Photogrammetric recession measurements of an ablating surface

• US 8,290,246 B1
• Filed: 12/17/2007
• Issued: 10/16/2012
• Est. Priority Date: 12/17/2007
• Status: Active Grant

• Current Assignee: USA As Represented By The Administrator Of The NASA
• Original Assignee: The United States of America As Represented By The Secretary of Agriculture
• Inventors: Schairer, Edward T., Heineck, James T.
• Primary Examiner(s): Desire, Gregory M
• Application Number:
  US11/958,296
• Time in Patent Office: 1,765 Days
• Field of Search: 382/154, 348/47, 356/601, 356/603
• US Class Current: 382/154
• CPC Class Codes: G06T 2207/10021 Stereoscopic video; Stereoscopic image sequence
• CPC Class Codes: G06T 2207/30108 Industrial image inspection
• CPC Class Codes: G06T 7/246 using feature-based methods, e.g. the tracking of corners or segments

Abstract

An instrument and method for measuring the time history of recession of an ablating surface of a test article during testing in a high enthalpy thermal test facility, such as an arcjet. The method advances prior art by providing time-history data over the full ablating surface without targets and without any modifications to the test article. The method is non-intrusive, simple to implement, requires no external light source, and does not interfere with normal operations of the arcjet facility.

Claims

1. A system for measuring recession of an ablative surface during testing in an arcjet facility, the system comprising:

(1) at least first and second cameras, positioned in or adjacent to an arcjet facility so that each camera views an ablating surface of a test article, having an arbitrary shape, from a different direction, and so that each of the at least first and second cameras acquires time-synchronized images of the ablating surface at a sequence of spaced apart imaging times during which the ablating surface is exposed to flow of a heated fluid in the arcjet facility and thereby undergoes ablation;

(2) a calibration mechanism for providing camera calibration coefficients for each of the at least first and second cameras by imaging a three dimensional calibration object and determining approximate transformations between two dimensional image-plane coordinates and three-dimensional physical object-space coordinates;

(3) a three dimensional surface grid of nodes that conforms to an initial shape of the ablating surface, to define measurement points on the ablating surface; and

(4) a computer that is programmed;

(a) to define image-plane coordinates for corresponding measurement points for each of the at least first and second cameras by mapping the nodes of the surface grid from the physical object-space coordinates to the image-plane coordinates for each of the at least first and second cameras;

(b) to track measurement points from each of the at least first and second cameras for the sequence of imaging times; and

(c) to compute the physical object-space coordinates of each measurement point from the image-plane coordinates and the camera calibration coefficients for the at least first and second cameras, to thereby estimate recession of the ablating surface.

2. The system according to claim 1, wherein said images of said ablating surface are acquired by a process comprising fitting said at least first and second cameras with band-pass interference filters to improve at least one of sharpness and contrast of said images by eliminating chromatic aberration.

3. The system according to claim 1, wherein said initial shape of said ablating surface is at least one of a portion of a plane, a portion of a sphere and a portion of a cylinder.

4. The system according to claim 1, wherein no targets and no fiducial marks are provided for said ablating surface, and appearance of the ablating surface changes continually as ablation proceeds.

5. The system according to claim 1, wherein said measurement points are tracked for said first camera by defining a small, rectangular interrogation window, centered on each of said measurement points, and providing high-pass filtering of image intensity data within the window.

6. The system according to claim 5, wherein said step of tracking said measurement points is accomplished for said first camera by successive cross correlation of filtered image intensity data within said small interrogation window centered on each measurement point.

7. The system according to claim 1, wherein said computer is further programmed to track said measurement points for said second camera by applying independent global, de-warp transformations to images from said first camera and from said second camera before performing cross correlation between said first and second cameras.

8. The system according to claim 1, wherein said computer is further programmed to track said measurement points for said second camera by applying a different, local, de-warp transformation to image data from said first and second cameras at each measurement point before performing cross correlation between said first and second cameras, where the local de-warp transformation approximates a view of said ablating surface as seen from a point on a line perpendicular to said ablating surface at said measurement point, and a local transformation is applied only to a portion of said image that is within said interrogation window.

9. The system according to claim 1, wherein said computer is further programmed to track said measurement points by constraining each of said measurement points to remain at a fixed (x,y) location in said physical object-space.