dji FLYCART 30

DJI FlyCart 30 User Manual
60
©
2024 DJI All Rights Reserved.
• It is recommended to use Method 1 to stop the motors. When using Method 2 to stop
the motors, the aircraft may roll over if it is not completely grounded. Use Method 2
with caution.
• After landing, power o the aircraft before turning o the remote controller.
Cruise/Maneuvering Flight
Flight Modes
The ight controller system of the aircraft supports the following ight modes. The aircraft will
y in N-mode (Normal) by default.
N-mode (Normal):
The aircraft utilizes GNSS or the RTK module for positioning. When the
GNSS signal is strong, the aircraft uses GNSS for positioning. When the RTK module is enabled
and the differential data transmission is strong, it provides centimeter-level positioning. It
will revert to Attitude mode when the GNSS signal is weak or when the compass experiences
interference.
S-mode (Sport):
The aircraft utilizes GNSS or the RTK module for positioning. By adjusting the
gain and expo settings, the maximum ight speed of the aircraft can be increased to 20 m/s.
The obstacle sensing performance will be reduced in S-mode. Fly with caution.
F-mode (Winch System)
: F-mode is based on N-mode. The flight speed is limited to allow
easier control of the aircraft. It is suitable to use when the aircraft position needs to be adjusted
slightly, such as before the winch system releases cargo.
If ASN mode has been selected in DJI Pilot 2, switch to F-mode to enter Attitude mode (A-mode).
In this mode, GNSS is not used for positioning and the aircraft can only maintain altitude using
the barometer. The ight speed in A-mode depends on the surroundings of the aircraft, such as
wind speed.
Attitude Mode Warning
In A-mode, the aircraft cannot position itself and is easily aected by its surroundings, which
may result in horizontal shifting. Use the remote controller to position the aircraft.
Maneuvering the aircraft in A-mode can be dicult. Make sure you are suciently familiar with
the aircraft behavior in A-mode. DO NOT y the aircraft too far away to avoid unnecessary risks.
Avoid ying in areas where GNSS signal is weak or in narrow and conned spaces. Otherwise,
the aircraft will be forced to enter Attitude mode, leading to potential ight hazards. Land the
aircraft in a safe place as soon as possible.
• Obstacle sensing performance is reduced in S-mode. Pay attention to the surrounding
environment and obstacles on the route when ying the aircraft in S-mode.
• Please note that when flying in S-mode, the flight speed of the aircraft will greatly
increase compared with that in N-mode (Normal). Accordingly, the braking distance will
also increase signicantly. When ying in a windless environment, a minimum braking
distance of 50 m (164 ft) is required.
• DO NOT switch from N-mode to either S-mode or A-mode unless you are suciently
familiar with the aircraft behavior under each ight mode.