Aero-y200
Product Overview
The Aero-Y200 UAV features strong anti-interference capabilities with a GPS and Beidou four-antenna anti-jamming module, complemented by inertial navigation for enhanced precision. It is equipped with a dual-channel thermal imaging and visible-light AI seeker, enabling effective day and night operations. The drone supports autonomous guidance with manual target confirmation via image transmission and leverages deep learning to process target information, allowing guided attacks based on uploaded images. Additionally, it boasts a 50km military-grade image and data transmission system for real-time operational control.
PRODUCT DESCRIPTION
The Aero-Y200 is a long-range intelligent UAV designed with a compact, tailless delta-wing aerodynamic layout for optimal maneuverability. Engineered for primary swarm operations as a loitering munition, it measures 3.4 meters in length and features a wooden propeller with an optional rocket-assisted takeoff. Weighing 100 kg in total, it carries a 30 kg warhead and is powered by a 17.5-horsepower small-to-medium aero engine. The UAV is capable of dynamically altering its target mid-flight, combining the characteristics of a cruise missile with advanced inertial navigation and GPS guidance for precision strikes.
Specifications
Strong anti-interference
Equipped with GPS & Beidou 4-antenna anti-interference module
Dual-channel thermal imaging
Visible light AI seeker, attack day and night
Deep learning
The target information can be input into the guider in the form of pictures, and the guided attack can be carried out according to the pictures
Typical Mission Profile
After takeoff, the Aero-Y200 UAV ascends to a safe altitude before transitioning to level flight. It then climbs to a cruising altitude of 1,000 meters, maintaining a speed of 180 km/h. As it nears the target area, the UAV enters its attack range, initiating a glide and dive while adjusting its course to precisely align with the target waypoint before executing the strike.
The standard flight mission table defines each stage of flight, detailing function names, engine stall selection, altitude, speed, distance, and duration. It also allows for direct estimation of fuel consumption for the entire mission profile. By analyzing a given speed sequence, it calculates the corresponding climb gradient and rate at various altitudes, providing a data table and curve. The UAV’s maximum climb rate at different altitudes determines its overall climbing capability, while the point where the climb rate approaches zero represents its theoretical maximum altitude.
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