WEBVTT

00:01.630 --> 00:04.080
Hi , my name is Jessica Peterson . I'm

00:04.080 --> 00:06.191
a flight test engineer at Edwards Air

00:06.191 --> 00:08.358
Force Base where we do flight tests on

00:08.358 --> 00:10.469
new systems for the Air Force . Today

00:10.469 --> 00:12.247
I'm gonna talk to you about the

00:12.247 --> 00:14.302
automatic ground collision avoidance

00:14.302 --> 00:16.610
system , how we tested it and the lives

00:16.610 --> 00:17.888
that have been saved .

00:20.450 --> 00:22.506
Alright , so I want to talk to you a

00:22.506 --> 00:24.728
little bit about Edwards Air Force Base

00:24.728 --> 00:24.720
and the things that have been done

00:24.720 --> 00:27.800
there . Edwards is the premier location

00:27.800 --> 00:29.856
for flight test and we have a really

00:29.856 --> 00:31.689
rich history of things that have

00:31.689 --> 00:33.911
happened . A couple I want to highlight

00:33.911 --> 00:33.560
because they're related to some of the

00:33.560 --> 00:35.727
schools here in the antelope valley is

00:35.727 --> 00:38.760
joe walker . He was an X 15 pilot and

00:38.760 --> 00:41.240
he received his astronaut wings by

00:41.240 --> 00:44.310
taking the X 15 to very very high

00:44.310 --> 00:46.532
altitudes , joe walker middle school is

00:46.532 --> 00:49.540
named after him . The other X 15 pilot

00:49.550 --> 00:51.880
is Pete Knight . So Pete Knight still

00:51.880 --> 00:54.160
holds the record for the fastest manned

00:54.160 --> 00:57.750
flight in the X 15 . He went mach 6.72

00:57.760 --> 01:00.230
which is 6.72 times faster than the

01:00.230 --> 01:02.119
speed of sound . So both . Pretty

01:02.119 --> 01:04.230
amazing . Night . High school in East

01:04.230 --> 01:06.452
Palmdale is named after Pete night . So

01:06.452 --> 01:08.452
if any kids from joe walker or from

01:08.452 --> 01:10.508
high school are listening , you guys

01:10.508 --> 01:12.452
are going to a school that's named

01:12.452 --> 01:15.400
after historical legends . So a little

01:15.400 --> 01:17.622
bit of my background . I grew up in the

01:17.622 --> 01:19.344
antelope valley went to courts

01:19.344 --> 01:21.456
elementary , joe walker middle school

01:21.456 --> 01:23.622
and quartz Hill High school . In order

01:23.622 --> 01:25.456
to do my job I had to go and get

01:25.456 --> 01:27.622
engineering degrees . So I went to cal

01:27.622 --> 01:29.400
poly san luis Obispo and got an

01:29.400 --> 01:31.233
engineering degree in mechanical

01:31.233 --> 01:33.456
engineering . After that I decided that

01:33.456 --> 01:35.678
I wanted to get even more knowledge and

01:35.678 --> 01:37.733
I wanted to specialize in mechanical

01:37.733 --> 01:40.030
engineering and flight control systems .

01:40.040 --> 01:42.410
So I went and got a masters of science

01:42.420 --> 01:44.587
in mechanical engineering at the naval

01:44.587 --> 01:46.960
postgraduate school . I've been working

01:46.960 --> 01:49.660
at Edwards since 2005 and I've worked

01:49.660 --> 01:51.882
on a lot of different programs . One of

01:51.882 --> 01:54.080
them is the RQ four which is an

01:54.090 --> 01:57.390
unmanned vehicle that has the pilot on

01:57.390 --> 01:59.334
the ground flying with a mouse and

01:59.334 --> 02:01.780
keyboard . The other is the F 16 and

02:01.780 --> 02:04.002
the automatic systems . And that's what

02:04.002 --> 02:06.169
I'm gonna tell you about today . I got

02:06.169 --> 02:08.360
to go to test pilot school in 2017 and

02:08.360 --> 02:10.471
with that it has allowed me to fly in

02:10.471 --> 02:12.193
the backseat of many different

02:12.193 --> 02:14.416
airplanes . You can see a picture of me

02:14.416 --> 02:16.582
here with a T . 38 that has my name on

02:16.582 --> 02:18.850
the canopy rail which is pretty cool to

02:18.850 --> 02:22.650
have . Alright

02:22.660 --> 02:24.660
so what does it take to be a flight

02:24.660 --> 02:26.800
test engineer ? Well in addition to

02:26.800 --> 02:29.022
have the engineering degree , there's a

02:29.022 --> 02:31.244
lot of training that you have to do and

02:31.244 --> 02:33.522
so one of them is the altitude chamber .

