COMPLEX RADIO CONTROL SYSTEM
absolutely parallel to the axis of ailerons and the elevator. Sensor
trims are applied in the flight modes where the horizon is stabilised
Maximum pitch angle - definition of the maximum possible tilt
angle in horizon stabilisation mode (controlled by elevator input).
Sensor trim (Roll/Pitch) – using these parameters you can fine
tune the receiver position in the model if its position is not
6.1. PID control setting
6.2. "Stabilise" mode setting
Aileron/Roll rate, Elevator/Pitch rate, Rudder/Yaw rate - in this
section you set the individual PID control coefficients for each axis
separately for multicopter models. These coefficients are applied in
all flight modes to stabilise the rotational speed around each axis.
Minimum pitch angle - definition of the minimum possible tilt
angle in horizon stabilisation mode (controlled by elevator input).
PID transition delay - used to switch between flight modes that
use stabilisation with different gains of the PID coefficients. This
feature guarantees that the change of the coefficients does not
cause erratic behavior in flight.
aileron input).
Aileron/Roll angle, Elevator/Pitch angle, Rudder/Yaw angle -
here you can change the proportional gain of attitude stabilisation,
e.g. horizon. The higher the coefficients you specify, the faster the
model is reoriented to the new attitude.
Maximum roll angle - defines the maximum possible tilt angle to
the left and right in the horizon stabilisation mode (controlled by
Vertical Speed - PID coefficients to stabilise the climb and descent
rate.
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