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LH-SN1800

Category:

UAV SERIES

Basic Performance:

The LH-SN1800-1.8M type airframe is a six-axis airframe. The whole aircraft uses 3K carbon fiber prepreg. The molding process uses metal molds to form one layer to ensure the continuity of the fibers and the mechanical properties of the reinforced parts, ensuring the aircraft’s performance. The structure is light and achieves more suitable rigidity and strength.

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

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Features

Effective load

Up to 20 kg

Battery life

Up to 15-18min

Rain resistance
IP54/light rain

Wireless transmission
Data Link Plus
Picture transmission is integrated

Wind resistance level
Up to level 7

Takeoff altitude
0-5000米

Mount platform
Adapt to various application pods

Takeoff weight
Max 35kg

Multi-directional obstacle avoidance radar

Technical index

LH-SN1800-1.8M body technical index
Medicine box load	10L～20L
Flight time	15～18min
Motor/ESC	10 series/60A
propeller	32 inches
Recommended battery	Two pieces of 12S 30Ah/14S 30Ah
Takeoff altitude	＞0~5000 meters (high prototype)
Protection level / rainproof	IP54/light rain
Environmentally adaptive	Meet the relevant environmental requirements in GJB150A-2009
LH-SN1800-1.8M body size parameters
Symmetrical motor wheelbase	1800mm
Inner diameter of motor base	104mm in diameter
Battery compartment size	∅330x105mm(Diameter×height)
Equipment warehouse size	∅370x35mm(Diameter×height)

Flying platform

Model: LH-SN1800 body adopts six-axis multi-rotor, folding arm configuration;
Body material: carbon fiber integrated molding technology;
Power system: Lithium battery power system; smart fast charge battery, fast charging in 20 minutes; support IP65 dustproof and waterproof
Body size: 1800mm
Maximum take-off gross weight 35kg, maximum mission load 20kg
Vertical take-off and landing capability without manual intervention, landing point offset ≤20cm;
Endurance time 15-18min (with CMAN, CAL, LAC-MRA, CNAS and the test report certified by the Ministry of Public Security);
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 altitude ≥5000m;
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 2.4 GHz and a control distance of 15 kilometers (standard version, customizable);
Flight control deviation: track deviation ≤0.5m, standard deviation ≤0.3m;
Hovering control deviation: horizontal deviation≤0.3m, vertical deviation≤0.3m;
模块化设计，具有快速组装和拆收功能，组装和拆收时间均小于3min（具备CMAN、CAL、LAC-MRA、CNAS及公安部认证的检测报告）；
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 measuring the heading and angle of the airborne dual GPS;
The mission cabin of the flight platform has a photoelectric pod quick release mechanism. Facilitate 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;
Scalability: It can be replaced with other sensors such as lidar;

Flight control and navigation system

Support full-process and fully autonomous flight；
Differential GNSS system supports GPS, GLONASS, Galileo, BDS four-star and eight-frequency signals；
Equipped with ground station monitoring function, which can monitor the operation status of the drone 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;

Broadband link

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 the ground station in real time;
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;

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;
It supports standard pre-flight inspection, and cannot take off if it fails the self-inspection;
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 task 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, The 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 nearest 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;