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10 auto return to launch mode(rth) test, 11 the altitude control of hovering mode, 12 camera gimbal stabilization adjust instructions – FeiYu Tech FY-41AP User Manual

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Guilin Feiyu Electronic Technology Co., Ltd

Guilin Feiyu Electronic Technology Co., Ltd http://www.feiyu-tech.com [email protected]

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13.10 Auto Return To Launch Mode(RTH) Test

First you should wait until the GPS positioning LED shows that the GPS positioning is

in a good condition

(Green light double flash each loop or triple flash each loop)

so

you can get a good hover effects.

The GPS will record the first positioning success point

as ―Home Point‖

.

Assuming the GPS hovering mode test is complete, we can now test the auto return

to launch function. Please control the aircraft to fly away for a certain distance in hovering

mode. Then switch CH5 to RTH mode.

If the aircraft return point less than 20 meters will automatically rise to 20 meters high

and then return and auto landing.

If the aircraft return point above 20 meters after return to home will auto landing.

13.11 The Altitude Control Of Hovering Mode

FY-41AP can automatically control flight altitude on hovering .Climbing and descending

rate is directly related to the throttle,

when the throttle stick is in the center position, 41AP

automatic locks the altitude

. Maximum means climb rate is 3 m/s, minimum means

decline rate is 1.5 m/s. The throttle stick can linearly control the aircraft climb and decline

rate.

13.12 Camera Gimbal Stabilization Adjust Instructions

Attention:

Please do not adjust the Camera Gimbal Stabilization until you have finished

the multi-rotor aircraft adjust.

Please according to following steps to adjust Camera Gimbal Stabilization :

(1) Gimbal Reverse

1) Shaking the Camera Gimbal on roll direction

, if 41AP doesn‘t give the

corresponding reverse correction, please choose Roll reverse.

2) Shaking the Camera Gimbal on pitch direction , if 41AP doesn‘t give the

corresponding reverse correction, please choose pitch reverse.

(2) Gimbal Gain