02:33.522 --> 02:35.633
So if you're flying in an airplane up

02:35.633 --> 02:38.790
at say 30,000 ft , one of the things

02:38.790 --> 02:41.012
one of the issues that you have is that

02:41.012 --> 02:43.600
there isn't very much oxygen and so if

02:43.600 --> 02:45.810
the mask that you're wearing or the

02:45.810 --> 02:48.580
canopy doesn't work correctly , you're

02:48.580 --> 02:50.840
not gonna have enough oxygen . And so

02:50.840 --> 02:53.830
they train you how to identify if you

02:53.830 --> 02:56.070
don't have enough oxygen by putting you

02:56.070 --> 02:58.181
in a chamber on the ground where they

02:58.181 --> 03:00.880
start to remove the oxygen . The other

03:00.880 --> 03:03.047
thing type of training we do is called

03:03.047 --> 03:05.680
the center fuge . So everyone here I

03:05.680 --> 03:07.847
want you to think , have you ever been

03:07.847 --> 03:10.270
on a roller coaster and felt the force

03:10.280 --> 03:13.090
on your body on a roller coaster ? That

03:13.090 --> 03:15.500
same thing happens in an airplane . And

03:15.500 --> 03:17.970
so if the airplane is turning , you can

03:17.970 --> 03:21.530
pull what are called G forces . So nine

03:21.540 --> 03:24.890
Gs , which is what the F 16 can pull is

03:24.890 --> 03:28.490
nine times the force of gravity . Well ,

03:28.490 --> 03:30.712
the problem with that is that if you're

03:30.712 --> 03:33.360
pulling G forces it will pull the blood

03:33.370 --> 03:35.592
from your brain . And so you have to be

03:35.592 --> 03:37.980
trained on how to push that blood and

03:37.980 --> 03:40.400
keep it in your brain . It's called a G

03:40.400 --> 03:43.540
strain . I also had to learn survival .

03:43.550 --> 03:45.870
So if I have to eject from an airplane ,

03:45.880 --> 03:48.260
I have to know how to use my parachute

03:48.270 --> 03:50.470
and how to survive on the water or the

03:50.470 --> 03:54.310
land . All right , I'm

03:54.310 --> 03:56.254
gonna tell you about the automatic

03:56.254 --> 03:58.510
ground collision avoidance system , a

03:58.510 --> 04:00.677
system that I've been able to test and

04:00.677 --> 04:03.980
fly on for several years . One

04:03.980 --> 04:06.202
important thing to understand about the

04:06.202 --> 04:08.940
F 16 is that it has a low level mission ,

04:09.140 --> 04:11.300
meaning that the pilots will fly very

04:11.300 --> 04:13.411
close to the ground somewhere between

04:13.411 --> 04:16.190
200 to 500 ft , going very fast . They

04:16.190 --> 04:18.720
do this for terrain masking so that sir

04:18.895 --> 04:21.345
radars can't see them . It means they

04:21.345 --> 04:23.234
hide next to mountains and in the

04:23.234 --> 04:25.012
canyons . This can make it very

04:25.012 --> 04:27.015
challenging for a ground collision

04:27.015 --> 04:28.959
avoidance system because it has to

04:28.959 --> 04:31.605
allow the pilots to still fly close to

04:31.605 --> 04:33.827
the ground without getting in the way .

