FeiYu Tech Panda Autopilot - Manual (Page 47)

Guilin Feiyu Electronic Technology Co., Ltd
Guilin Feiyu Electronic Technology Co., Ltd http://www.feiyudz.cn [email protected]
Page 46
sensitivity. If your Rudder control sensitivity is high this parameter value should be
reduced, and vice versa.
For all other mix-control modes, the turning is complete via aileron only. Therefore this
‗Rud Turn Control‘ parameter has no effect on the aircraft.
Range :0-99.Default value:60.
3. Rud stab: Control gain to counter the rotation of Z Axis (perpendicular to the body of
the plane).The higher the value, the greater the control gain would be.
Range: 0-99. Default value: 20.
Stability Control
1. Pitch Stability: The amendment control gain given by the change of the flight pitch
angle .The higher of the setting, the greater of the control gain. Setting Range: 0-99.
Default value: 40.
2. Roll Stability: The amendment control gain given by the change of the flight roll
angle .The higher of the setting, the greater of the control gain. Setting Range: 0-99.
Default value: 40.
Auto take-off
1. Attack angle: Use this to adjust the Auto take-off pitch setting.
Setting Value Range: 0 to 40 Degrees
2. Take-off Spd: Ground speed setting during
take-off.
Setting Range: 0 to 99 meters per second
Vibration Detection and Adjustment
1. It is critical that the installation of the autopilot meets the vibration damping
requirements.
2. If the installation does not meet the requirements, it will affect the accuracy of the
attitude stabilization greatly.
3. Excessive vibration can cause unpredictable flight characteristics.
Vibration Damping Test Procedure:
1. Connect the power to the system and switch ON the plane.
2. Move the Control Mode switch to Auto Balance Mode or
manual mode.
3. Observe the attitude of the autopilot screen and ensure that
the attitude shown is correct.
4. Slowly activate throttle and spin the motor / propeller. Do not take off!
5. Increase throttle and hold for 20 seconds at different increments.