WEBVTT FILE 1 00:00:04.238 --> 00:00:06.740 The OSIRIS-REx mission is an asteroid sample return mission 2 00:00:06.740 --> 00:00:10.844 and the main goal is to collect 60 grams of pristine sample from 3 00:00:10.844 --> 00:00:15.015 the surface of the near-Earth asteroid Bennu. Bennu’s rocky 4 00:00:15.015 --> 00:00:18.418 surface presented a challenge for the original LIDAR-based 5 00:00:18.418 --> 00:00:22.623 approach to the Touch-and-Go sample acquisition event. As an 6 00:00:22.623 --> 00:00:25.692 alternative, the project developed an onboard, optical 7 00:00:25.692 --> 00:00:31.198 based approach called Natural Feature Tracking. NFT requires 8 00:00:31.198 --> 00:00:34.735 detailed, 3-dimensional maps of the surface of Bennu. In order 9 00:00:34.735 --> 00:00:37.504 to build those 3-dimensional maps, we needed many many images 10 00:00:37.504 --> 00:00:41.408 of particular patches of the surface on Bennu itself. So, all 11 00:00:41.408 --> 00:00:44.645 these surveys that we’ve done throughout the mission have been 12 00:00:44.645 --> 00:00:47.080 at distances between several kilometers from the asteroid, 13 00:00:47.080 --> 00:00:49.683 down to just a few hundred meters from the surface. And 14 00:00:49.683 --> 00:00:51.618 based on those different perspectives and what the 15 00:00:51.618 --> 00:00:55.122 shading of the terrain is, it is possible to build a 3D model. 16 00:00:55.122 --> 00:00:58.058 Very similar to how we have two eyes that allow us to have depth 17 00:00:58.058 --> 00:01:01.495 perception of what we see, NFT requires multiple features 18 00:01:01.495 --> 00:01:06.133 across the field of view to have a depth perception. The original 19 00:01:06.133 --> 00:01:09.970 TAG accuracy requirement was to touch the surface within a 20 00:01:09.970 --> 00:01:13.507 50-meter diameter circle. Based on Bennu’s rough surface, our 21 00:01:13.507 --> 00:01:16.577 actual performance has to be much better than that, at 22 00:01:16.577 --> 00:01:20.047 10-meters or less. And even within that 10-meter area, there 23 00:01:20.047 --> 00:01:23.984 could be smaller, localized hazards that may damage the 24 00:01:23.984 --> 00:01:26.920 spacecraft. Right now, we are working on a flight software 25 00:01:26.920 --> 00:01:31.458 patch to help us avoid hazards as we come in for our sample 26 00:01:31.458 --> 00:01:33.827 event. When we do Natural Feature Tracking, that is all 27 00:01:33.827 --> 00:01:36.663 autonomous onboard the spacecraft – where we load the 28 00:01:36.663 --> 00:01:39.733 features, or a catalog to the spacecraft – so we are telling 29 00:01:39.733 --> 00:01:42.569 it where we expect these features to be. So, as the 30 00:01:42.569 --> 00:01:45.539 spacecraft makes its progress down to taking the sample, we’re 31 00:01:45.539 --> 00:01:48.241 recording images and then locating those landmarks to make 32 00:01:48.241 --> 00:01:51.411 sure we’re on the right track. And if there are any issues with 33 00:01:51.411 --> 00:01:54.614 the trajectory or we see landmarks where we shouldn’t, we 34 00:01:54.614 --> 00:01:57.651 know something’s up and we can back away and wave off the 35 00:01:57.651 --> 00:02:00.587 attempt and try again.