04:35.990 --> 04:37.830
So how does the automatic ground

04:37.830 --> 04:40.108
collision avoidance system work ? Well ,

04:40.108 --> 04:42.163
it performs an automatic recovery to

04:42.163 --> 04:44.219
avoid the ground when a collision is

04:44.219 --> 04:46.460
predicted , What this means is the

04:46.460 --> 04:48.630
system , the computer knows where the

04:48.630 --> 04:51.350
airplane is , what the flight path is ,

04:51.350 --> 04:53.406
so how it would look if the airplane

04:53.406 --> 04:55.517
does a recovery and where the terrain

04:55.517 --> 04:57.628
is , it knows Where the mountains are

04:57.628 --> 04:59.850
and where the Valleys are . And then it

04:59.850 --> 05:01.517
does a prediction that if the

05:01.517 --> 05:03.517
airplane's flight path will hit the

05:03.517 --> 05:05.572
mountain , that is when the computer

05:05.572 --> 05:07.794
will come on . We feel that this system

05:07.794 --> 05:09.739
back in 2014 and since then it has

05:09.739 --> 05:12.300
saved 12 pilots lives . I'm gonna show

05:12.300 --> 05:14.430
you one video of a pilot's life that

05:14.430 --> 05:17.850
was saved . So saving lives . Before we

05:17.850 --> 05:20.017
fielded the system , we did a study in

05:20.017 --> 05:23.590
12 years , there were 86 pilots , 156

05:23.600 --> 05:26.530
aircraft that related to $3.7 billion

05:26.530 --> 05:30.810
called-controlled

05:30.810 --> 05:33.205
flight into terrain or Collision with

05:33.205 --> 05:35.685
another airplane . The automatic ground

05:35.685 --> 05:37.907
collision avoidance system first tested

05:37.907 --> 05:40.175
on the F16 , which I got to work on and

05:40.175 --> 05:42.335
then put on other airplanes was

05:42.335 --> 05:44.865
projected to save 1-2 pilots per year .

05:45.025 --> 05:47.136
Since we fielded this system has been

05:47.136 --> 05:49.330
12 pilots lives that have been saved .

05:50.840 --> 05:53.760
So how do you safely test an automatic

05:53.760 --> 05:55.649
ground collision avoidance system

05:55.649 --> 05:57.816
without actually causing a collision ?

05:58.700 --> 06:00.811
The way that we did this is we put in

06:00.811 --> 06:03.033
something we call the terrain clearance

06:03.033 --> 06:04.978
buffer , meaning that we faked the

06:04.978 --> 06:07.144
computer to think that the terrain was

06:07.144 --> 06:09.440
higher than it actually was . This was

06:09.440 --> 06:12.560
important because we didn't want the

06:12.570 --> 06:14.570
airplane to hit the mountain if the

06:14.570 --> 06:18.220
system didn't work correctly . So

06:18.220 --> 06:20.260
now I'm gonna show you a test point

06:20.270 --> 06:22.270
what this looks like first . Let me

06:22.270 --> 06:24.690
talk you through the maneuver . So the

06:24.690 --> 06:28.120
pilot is going to start up at 43,000 ft .

06:28.140 --> 06:29.918
They're gonna roll the airplane

06:29.950 --> 06:33.910
inverted , pull very steep , nose low

06:33.910 --> 06:35.966
towards the ground and they're gonna

06:35.966 --> 06:38.820
try to get to 630 knots with the

06:38.830 --> 06:40.960
airplane almost vertical , going

06:40.960 --> 06:44.040
straight down And letting the nose fall .

06:44.050 --> 06:46.980
We expect the system to activate at

06:46.990 --> 06:49.800
33,000 ft and the computer to take

06:49.800 --> 06:52.370
control and maneuver away . Let's see

06:52.370 --> 06:55.720
what that looks like . So as an

06:55.730 --> 06:58.130
engineer , we would create a test card

06:58.140 --> 07:00.800
and this test card would tell the pilot ,

07:00.810 --> 07:03.040
not just the conditions like the

07:03.050 --> 07:05.550
altitude and the air speed , but also

07:05.550 --> 07:07.720
the computer settings . Remember how I

07:07.720 --> 07:09.664
talked about the terrain clearance

07:09.664 --> 07:11.498
buffer that would make it to the

07:11.498 --> 07:13.720
computer thought the terrain was higher

07:13.720 --> 07:15.609
for this test point . We put in a

07:15.609 --> 07:18.000
terrain clearance buffer of 6600 ft ,

07:18.010 --> 07:19.843
meaning the computer thought the

07:19.843 --> 07:21.954
terrain was higher than that . And so

07:21.954 --> 07:24.177
that's how we know when the computer is

07:24.177 --> 07:27.600
supposed to activate . So I'm gonna

07:27.600 --> 07:30.340
show you a heads up display of a test

07:30.340 --> 07:32.451
point and I'm gonna show you multiple

07:32.451 --> 07:34.451
heads up displays . So first let me

07:34.451 --> 07:36.673
talk through what you're gonna see when

07:36.673 --> 07:38.673
the airplane is starting at level .

