| 摘要 |
The invention concerns a method for measuring a shape anomaly (6) on an aircraft structural panel, including the following operations: projecting a target pattern at the site of the anomaly (6) on the panel (5); producing at least two images of said projected pattern; processing said two images by stereocorrelation to obtain measurements of the anomaly. The invention also concerns a system for implementing said method, comprising: a projecting device (3) for projecting a target pattern at the site of the anomaly (6) on the panel (5); at least two imaging devices (2a, 2b) for producing each an image of the target pattern; and means for processing said target pattern images. |
