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Aircraft & TX Basic Operation

Definitions

Stick neutral position and stick released means the stick of TX is pushed to the central position.

Command Stick means the stick of TX is pushed away from the central position.

is the nose direction）

（

GPS ATTI. ATTI. Manual

OFF Course Lock Home Point Lock

You can change the operation mode of the TX according to the advanced manual if necessary.

Aircraft

Throttle stick is for aircraft up& down

control. The aircraft will hold the height

automatically if the stick released. The

throttle stick cannot hold the central

position when released.

Yaw stick is for aircraft rudder control.

Command stick is responding to the changing angle velocity of

the aircraft, with the maximum rudder angular velocity is

200°/s. Left push the stick, counter clock-wise rotation of the

aircraft, vice versa.

Roll stick is for aircraft left/right control

and Pitch stick is for front/back control.

Command stick is responding to the

changing angle of the aircraft. Stick

neutral position is for 0˚, its endpoint is

45˚. The roll and pitch stick holds the

central position when released.

Use a 3-position switch on the TX as mode control switch. After

connection to the GPS module, GPS ATTI. Mode is available.

Pay attention because the GPS ATTI. Mode is dependent on

the number of GPS satellites acquired by the main controller.

Use a 3-position switch on the TX as Intelligent Orientation

Control (IOC) switch. Flip the switch to OFF in basic flight.

Use IOC function when you are family with basic flight.

Download the advanced manual from DJI website to get more details.

GPS ATTI. /ATTI. Mode

In GPS Mode, the aircraft will hover (hold

horizontal position) when sticks released.

In ATTI. Mode, the aircraft will keep attitude

stabilizing

without

horizontal

(different from hover in GPS Mode)

Manual Mode

Throttle stick is for

aircraft up& down

control

without

height

function.

Command stick is

the changing angle

velocity (the max

velocity is 150°/s) of

the aircraft.

The

aircraft

keep the front/back

/left/right

not

rotate, but without

attitude

stabilizing

in 0˚.

position

hold

will

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