aluminum composite signage material.
9. The system of claim 1 wherein the interior surface of the calibration cover includes at least one of an Air Force 1951 calibration test pattern, a dot array calibration target pattern and a line grid pattern.
10. A method for performing self-calibrating on an optical navigation system, comprising:
capturing frames of image data of an interior surface of a calibration cover of the system, the calibration cover being configured to be positioned to cover an aperture of a housing of the system;
detecting a performance-related change of the system using the frames of image data of the interior surface of the calibration cover; and
initiating a predefined procedure in response to the performance-related change of the system.
11. The method of claim 10 wherein the detecting includes analyzing the frames of image data of the interior surface of the calibration cover to detect fixed pattern noise in the frames of image data that is attributable to contaminating particles on some of the components of the system.
12. The method of claim 10 wherein the detecting includes analyzing the frames of image data of the interior surface of the calibration cover to determine the light emitting power of a light source of the system.
13. The method of claim 10 wherein the detecting includes analyzing the frames of image data of the interior surface of the calibration cover to determine optical characteristics of the system with respect to an image capturing operation of the system.
14. The method of claim 10 wherein the detecting includes comparing displacement measurements derived using the frames of image data of the interior surface of the calibration cover with known distances on the interior surface to determine the accuracy of the system.
15. The method of claim 10 wherein the initiating the predefined procedure includes changing at least one operating parameter of the system.
16. The method of claim 10 wherein the initiating the predefined procedure includes notifying a user of the performance-related change of the optical navigation system.
17. The method of claim 10 wherein the interior surface is at least partially coated with white aluminum composite signage material.
18. The method of claim 10 wherein the interior surface includes at least one of an Air Force 1951 calibration test pattern, a dot array calibration target pattern and a line grid pattern.
19. An optical navigation system comprising:
a housing including an aperture;
a calibration cover having an interior surface, the calibration cover being positioned to cover the aperture of the housing, the interior surface of the calibration cover being at least partially coated with white aluminum composite signage material;
an image sensor having an array of photosensitive elements configured to capture frames of image data of the interior surface of the calibration cover when the interior surface of the calibration cover is positioned in the field of view of the image sensor and to capture frames of image data of a navigation surface when the calibration cover is not positioned in the field of view of the image sensor; and
a self-calibration module operably connected to the image sensor, the self-calibration module being configured to detect a performance-related change of the system using the frames of image data of the interior surface of the calibration cover, the self-calibration module being further configured to initiate a predefined procedure in response to the performance-related change of the system.
20. The system of claim 19 wherein the interior surface of the calibration cover further includes at least one of an Air Force 1951 calibration test pattern, a dot array calibration target pattern and a line grid pattern.