Intel FALCON 8+ User Manual page 168

USER MANUAL
INTEL® FALCON™ 8+ UAS
Table 4.1: Status Display Menu Structure (Continued)
When the Fal-
32%
con F8 is
ing battery
switched on
capacity of the
and there is
CTR
already an
GPS
established
nal strength; at
connection
least four bars
with the CTR,
are required
after a few sec-
for flying in
onds the
GPS-Mode.
screen
Cam
changes to the
of the camera
Main Screen.
gimbal. Values
vary from
approx. -100°
to +100° (-90°
On this screen, means the
camera is
you will find
looking verti-
the following
information: cally down-
wards).
: Bat-
15.3V
tery voltage
level of the
UAV
After a few Here you must
seconds, the select the
screen mode deter-
changes to mining how
Link loss proc. the UAV will
behave in case
of a lost link.
For help
selecting the
mode, see
"LINK LOSS
PROCEDURE"
on page 116.
Pushing the RIGHT/LEFT arrow buttons in the Main Screen leads you to different
screens. For more information about these screens see "The Main Information
Screens" on page 178.
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: Remain-
Height
Barometrically
measured
height above
ground level
: GPS sig-
(0m = where
the propellers
are started).
Flighttime
The flight time
counter will
: Tilt angle
start when the
propellers are
switched on
and is updated
as soon as one
battery is
changed.
: Flight mode
G
(G, H, M, see
"FLIGHT
MODES" on
page 120)
After selecting
the appropri-
ate Link Loss
Procedure by
pushing ENT,
confirming the
screen
changes to the
Main Screen.
: : Counter of
0
triggers sent to
the camera.
: Status line.
OK
Everything is
OK with the
system. Other-
wise there will
: be the warn-
ing
<- Check
. In this
Msg
case press the
LEFT arrow
button 5 times,
until the Error
Message
Screen is
shown. see
"AscTec Trin-
ity Control
Unit System
Warnings" on
page 156.
168