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.