Introduction to the ZD-108:
ZD-108 is a set of professional-class long-haul aerial photography system, can be paired with professional camera head system, with portable and easy to use, good operation and security and stability and other advantages. The highly integrated design concept makes the installation and commissioning of the system simple and fast. Efficient flight control system provides the flight platform with excellent user experience and stable flight posture, sophisticated GPS receivers and IMU sensors for high-precision navigation control, self-patented central power distribution boards, high-speed motors and electric tones, with high-efficiency propellers, providing efficient power and responsive maneuverabilityCombining data chains with a variety of anti-jamming and encryption technologies to provide safe and reliable real-time data transmission, the aircraft can be used for longer periods of time, avoiding frequent battery replacements, and reducing aerial photography costs.
Product features:
Safe and stable
The ZD-108 features a four-axis octa-rotor design layout, with the main structural components using carbon fiber composites and aeronautical aluminum with a high quality strength, ensuring maximum weight reduction while maintaining body strength. Integrated central power distribution board, so that the whole machine power system, power supply system and control system arrangement and connection more secure and convenient.Mature industrial-grade flight control system, using efficient and stable CPU, integrated high-precision IMU sensors and GPS receivers, the use of advanced temperature compensation, accurate data calibration and high-precision loop control algorithms, to ensure safe and reliable flight control while providing a comfortable handling feel.
Portable and easy to use
All arms can be folded down to minimize the volume of the entire machine transport, simply lift the arm, lock the rotary buckle, you can expand the body.The central power distribution board is integrated with the power conversion function, which gives power to the power distribution board, which can bring the system into a working-ready state and greatly shorten the preparation time.
Flight control mode
In order to meet the needs of different application scenarios, a variety of control modes are designed, and the performance of aircraft in different modes will be different.
(1) Manual mode: flight attitude and other controls rely entirely on the ground remote control.
(2) Attitude mode: flight control automatic control stable attitude, throttle mid-point lock height, other control by the ground remote control.
(3) GPS mode: flight control automatic control stability attitude, throttle center lock height, rocker mid-position lock position, other control by the ground remote control.
(4) Fully automatic route mode: pre-planned flight routes on Google Maps, by the flight control system independently control the aircraft take-off and landing and over-the-horizon precision flight.
(5) full autonomous take-off and landing: to maintain the aircraft posture stability, one-click automatic completion of the aircraft's fixed-point take-off and landing.
(6) Intelligent direction control: redefine the aircraft direction, release the head orientation and the direction lock relationship.
Security mechanisms
In order to prevent accidental aircraft crash, multiple protection mechanisms are designed:
(1) Out-of-control protection: remote control signal is lost when it can hover or return.
(2) Low voltage protection: when the power voltage is too low, alert the controller, return or land autonomously.
(3) One-click return: remote control or flight abnormal, switch to autonomous return mode by switching one click.
(4) Can be added to the parachute drop system.
GH4 gimlet system (Panasonic GH4 micro-single camera, 4K 30p recording)
(1) Three modes of work
Direction locking control
Non-directional locking control
FPV mode (reset)
2 Built-in stand-alone IMU module
(3) Cloud head dedicated servo drive module
(4) HDMI-AV module
(5) Wireless video transmission support
(6) Camera shutter control support
(7) Wide range voltage input support
(8) S-Bus/PPM receiver support
(9) GH4 camera parameters:
Camera Frame 4/3 Frame Camera
Total pixels 17 megapixels
Effective pixels 16 megapixels
Zoom multiple depends on lens
Digital Zoom Multiple 4x Digital Zoom
Operating mode with full manual function
Sensor type CMOS sensor
Sensor size 17.3 x 13mm
Sensor description frame ratio: 3:2, 16:9, 4:3, 1:1
Video processing system Venus Engine IX, maximum resolution 4608 x 3456
Photo resolution 4608 x 3072,4608 x 2592,3456 x 3456,3264 x 2448,3264 x 2176,2448 x 2448,2336 x 1752,2356 x 1560, 1920 x 1080,
1744*1744,1824*1368,1824*1216,1824*1024,1712*1712
Technical parameters:
| Aircraft | |
| Standard take-off weight | 19kg(Equipped with aerial photography equipment) |
| Maximum take-off weight | 27kg |
| Maximum payload | 10kg |
| Specifications | 1800*1800*600 mm(Expand with paddles) 700*700*600 mm(Folding) |
| Power battery | 6s 15c 22000mah*2 |
| Relative flight altitude | 1000m |
| Active job time | About30 min(with a head and camera) |
| Maximum battery life | 40 min |
| Control Radius | 1 km(Optional addition5km/10km） |
| Hover accuracy | Vertical: splusmn;0.5 m, level: splusmn;1.5 m |
| Maximum lift speed | 6 m/s |
| Maximum cruising speed | 10 m/s |
| Maximum tilt angle | 35° |
| Wind resistance | 4Level |
| Working environment temperature | -10℃ ~ 40℃ |