07:38.673 --> 07:40.784
You're gonna see a flight path marker

07:40.784 --> 07:43.770
above the horizon . What that looks

07:43.770 --> 07:45.980
like is a flight path marker above a

07:45.980 --> 07:49.110
solid line . You're gonna see current G ,

07:49.200 --> 07:52.610
the airspeed , the altitude and in the

07:52.610 --> 07:54.277
height above the ground . The

07:54.277 --> 07:56.499
difference between the height above the

07:56.499 --> 07:58.666
ground and the altitude . In this case

07:58.666 --> 08:02.170
it's about 5500 ft . That is the height

08:02.180 --> 08:04.347
of the terrain . So the mountain below

08:04.347 --> 08:08.210
you . When the pilot

08:08.210 --> 08:10.377
starts to roll inverted what that will

08:10.377 --> 08:12.720
look like in the hud is a flight path

08:12.720 --> 08:16.200
marker will start moving to turn

08:16.210 --> 08:19.810
to go inverted . Once

08:19.810 --> 08:22.032
inverted , you will see the flight path

08:22.032 --> 08:24.430
marker below the horizon and here is

08:24.440 --> 08:27.620
10° nose low corresponding to this

08:27.620 --> 08:31.570
position . Next the

08:31.570 --> 08:34.110
airplane will get very steep , very

08:34.110 --> 08:36.990
nose low and you'll see auto G cast

08:37.000 --> 08:39.056
starting to think about activating .

08:39.056 --> 08:41.000
These are called the auto G cast .

08:41.000 --> 08:43.130
Chevron's when they touch is when the

08:43.130 --> 08:44.500
maneuver will occur

08:47.410 --> 08:49.910
at the auto G CASS activation . You'll

08:49.910 --> 08:52.360
see a break X . So the chevron's come

08:52.360 --> 08:54.700
together and the word fly up , you'll

08:54.710 --> 08:58.100
also hear a solid tone and the word fly

08:58.100 --> 09:01.990
up will be flashing when the

09:01.990 --> 09:04.840
maneuver is complete , the chevron's

09:04.850 --> 09:07.017
will go away and you'll see the flight

09:07.017 --> 09:08.850
path marker getting close to the

09:08.850 --> 09:09.460
horizon .

09:12.880 --> 09:14.824
Alright , so let's watch this test

09:14.824 --> 09:16.436
point and see how it works .

