LH-MJY1600

Category:

UAV SERIES

Basic Performance:

Modular design, reliability and portability of giant soft-shelled turtle. The fuselage is made of carbon fiber + composite materials, which is light in weight. It can carry items up to 15kg in weight, and the maximum flight distance can reach 120min.

Qingdao Lei Zhenzi Technology Co., Ltd.

Tel: +86-(0532)55676650 +86-17864191360

Email: 1353006353@qq.com

Contact: Manager MaoAdd: Room 1402, 14th Floor, Building A1, Zhongke R&D City, No. 151, Huizhiqiao Road, High-tech Zone, Qingdao City, Shandong Province

Intention to submit

Features

Effective load

15 kg

Battery life

Up to 120min

Rain resistance
IP45/light rain

Wireless transmission
Data Link Plus
Picture transmission is integrated

Wind resistance level
Up to level 7

Takeoff altitude
0-5000 meters

Mount platform
Adapt to various application pods

Takeoff weight
Up to 32kg

Link down
Return home

Technical index

LH-MJY1600-1.6M body technical index
Recommended mount	3kg~15kg
Flight time	120min(No load)
Body weight	3.45kg
Maximum take-off weight	32kg
Recommended take-off weight	18kg~30kg
Motor/ESC	8 series/10 series/60A
8 series/10 series/60A	27 inch~30 inch
Recommended battery	两块12S 30Ah
Takeoff altitude	＞0~5000米（高原型）
Protection level / rainproof	IP54/light rain
Environmentally adaptive	Meet the relevant environmental requirements in GJB150A-2009
LH-MJY1600-1.6M body size parameters
Symmetrical motor wheelbase	1613mm
Inner diameter of motor base	95mm in diameter
Battery compartment size	∅330x105mm(Diameter×height)
Equipment warehouse size	∅370x35mm(Diameter×height)
Landing gear height	324mm
Packing box size	95x79x68cm(Length×Width×Height)

Flying platform

Model: LH-MJY1600 body adopts six-axis multi-rotor, plug-in arm configuration;
Body material: carbon fiber integrated molding technology;
Power system: lithium battery power system;
Body size: 1600mm;
The maximum total take-off weight is 32kg, the maximum mission load is 15kg, and the standard mission load is 5kg;
Vertical take-off and landing capability without manual intervention, landing point offset ≤20cm;
No-load endurance time 120min (with CMAN, CAL, LAC-MRA, CNAS and the test report certified by the Ministry of Public Security);
Standard mission loading life time is 90min;
Cruising speed ≥45km/h, maximum level flight speed ≥54km/h;
Wind resistance ≥ Level 7 (with CMAN, CAL, LAC-MRA, CNAS and test reports certified by the Ministry of Public Security);
Take-off altitude ≥3500m, level flight ceiling ≥6000m (with CMAN, CAL, LAC-MRA, CNAS and test reports certified by the Ministry of Public Security);
Flight attitude stability: pitch angle stability ≤ 4°, roll angle stability ≤ 5°, yaw angle stability ≤ 3°;
The image transmission scheme adopts an integrated scheme of image and data, with a frequency of 2.4GHz and a control distance of 15km (standard version, customizable);
Flight control deviation: track deviation ≤0.5m, standard deviation ≤0.3m;
Hovering control deviation: horizontal deviation ≤ 0.3 m, vertical deviation ≤ 0.3 m;
Modular design, with fast assembly and disassembly functions, the assembly and disassembly time is less than 3 minutes (with CMAN, CAL, LAC-MRA, CNAS and the Ministry of Public Security certification test report);
The drone supports one-key return to home, supports low battery voltage alarm; supports link interruption to return; supports flight area limitation function;
The flight platform has the function of airborne dual GPS to measure the heading angle (with CMAN, CAL, LAC-MRA, CNAS and test reports certified by the Ministry of Public Security);
There is a photoelectric pod quick release mechanism in the mission cabin of the flight platform. Facilitate the quick disassembly of the pod before and after the mission;
Night navigation capability: with navigation indicator;
Carrying capacity: It has the ability to simultaneously carry multiple devices such as dual-optical optoelectronic pods, image transmission, and orthophoto cameras (with CMAN, CAL, LAC-MRA, CNAS and the Ministry of Public Security certified test reports);
Scalability: It can be replaced with other sensors such as lidar (with CMAN, CAL, LAC-MRA, CNAS, and inspection reports certified by the Ministry of Public Security);

Flight control and navigation system

Support the whole process and fully autonomous flight;
Differential GNSS system supports GPS, GLONASS, Galileo, BDS four-star and eight-frequency signals;
With the monitoring function of the ground station, the operation status of the drone can be monitored in real time at the ground station;
Emergency response capability: has the function of near-ground avoidance;
Temperature compensation, all sensors can perform temperature compensation in the range of -20 degrees to 70 degrees;
Sensor integration, with 3-axis accelerometer, 3-axis angular velocity meter, magnetic sensor, dynamic and static pressure sensor;
The black box can store 4 hours of detailed flight data at a frequency of 50 Hz;
Waypoints, ≥800;
Update frequency, ≥200Hz;

Communication link

Configure dual telemetry remote control links, one of which is disconnected and can be switched to the other link (with CMAN, CAL, LAC-MRA, CNAS and test reports certified by the Ministry of Public Security);
The working frequency band meets the relevant requirements of the Ministry of Industry and Information Technology on drone-piloted aircraft systems;
Maximum bit rate ≥8Mbps;
Transmission video resolution ≥1080P 50fps;
Full end-to-end delay of video boundary ≤200ms;
Operating distance 15km (standard version, can be customized) (with CMAN, CAL, LAC-MRA, CNAS and the Ministry of Public Security certification test report);
RF power ≤2W;
3 communication link

Ground command station

The ground command station is a handheld ground operation terminal, integrated with a 7-inch high-definition high-brightness screen, the screen resolution is ≥1080P, and the total weight is 1kg;

Operating system: Android;
Digital image transmission and remote control: data link, remote control link, and video link are integrated;
Built-in battery working time ≥6h, and with external backup battery access function;
Support USB projection to computer or display screen;
Control radius ≥15 kilometers (standard version, can be customized);
Built-in GPS, built-in 4G module;
Working temperature: -20℃~60℃;
Support one aircraft dual control function, which can realize separate control of aircraft and mount;
Pod angle control, zoom, infrared mode, screen switching, image tracking, infrared correction, OSD display, brightness adjustment, contrast adjustment, landing instructions and other functional physical buttons;
Support standard pre-flight inspection, and cannot take off if the self-inspection fails;
Support multiple mission modes such as area scan, path scan, fixed-point gaze, etc., automatically plan and execute the flight plan, improve mission efficiency;
Comprehensive display of system status and mission status, including: attitude, speed, altitude, position, route status, battery status, link status, photoelectric pod status and other information, image data (infrared images include heat map data) can be stored and exported, Flight log data is complete, can be stored and exported;
Support custom video OSD display information content and language;
Support route preview function, which can visually display route altitude and terrain altitude difference to avoid mountain collision accidents;
Support automatic emergency landing, in case of failure and unable to return to the preset landing point, the closest preset emergency landing point will be automatically selected for forced landing to ensure safety;
Support real-time video output, and input the video of the photoelectric pod to the back-end equipment through the network port;