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21
insurance will be locked up automatically exceeding 5 seconds.
Notices:
Rod moving:
Rudder in the left- most position, elevator in the bottom, aileron in
the right-most position,throttle in the bottom.
For the right or left throttle, user
need to judge by self that the motor arming direction is
八
or V shape.
After moving rod as V shaped,
motor will not be enabled automatically
, user
need to push the throttle stick to the minimum position to enable the motor
after moving rod.
（
2
2
2
2
）
Vibrating
Vibrating
Vibrating
Vibrating and
and
and
and Shaking
Shaking
Shaking
Shaking
During flight, user need observe the
“vibrate state”
and
“shake state ”
in
“data”
page to judge the shaking status of IMU. In stable flight, it is normal when the
“vibrate state“ and “shake state ” range from 0~9, the smaller the number the
smaller the shaking, the number will directly affect flying performance.
Tips:
Vibrating coefficient:
the maximum acceleration of alternate motion(vibrate) in
up&down/left&right/back&forth three directions.
Shaking coefficients:
the maximum angular velocity of rotary movement around
X/Y/Z three axises.
(3)
(3)
(3)
(3) Manual
Manual
Manual
Manual servo
servo
servo
servo position
position
position
position and
and
and
and real
real
real
real servo
servo
servo
servo position
position
position
position
Manual servo position
After channel calibration on transmitter, when user put the stick in the middle
position, the value of rudder, elevator and aileron in
“manual servo position”
of
GCS should be small (no more than 2) . If user already adjusted the trim and the
manual servo position is not near the center, need to
click on
“Neutral Position”
