2 Basic flying
Read this section before basic flight testing.
2.1Control Mode Instruction
The aircraft performs differently when using different control modes. Please read the following table to know
the different control modes, which may help you to achieve a more involved flight experience.
Command
Linearity
Control the aircraft to rotate in clockwise and counter clockwise direction.
Yaw
Aircraft attitude control; Mid point of stick is for 0˚
Roll and Pitch
Aircraft height control.
Throttle
meter from ground when the throttle stick is in mid position.
All Sticks
Lock position if GPS signal
Released
When GPS signal has been
GPS Lost
lost for 3s, system enters
ATTI. Mode automatically.
IOC
Supported
The
FailSafe
Mode if the Transmitter signal is lost and no
Protection
matter if Transmitter signal recovers or not,
system will not exit failsafe mode automatically.
GPS Involved
Low-voltage
LED alert with Descending or Go Home &
Protection
Environment
recommended
*Default is Manual, users can set to ATTI.1 in Assistant software. The biggest difference between ATTI.1 and ATTI.2
is that they are working differently in the protection situations.
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Control Mode 3
GPS
attitude, and its endpoint is 35˚.
Maintain the altitude best above 1
is adequate.
CL/HL/POI
flight control system will enter FailSafe
YES
Landing precautions
Open flying field;
Good GPS signal
15 |
Control Mode 2
ATTI. 2
ATTI. 1
YES
angular velocity 150°/s
Only attitude stabilizing. No
position locking.
---
CL
The
FailSafe Mode if the Transmitter signal is
lost and the system will exit Failsafe once
Narrow Space;
GPS signal bad
Control Mode 1*
Manual
Maximum rudder
Max-angular velocity is 150°/s.
No attitude angle limit.
No altitude locking when the
throttle stick is in mid position.
Keep original
attitude.
---
None
flight control system will enter
the signal recovers.
NO
Only LED alert
Regain control in emergency
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