LH-ARES2400

Category:

UAV SERIES

Basic Performance:

It adopts high-definition carbon fiber integrated body structure, which has good rigidity and light weight. It can carry up to 30kg of items to fly, and the flight time can reach 75min. Remote control operation, support one-key take-off, one-key return home, one-key landing and other instant tasks, can accurately set waypoint tasks, fixed-point flight. Highly centralized rainproof gimbal design, can fly in light rain environment.

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

Up to 30 kg

Battery life

Up to 75min

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 meters

Mount platform
Adapt to various application pods

Takeoff weight
Up to 80kg

Link down
Return home

Technical index

LH-ARES2400-2.4M body technical indicators
Recommended mount	12kg~30kg
Flight time	75min (15kg load), 60min (25kg load)
Body weight	6kg
Empty weight	2.7kg(Including: airframe/motor/ESC/propeller/power cable)
Maximum take-off weight	80kg
Recommended take-off weight	35kg~80kg
Recommended motor/ESC	M15/80A
Recommended propeller	34寸
Recommended battery	12块6S 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-ARES2400-2.4M body size parameters
Symmetrical motor wheelbase	2400mm
Inner diameter of motor base	117mm diameter
Battery compartment size	∅410x140mm(Diameter×height)
Equipment warehouse size	∅410x50mm(Diameter×height)
Landing gear height	311mm

Flying platform

Model: LH-ARES2400 body adopts eight-axis multi-rotor, plug-in arm configuration;
Body material: carbon fiber integrated molding technology;
Power system: lithium battery power system;
Body size: 2400mm;
The maximum total take-off weight is 80kg, and the maximum mission load is 30kg;
Vertical take-off and landing capability without manual intervention, landing point offset ≤20cm;
No-load endurance time is 75min;
Standard mission loading life time is 50min;
Cruising speed ≥40km/h, maximum level flight speed ≥50km/h;
Wind resistance ≥8;
Take-off altitude ≥3500m, level flight altitude ≥6000m;
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 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;
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 quick disassembly of the pod before and after the mission;
Night navigation capability: with navigation indicator;
Carrying ability: It has the ability to carry multiple devices such as dual-light photoelectric pod, image transmission, and orthophoto camera at the same time;
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 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;

Broadband link

Configure dual telemetry and remote control links, one of which is disconnected and can be switched to the other link;
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, customizable);
RF power ≤2W;

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;