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1
7
60 ~ 180
(Default 100)
The sensitivity of hovering and rightward spin. The stop speed used for preventing
the side wind, hovering shift and rightward spinning.
Suggestion
The sensitivity is RUDRSTOP*TAILGAIN when the hovering and rightward
spinning stop. When the ability to prevent side wind is poor, hovering drifts
rightward or slow rightward pinning stopping speed, turn up the RUDRSTOP value.
Tail rebounds when stopping, rightward pinning turn down the RUDRSTOP value.
This value is not allowed to turned extremly.
4
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RUDD-ACC ------ Rudder Accelerate Delay
Menu items
Description
0 ~ 15
(Default 0)
The higher the value, the smoother and longer it takes to reach piro speed from static.
Suggestion
Increase RUDD-ACC on lag tail.
5
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RUDD-DEC ------ Rudder Decelerate Dealy
Menu items
Description
0 ~ 15
(Default 0)
The higher the value, the longer it takes for the tail to slow down. Used to smoothen
the deceleration of piro when coming to a stop.
Suggestion
Increase RUDD-DEC on rebounded tail.
6
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RUDD-EXP ------ Rudder Stick Expo Curve
Menu items
Description
-100 ~ +100
(Default 0)
Rudder expo curve to the stick movement
7
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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.
TAIL TORQUE COMP Submenu Configuration Steps:
1
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PIT-COMP ----- Compensation of Collective Pitch to Tail Rotor
Item
Description
-100 ~ +100
(Default 0)
The change of collective pitch causes the change of rotary speed of main rotor, and
tail deviation, adjust PIT-COMP value until the torque change can be offset
completely. If the torque change causes tail deviate leftward, compensate rightward
rudder direction input, i.e. compensate reversely rudder direction input.
Identification of
Compensation
Direction
Turn off brushless motor power or engine throttle, push collective pitch stick,
adjust PIT-COMP value, check if the compensation direction of collective pitch to
tail rotor is correct.
2
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CYC-COMP ----- Compensation of Ring Pitch to Tail Rotor
Item
Description
-100 ~ +100
(Default 0)
The change of ring pitch causes the change of rotary speed of main rotor, and tail
deviation, adjust CYC-COMP value until the torque change can be offset
completely. If the torque change causes tail deviate leftward, compensate rightward
rudder direction input, i.e. compensate reversely rudder direction input.
Identification of
Compensation
Direction
Turn off brushless motor power or engine throttle, push elevation or aileron stick,
adjust CYC-COMP value, check if the compensation direction of ring pitch to tail
rotor is correct.