LH-ZEUS1200

Category:

UAV SERIES

Basic Performance:

The LH-ZEUS1200 series (quad-rotor, 1.2m) body is a four-axis body with a folding arm configuration; the whole machine uses 1K carbon fiber prepreg, and the molding process uses metal molds to form one layer to ensure fiber continuity and The mechanical properties of the reinforced parts ensure that the structure of the aircraft 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

2.5kg

Battery life

Up to 100min

Rain resistance
IP65/moderate 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 10kg

Link down
Return home

Technical index

LH-ZEUS1200-0.9M body technical index
Recommended mount	＜2.5kg
Flight time	100min (no load), 85min/0.6kg
Body weight	1.1kg
Empty weight	2.7kg(Including: airframe/motor/ESC/propeller/power cable)
Maximum take-off weight	10kg
Recommended take-off weight	6.5~8.5kg
Motor/ESC	6 series/40A
propeller	22 inches
Wind resistance level	Up to level 7
Takeoff altitude	＞0~5000 meters (high prototype)
Protection level / rainproof	IP65/moderate rain
Environmentally adaptive	Meet the relevant environmental requirements in GJB150A-2009
LH-ZEUS1200-0.9M body size parameters
Expand Size	900×900×361 mm(Length×Width×Height)
Folded size	480×480×170 mm(Length×Width×Height)
Symmetrical motor wheelbase	900mm
Inner diameter of motor base	∅75mm
Battery compartment size	205x160x52mm(Length×Width×Height)
Equipment warehouse size	230x160x32mm(Length×Width×Height)

Flying platform

Model: LH-ZEUS1200 body adopts four-axis multi-rotor, plug-in arm configuration;
Body material: carbon fiber integrated molding technology;
Power system: lithium battery power system;
Body size: 900*900*361mm
The maximum total take-off weight is 10kg, and the maximum mission load is 2.5kg;
Vertical take-off and landing capability without manual intervention, landing point offset ≤20cm;
No-load endurance time is 100min;
Standard mission loading life time is 65min;
Cruising speed 45km/h, maximum level flight speed 54km/h;
Wind resistance ≥7;
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;
Modular design, with fast assembly and disassembly functions, the assembly and disassembly time are less than 3 minutes;
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;
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;
Expansibility: It can be replaced with other sensors such as lidar;

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;

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 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;

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;