09:17.830 --> 09:19.770
451.45

09:25.730 --> 09:27.620
pulling no slow

09:31.000 --> 09:33.300
here you can see these very steep ,

09:34.290 --> 09:37.870
there's the auto details activation is

09:37.870 --> 09:39.250
now in the fall

09:41.430 --> 09:43.970
altitude altitude

09:51.550 --> 09:55.420
control . So

09:55.420 --> 09:57.531
maneuver complete good data . We look

09:57.531 --> 09:59.642
at data and then be able to clear him

09:59.642 --> 10:01.642
to the next condition . So that's a

10:01.642 --> 10:05.060
success . So testing doesn't always go

10:05.060 --> 10:07.227
as we expected . So now I'm gonna show

10:07.227 --> 10:09.338
you another condition where we tested

10:09.338 --> 10:11.560
and we found a system failure . So this

10:11.560 --> 10:14.230
is the same test point as before . But

10:14.230 --> 10:16.350
in this scenario the computer is not

10:16.350 --> 10:18.517
able to process the information and it

10:18.517 --> 10:20.430
fails . Meaning auto G cast isn't

10:20.430 --> 10:22.597
working . What you're going to hear on

10:22.597 --> 10:24.541
the radio is you're gonna hear the

10:24.541 --> 10:26.652
control room saying abort abort abort

10:26.652 --> 10:28.874
and then the pie having to manually fly

10:28.874 --> 10:31.097
the airplane because the computer isn't

10:31.097 --> 10:33.319
working . The other thing you'll see is

10:33.319 --> 10:35.430
in the heads up display the words NOg

10:35.430 --> 10:37.445
CASS . I want you to note that the

10:37.445 --> 10:39.615
pilot doesn't realize the system has

10:39.615 --> 10:41.837
failed because he's flying the airplane

10:41.837 --> 10:44.004
until after the control room calls the

10:44.004 --> 10:46.171
aboard aboard aboard . This means that

10:46.171 --> 10:48.226
we have good teamwork and one of the

10:48.226 --> 10:50.393
reasons that we use a control room for

10:50.393 --> 10:52.615
flight test . Let's watch the video . 6

10:52.615 --> 10:56.260
30 x 34 . What has

10:56.260 --> 10:57.260
happened

11:00.950 --> 11:03.230
again ? Pulling those low

11:07.760 --> 11:08.320
here ,

11:15.860 --> 11:18.410
altitude , altitude

11:22.050 --> 11:24.272
and that's where the pilot realizes the

11:24.272 --> 11:27.710
system has failed . So that also is a

11:27.710 --> 11:29.877
good test point . We found the failure

11:29.877 --> 11:32.099
and then we were able to go back in and

11:32.099 --> 11:34.154
fix the system so that would protect

11:34.154 --> 11:37.310
the pilots in all conditions . Alright ,

11:37.310 --> 11:39.421
now I'm gonna show you where this all

11:39.421 --> 11:41.532
comes together . So this is after the

11:41.532 --> 11:43.643
system was fielded and put on all the

11:43.643 --> 11:45.700
operational F 16 . There was a new

11:45.700 --> 11:48.560
pilot in training that was having a bad

11:48.560 --> 11:51.160
day , did not do a good G strain and

11:51.160 --> 11:54.020
passes out in the airplane as he has

11:54.020 --> 11:56.580
passed out . His airplane gets steeper

11:56.580 --> 11:58.850
and steeper , looking very similar to

11:58.850 --> 12:01.120
the test points that you just saw the

12:01.120 --> 12:03.880
airplane will do an automatic maneuver

12:03.890 --> 12:05.779
and recover the aircraft from the

12:05.779 --> 12:07.668
ground . Now , what I want you to

12:07.668 --> 12:09.668
listen for is on the radio , you're

12:09.668 --> 12:12.260
gonna hear the words recover recover

12:12.270 --> 12:14.360
and that is the pilot's wingman in

12:14.360 --> 12:16.680
another airplane yelling at him over

12:16.680 --> 12:19.170
the radio trying to save his life .

12:19.190 --> 12:20.523
Let's watch the video .

12:36.020 --> 12:39.220
So right here coloring five Gs , six Gs

12:39.230 --> 12:41.840
eight Gs , you hear his G strain and

12:41.840 --> 12:43.951
now he's passed out . The airplane is

12:43.951 --> 12:47.780
getting steeper and steeper faster .

12:51.940 --> 12:53.107
That was a sweet man

12:57.230 --> 12:57.820
after

13:07.910 --> 13:08.910
knock it off .

13:12.150 --> 13:13.550
You get yourself back .

13:20.990 --> 13:23.590
So you saw how auto G cast saved that

13:23.590 --> 13:25.479
pilots lives . We got to meet him

13:25.479 --> 13:27.646
afterwards actually he came to Edwards

13:27.646 --> 13:29.868
Air Force Base and he told us that when

13:29.868 --> 13:31.757
he woke up and heard that tone he

13:31.757 --> 13:33.868
thought it was the alarm going off in

13:33.868 --> 13:36.034
his bed . I want to close with showing

13:36.034 --> 13:38.220
you how hard it is to ride that line

13:38.230 --> 13:40.490
between being able to save pilots lives

13:40.490 --> 13:42.490
by not hitting the ground but still

13:42.490 --> 13:44.379
allowing them to do them a normal

13:44.379 --> 13:46.434
maneuver . This is called a straight

13:46.434 --> 13:48.490
run and this is where the pilot uses

13:48.490 --> 13:50.712
the nose of the airplane , the point at

13:50.712 --> 13:52.934
the ground so they can shoot bullets at

13:52.934 --> 13:55.268
things on the ground . In this maneuver ,

13:55.268 --> 13:57.434
the pilot needs to go all the way down

13:57.434 --> 13:59.490
to 90 ft above the ground and auto-G

13:59.490 --> 14:01.434
cast is not supposed to activate .

14:01.434 --> 14:03.657
You'll see in the video . The chevron's

14:03.657 --> 14:06.070
get very close with auto Gps thinking

14:06.070 --> 14:08.014
that it needs to activate but they

14:08.014 --> 14:10.126
never touch and the system never gets

14:10.126 --> 14:12.181
in the way and so that's the perfect

14:12.181 --> 14:14.403
balance between being nuisance free and

14:14.403 --> 14:17.220
preventing collisions here . You see

14:17.220 --> 14:18.610
the pilot turning in

14:21.130 --> 14:22.700
36 drive

14:38.280 --> 14:40.390
So all the way down to 90 ft . The

14:40.390 --> 14:41.779
system never activated .

14:45.690 --> 14:47.912
So in closing thoughts , it's been very

14:47.912 --> 14:49.968
rewarding . Working on the collision

14:49.968 --> 14:52.023
avoidance systems , you can see with

14:52.023 --> 14:54.079
engineering , how we learn about the

14:54.079 --> 14:54.020
system , put in different numbers to

14:54.020 --> 14:56.076
keep ourselves safe and then back up

14:56.076 --> 14:58.298
the pilot by watching parameters in the

14:58.298 --> 15:00.353
control room and in the aircraft . I

15:00.353 --> 15:02.520
hope you enjoyed learning about flight

15:02.520 --> 15:04.576
test and learning a little bit about

15:04.576 --> 15:04.560
collision avoidance . Thanks .

