Guilin Feiyu Electronic Technology Co., Ltd
Guilin Feiyu Electronic Technology Co., Ltd http://www.feiyudz.cn Email:[email protected]
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Altitude control
1.
Pitch control:
The higher the value, the higher the pitch up or down of the aircraft
nose. Maximum pitch up setting is + 20 degrees.
Maximum pitch down setting: - 20 degrees.
Range is 0 to 99. Default value: 50.
The following table shows Pitch angle control when the plane reaches 10 meter altitude:
Value
set
Attitude up
30
50
(
default
)
70
10 m
6°
10°
14°
2.
Alt Ofs integ:
Also known as Attitude Deviation Integration. This setting controls the
gain to integrate the aircraft current altitude to the target altitude.
The higher the value,
the greater the speed to match current and target altitude via pitch control.
Value Range: 0 to99, Default value: 10
3.
Altitude damping:
Pitch control gain to counter aircraft altitude change. The higher the
value, the greater the pitch action.
Value Range: 0 to 99. Default value: 50.
Throttle control
1.
Spd control:
This setting controls the aircraft speed in reference to the GPS speed
change. The higher the value, the greater the throttle control gain.
Value Range: 0 to 99. Default value: 50.
2.
Spd damping:
This setting controls the throttle control gain to counter changes in
airspeed.
The higher the value, the greater the control will gain.
Value Range: 0 to 99. Default value: 50.
Heading stabilization
1.
Side Offset Damping
:
Adjust gain to control the change in Side Offset damping.
The bigger the value, the bigger the control gain.
Range: 0-9. Default value: 5
2.
Rud Turn Control
:
When Selecting ―
Normal&No AIL/Turn via AIL&RUD
‖ or ―
Elevons/ Turn via
AIL&RUD
‖ in the Mix Control mode manual, the Parameter will be effected.
In these Two control mode, the turning of the plane is complete via both the Aileron and
Rudder.
The ‗Rud Turn Control‘ adjusts the gain of the rudder during automated aircraft turning.
This gain is linearly proportional. i,e, the value should be adjusted according to the Rudder