中文
Wings in Emergency, Uninterrupted Communication
HC-541 adopts a composite vertical take-off and landing fixed wing layout, the fuselage is molded from carbon fiber and foam sandwich, the structure is light weight and high strength, and the wing and tail are removable design. It can carry photoelectric cameras, rapid 3D modeling payloads, airborne public network base stations, airborne PDT cluster base stations, airborne broadband AD hoc networking equipment, airborne satellite communication equipment, airborne personnel search and rescue payloads, etc., and can be applied to emergency communication, reconnaissance aerial survey and other scenarios.
6h long endurance
30kg payload
Hybrid power system
Convenient take-off & landing
Air-cooled, twin-cylinder, horizontally-opposed, two-stroke, direct-drive aero-engine and super high power to meet the demand of the UAV climbing speed and provide stable power supply for the entire mission system.
HC-541 emergency communication compound-wing UAV is equipped with airborne satellite communication equipment, airborne public network base station, maintains link communication with satellites through high-altitude flight, adopts 4G/5G communication technology, transmits business data back to the operator's core network through satellite transmission, restores public network communication in the disaster-hit area directionally, and provides voice, SMS and Internet services for users in the disaster-hit areas.
HC-541 emergency communication compound-wing UAV is equipped with airborne satellite communication equipment, airborne PDT cluster base stations, airborne broadband AD hoc networking equipment, etc., to quickly build emergency communication private network for public security, emergency and other departments, to meet the real-time information and command exchange requirements between the command center and frontline search and rescue personnel, and to ensure the smooth progress of rescue work.
HC-541 emergency communication compound-wing UAV is equipped with rapid 3D modeling payloads, which can quickly complete aerial survey data acquisition, generate 3D models in real time, and publish a map to the emergency command of the Ministry of Emergency Management in real time, quickly provide real-time 3D situation maps for the front and rear command, and assist in the research and judgment of disaster development.
HC-541 equipped with photoelectric camera can be used in inspection and emergency search and rescue and other scenarios, two-axis three-lens target positioning camera, integrated with 30x optical zoom visible light camera, 640×512 high-resolution infrared camera, laser range finder, and high-precision gyro-stabilized platform, with all-weather work capability.
The flight control system integrates the flight control computer and the micro-integrated navigation system (GPS/INS), which has the functions of one-click automatic take-off, landing, hovering, circling, return, altitude hold, opening parachute and various forms of autonomous cruise according to the scheduled route.
Autonomous Takeoff and Landing & Route Planning
Automatic Flight Beyond Visual Range
Control the Attitude of the Aircraft
Switch the Flight Mode Online
Empowering flight operations with unlimited potential
Empowering flight operations with unlimited potential
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