Can take off and land vertically, autonomous route high-speed cruise flight, air hover, etc
. Can be equipped with dual photoelectric pods (visible and infrared detection), intelligent identification and tracking of targets
Support rapid disassembly of wing, tail and pylon
. Super endurance, lasting for 2h
Maximum mission load up to 5kg
Control radius 50km
G10 is the first uav model using tilt-rotor technology. Combining the advantages of multi-rotor vertical takeoff and landing and the high speed and long flight time of fixed wing, it can take off and land vertically to adapt to the complex and narrow terrain such as mountains and ships. It can effectively improve the problems of short flight time and limited range of motion of multi-rotor uav.
G10 uav is equipped with intelligent and fully autonomous flight capability. It can take off, hover, tilt, fly and land with one button. It is easy to operate and has a low threshold for users. Equipped with optical pod to complete aerial reconnaissance, target acquisition, target tracking and other tasks.
The aircraft adopts mechanical and electrical integration design, the integration of mechanical interface and electrical interface, the whole machine is easy to disassemble, greatly reducing the time of deployment and withdrawal. Pure electric power system, safe and reliable.
Technical Specification
|
aircraft |
Maximum overall size |
9mX3.3mx0.55m (captain-wingspan - aircraft height) |
|
Weight |
18kg (including battery, no photovoltaic pod and link) |
|
|
Navigation lights can be visual distance |
1 km |
|
|
Available onboard |
Double photoelectricity pod, hd camera, hd digital camera, etc |
|
|
purpose |
High-altitude shooting, monitoring, reconnaissance, survey, real-time transmission of video to the ground receiving equipment, and save high-definition video. |
|
|
flightmode |
Fully autonomous mode |
|
|
Drone specifications |
positioning system |
GPS, accelerometer, gyroscope, magnetometer, barometer |
|
Power type |
electric |
|
|
Max range |
135km |
|
|
Max endurance |
2 h |
|
|
Max control radius |
50 km (ground station ) |
|
|
Max flight speed |
180Km/h |
|
|
Cruising speeds |
72km/h |
|
|
Max flight altitude |
5 km |
|
|
Max sustained wind speed |
Cruise resistance wind 6, take off and land resistance crosswind 4 |
|
|
Max mission payload |
5kg |
|
|
Max take-off weight |
33kg |
|
|
Body material |
All carbon fiber body |
|
|
Remote characters |
Function |
1. Control the flight attitude and direction of the aircraft through the remote pole device; |
|
working frequency |
2.4GHZ |
|
|
Signal effective range |
1Km (open outdoor without interference) |
|
|
power supply mode |
Lithium battery, rechargeable, 2000mAh, 7.4v |
|
|
run time |
> 4 hours |
|
|
D06 ground control station |
Ground control station power supply system |
Input voltage: 100-240 vac 50/60 HZ |
|
working frequency |
The video adopts 580±5MHZ for full hd video reception The communication adopts 840±5MHZ data transmission module for transceiver control |
|
|
Signal effective range |
50km (open outdoor without interference) |
|
|
screen resolution |
1920 X 1080 |
|
|
Video storage resolution |
Hd 1080 p |
|
|
interface type |
USBX2，HDMIX1，RJ45X1 |