User's Manual

46
large value of travel is specified, when the sticks are moved at t he same time, the controls may bind or run
out of travel. Decrease the travel until no binding occurs.
Adjustability:
• Requires use of CH2 and CH4.
•
Independently adjustable travels allow for differences in servo travels.
• Rudder differential is not available. (To create rudder differential, set RUD1 and 2 to 0, then use two
programmable mixes, RUD-ELE and RUD-RUD, setting different percents for up and down. These are your
new rudder travels. Trim and l ink off, switch assignment null so you can’t accidentally turn off rudder.
3.3.11 ELEVON
ADJUSTABILITY:
•
Requires use of CH1 and CH2.
• Independently adjustable aileron t ravel allows aileron differential.
• Independently adjustable elevator travel allows for differences in up vs. down travel.
• The separate ELEVON settings for each condition can be set. (GLID only)
Note: When changing the polarit y of a rate, "change rate dir?" is displayed for a check. Please set up after
pressing DIAL for 1 second and canceling an alarm display. (GLID only)
Note: Be sure t o move the elevator and aileron sticks to full deflection during setup. If large t ravels are
specified, when the AILERON and ELEVATOR STICKS are moved at the same time t he controls may bind
or run out of travel.
Goals Steps Inputs
Activate
ELEVON.
Adjust aileron
down travel to
90% of up
travel, creating
aileron
differential.
Open ELEVON
to BASIC . again to ADVANCE
to ELEVON,
Activate the function.
to MIX,PUSH to ACT.
O
p
tional: ad
j
ust u
p
/down travel
se
p
aratel
y
for the servos as
ailerons.
(
Ex:down to 90%
)
to AIL1.PUSH. Aileron Stick. to 90%
to AIL2.PUSH. Aileron Stick. to 90%
Optional: adjust the elevator travel
of each servo.(Ex:right servos
elev. Travel to 98%, left to 105%.)
to ELE2.PUSH. to 98%.
to ELE1.PUSH. to 105%
Close
3.3.12 Gyro Sense
The gyros have two operations modes: GY mode and STD mode.
•
STD mode: This mode performs general proportional control operation. For instance, it controls the gyro so
that changes are countered when the attitude of the aircraft is changed by cross-wind, etc.
•GY mode: This mode performs both proportional and integrated control operation. The difference between
Normal mode and GY mode operation is that where as the Normal mode only counters changes in attitude,
the GY mode returns to the original controlled variable simultaneously with countering changes in attitude.
For example, during knife edge flying, aileron and elevator meeting rudder is normally necessary, but in the
GY mode, meeting rudder is performed automatically by the gyro.