computer radio control system
steps, as the model might begin to oscillate very quickly.
When testing the modified coefficients, take off and apply small but
fast movements on the inputs and check if the multicopter reacts
quickly, but without overshots. The rudder axis (Yaw) is not so
critical for fine tuning the gain - after moving a stick in yaw
direction, the multicopter should not become unstable and should
not experience significant changes in altitude. Leave the derivative
coefficient at zero.
For multicopter models, the altitude and climb/descent stabilizati-
on can also be tuned. If the model responds more violently than
expected to the climb command, lower the proportional
coefficient in the appropriate row (Vertical Speed). Conversely, if it
does not respond to the altitude change at all, increase the
coefficient value.
4.2.2 Choice of flight modes
Depending on your preferences,
choose which flight modes to use
during flight - a total of 5 are available,
switching between three is available
(see the Description of flight modes
section).
For each flight mode, you can set the default gain (this multiplies
the proportional, integral and derivative coefficients in all axes),
and you can specify whether you want to use gain tuning via special
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