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DJI FlyCart 30
User Manual
10
©
2024 DJI All Rights Reserved.
Flight Control Surfaces
Not applicable for multicopters.
Propulsion System
The propulsion system consists of motors, ESCs, and folding propellers, to provide stable and
powerful thrust.
Avionics
The avionics includes an aerial-electronics system, image transmission system, binocular vision
and radar system, cargo system, parachute, and FPV module.
Flight Control and Navigation System
The ight control and navigation system built into the aircraft is integrated with modules such
as the ight controller, IMU, barometer, GNSS receiver, RTK module, and compass, providing
stable and reliable navigation and control. The dedicated industrial ight controller provides
multiple flight modes and operation modes for various applications. The GNSS+RTK dual-
redundancy system is compatible with GPS, GLONASS, BeiDou, QZSS, and Galileo. The aircraft
also supports centimeterlevel positioning when used with the built-in onboard D-RTK antennas.
Dual-antenna technology provides strong resistance against magnetic interference.
Communication Equipment
The aircraft boasts two OCUSYNC
TM
image transmission antennas and DJI O3 image transmission
system, oering a maximum transmission range of 20 km for communication with the remote
controller.
FPV Module
The FlyCart 30 aircraft is equipped with an HD FPV gimbal camera. It helps the pilot to have
better visibility of the ight environment and assists the aircraft in landing and releasing cargo
precisely via the AR projection feature.
The tilt of the gimbal camera can be adjusted by using the left dial of the remote controller or
the gimbal camera adjustment button in the DJI Pilot 2 app.
Binocular Vision System and Active Phased Array Radars
The aircraft is equipped with a phased array radar system and binocular vision system.
The systems provide multi-directional obstacle sensing as well as bypass functions to ensure
flight safety. In addition, the flight control system limits the descent speed of the aircraft
according to the distance between the aircraft and the ground, as detected by the radar
module. This helps the aircraft make smooth landings.
The max horizontal ight speed is limited to 15 m/s, while max ascent speed is limited to 5 m/s,
and descent speed is limited to 3 m/s.
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