G5 Electronic Flight Instrument Pilot's Guide for Non-Certified Aircraft
190-02072-00 Rev. G
76
Additional Features
System Overview
Flight Instruments
AFCS
Additional F
eatur
es
Index
Once engaged, the torque applied by ESP is at its maximum when bank angle is
15º more than the configured bank limit, and tapers to the minimum applied torque
when the bank angle is 15º less than the configured bank limit. The force increases
as roll attitude increases and decreases as roll attitude decreases. The applied force is
intended to encourage pilot input to return the airplane to a more normal roll attitude.
When beyond 15º of the configured bank limit, the maximum torque is held until the
aircraft returns inside the protected envelope.
Figure 4-4 ESP Roll Operating Range When Engaged
(Force Increases as Roll Increases & Decreases as Roll Decreases)
0º
10º
10º
20º
20º
30º
30º
45º
45º
60º
60º
75º
75º
90º
90º
Configured
Bank Limit
(45
º)
Minimum
ESP Torque
(30
º)
Maximum
ESP Torque
(60
º)
Maximum
ESP Torque
(60
º)
Minimum
ESP Torque
(30
º)
Configured
Bank Limit
(45
º)
4.1.2 PITCH ENGAGEMENT
ESP pitch engagement is configurable between 10º and 25º nose-up and between
5º and 25º nose-down. Once engaged, the torque applied by ESP is at its maximum
when pitch is 5º more than the configured nose-up and nose-down pitch limits, and
tapers to the minimum applied torque when pitch is 5º less than the configured nose-
up and nose-down pitch limits. When beyond 5º of the configured pitch limit, the
maximum torque is held until the aircraft returns inside the protected envelope.
The opposing force increases or decreases depending on the pitch angle and the
direction of pitch travel. This force is intended to encourage movement in the pitch axis
in the direction of the normal pitch attitude range for the aircraft.
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