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RUDRSTOP - Rudder Right Piro Stop Gain
Menu items
Description
60 - 180
(Default 100)
The sensitivity of hovering and clockwise spin. The stop speed used for preventing the side wind,
hovering shift and clockwise rotation.
Suggestion
The sensitivity is RUDRSTOP*TAILGAIN when the hovering and clockwise rotation stop. If the
ability to prevent side wind is poor, hovering drifts rightward, or slow clockwise tail rotation
stopping speed, increase the RUDRSTOP value. If the tail rebounds when stopping, on clockwise
tail rotation, decrease the RUDRSTOP value. This value should not be varied greatly in any one
instance.
RUDD-ACC - Rudder Accelerate Delay
Menu items
Description
0 - 15
(Default 0)
The higher the value, the longer it takes to reach the required Piro speed from stationary.
Suggestion
Increase RUDD-ACC on lag tail.
RUDD-DEC - Rudder Decelerate Delay
Menu items
Description
0 ~ 15
(Default 0)
The higher the value, the longer it takes for the tail to slow down. Used to smooth the deceleration
of a piro when coming to a stop.
Suggestion
Increase RUDD-DEC on rebounded tail.
RUDD-EXP - Rudder Stick Expo Curve
Menu items
Description
-100 - +100
(Default 0)
Rudder expo curve relative to stick input.
RUD-SENS - Rudder Stick sensitive
Menu items
Description
50 - 150
(Default 100)
Fine tune the stick response to the actual piro rate. The higher the setting, the more sensitive the
stick movement.
9: TAIL TORQUE COMP
Submenu Configuration Steps
PIT-COMP - Compensation of Collective Pitch to Tail Rotor
Item
Description
-100 - +100
(Default 0)
A change in collective pitch will cause a change in the head speed of the main rotor, as well as
causing a tail deviation. Adjust the
PIT-COMP
value until this torque change can be offset
completely. If the torque change causes tail deviation counter-clockwise, compensate with
rightward rudder direction input, i.e. compensate reversely rudder direction input.
Identification of
Compensation
Direction
Turn off brushless motor power or engine throttle, push the collective pitch stick, adjust PIT-
COMP value, check if the compensation direction of collective pitch to tail rotor is correct.