USER MANUAL
INTEL® FALCON™ 8+ UAS
© 2017 Intel Corporation. All rights reserved 153
Flight Controller Screen
Shows an overview of two Trinity flight controller
modules (NAV1 and NAV2). The third flight con-
troller (PER - peripheral processor) is monitoring
these two. In flight, one controller is active and
displayed as redundant. As soon as the third one
detects an issue, it will switch to NAV2 and give an
acoustic and optical warning.
NAV1 = 1st Trinity flight controller module (navi-
gational processor 1).
NAV2 = 2nd Trinity flight controller module (navi-
gational processor 2).
Mode = Current mode of the NAV1 and NAV2
Trinity modules.
ACTV = NAV1 is active.
STBY = NAV2 is in standby.
ALL OKAY = No issues detected by the system.
REDUND = No issues detected by the system and
the flight controllers are working redundantly.
OK = Status line. This is the same informa-
tion as on the Main Screen.
Error Message Screen (optional)
This screen is only displayed if there are system
warnings. In this case the status line will show
<- Check Msg.
In “AscTec Trinity Control Unit System Warnings”
on page 129, you will find detailed descriptions
and a list of possible system warnings.
N1C:n´t fly home - (= can’t fly home) warn-
ing from 1st Trinity flight controller (no GPS sig-
nal and
Goto Home activated).
N2C:n´t fly home - (= can’t fly home) warn-
ing from 2nd Trinity flight controller (no GPS sig-
nal and Goto Home activated).
<- Check Msg in status line. Shown whenever
there is a system warning.
Figure 4.2: Main Information Screens (Continued)
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