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A photogrammetric on-orbit inspection for orbiter thermal protection system

机译:轨道热防护系统的摄影测量在轨检查

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摘要

Due to the Columbia Space Shuttle Accident of February 2003, the ColumbiaAccident Investigation Board determined the need for an on-orbit inspection systemfor the Thermal Protection System that accurately determines damage depth to 0.25". NASA contracted the Spacecraft Technology Center in College Station, Texas, for aproof-of-concept photogrammetric system. This system involves a high quality digitalcamera placed on the International Space Station, capable of taking high fidelityimages of the orbiter as it rotates through the Rendezvous Pitch Maneuver. Due tothe pitch rotation, the images are tilted at different angles. The tilt causes the damageto exhibit parallax between multiple images. The tilted images are therefore registeredto the near-vertical images using visually striking features on the undamaged surfaceof the Thermal Protection System that appear in multiple images taken at differenttilt angles. The images become relatively oriented after registration, and features inone image are ensured to lie on the epipolar line in the other images. Features thatdo not lie on the undamaged surface, however, are shifted in the tilted images. Thesepixels are matched to the near-vertical image using a sliding-window area-matchingapproach. The windows are matched using a least-squares error method. The changein location for a pixel in a tilted image from its expected location on the undamagedsurface is called the pixel disparity. This disparity is linearly scaled using the tiltangle and the pixel sampling to determine the depth of the damage at that pixel location. The algorithm is tested on a set of damaged tiles at the Johnson SpaceCenter in Houston and the photogrammetric damage depth is then compared to a setof truth data provided by NASA. The photogrammetric method shows promise, withthe 0.25" error limit being exceeded in only a few pixel locations. Once the cameraproperties are fully known from calibration, this systematic error should be reduced.
机译:由于2003年2月发生的哥伦比亚号航天飞机事故,哥伦比亚事故调查委员会确定了对热保护系统的在轨检查系统的需要,该系统可以精确确定损坏深度为0.25英寸。美国宇航局与德克萨斯州大学城的航天器技术中心签约,用于概念验证摄影测量系统的系统,该系统包括放置在国际空间站上的高质量数码相机,当其通过交会俯仰操纵旋转时,能够拍摄高保真度的图像,由于俯仰旋转,图像在倾斜会导致损坏在多张图像之间显示视差,因此,倾斜倾斜的图像会在热保护系统未损坏的表面上使用视觉上明显的特征对齐到近乎垂直的图像,这些特征出现在以不同倾斜角度拍摄的多张图像中。注册后相对定位,并且功能不一确保法师位于其他图像的对极线上。但是,未位于未损坏表面上的特征会在倾斜的图像中移动。使用滑动窗口面积匹配方法将这些像素匹配到近垂直图像。使用最小二乘误差法对窗口进行匹配。倾斜图像中的像素从其在未损坏表面上的预期位置的改变位置称为像素视差。使用倾斜角度和像素采样来线性缩放此视差,以确定该像素位置处的损坏深度。该算法在休斯敦的约翰逊航天中心的一组损坏的瓷砖上进行了测试,然后将摄影测量的损坏深度与NASA提供的一组真实数据进行了比较。摄影测量方法显示出希望,仅在几个像素位置就超过了0.25“的误差极限。一旦通过校准完全了解了相机的性能,就应该减少这种系统误差。

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    Gesting Peter Paul;

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  • 年度 2006
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