Product Introduction:

The HWA-CQ85 unmanned target drone is designed in a composite form of quadcopter and fixed wing, with quadcopter vertical takeoff and landing and hovering, and fixed wing long endurance and fast flight, combining the advantages of rotary wing aircraft and fixed wing unmanned aerial vehicles. The front engine can stably drive towed target flight, meeting the requirements of aerial target simulation applications.

Main technical parameters of unmanned aerial vehicles

Layout form: Mixed fixed wing and quadcopter;

L takeoff and landing mode: vertical takeoff and landing;

L Landing site: 10 meters * 10 meters flat ground;

Wingspan: 5.5m;

Captain: 3.6m;

Body color: Orange red (can be painted according to requirements);

L beacon light: supported;

Maximum takeoff weight: 85kg;

Payload: 7kg;

Cruise speed: 150km/h;

Maximum speed: 180km/h;

Maximum climb rate: 4m/s;

Maximum battery life: 2.5h;

Maximum range: 250km;

Continuous takeoff interval: 15 minutes;

L takeoff and landing altitude capability: altitude 4500m;

L ceiling: altitude 5000m;

Suitable load: infrared radiation source, electro-optical pod, Longbo ball, etc;

Working temperature:- 30℃～+50℃；

Storage temperature:- 35℃～+55℃；

Storage lifespan: For warehouses with humidity not exceeding 85%, the lifespan under storage conditions inside the packaging box should not be less than 3 years;

Special meteorological conditions: can fly normally in light rain/snow/heavy fog weather;

Wind resistance: Level 6;

Remote control radius: 30km (further distance can be customized according to requirements);

Flight control performance:

Horizontal positioning accuracy of unmanned aerial vehicles: less than 20m;

UAV altitude positioning accuracy: less than 50m;

Heading measurement accuracy: less than 3 °;

Heading measurement range: ± 180 °;

Attitude measurement accuracy: less than 2 °;

Attitude measurement range: ± 90 °;

Control function: Supports program control for automatic flight of drones, supports manual temporary change of waypoint during drone flight, and supports manual control of drone flight;

Information display: The ground station can display and control real-time unmanned aerial vehicle status information, including altitude, speed, position, heading, attitude, flight path, preset path, battery voltage, and other information.

Information storage: Ground stations and drone flight controllers can record real-time flight data and ground station related data;

Multi aircraft flight control: It has the ability to control multiple drones in one station, and can control 5 drones in one station;

Load control: The ground station can remotely and wirelessly control the ignition of the infrared source, or perform timed ignition at the set time of the ground station, supporting wired/wireless ignition control;

Drone assembly and disassembly time: The wings, tail fins, power batteries, etc. of the drone are designed for quick disassembly and can be assembled and disassembled by hand, with an assembly time of no more than 10 minutes;

L Service life: not less than 30 takeoffs and landings, not less than 100 flight hours;

Emergency recovery: Automatically return to the designated location according to the scheduled route in case of signal loss, low battery, or abnormal flight status.

Target dragging parameters:

Target structure: cylindrical hard target;

The distance from the released target to the drone shall not be less than 30 meters;

The length of the target after release: not less than 3.5 meters;

The diameter of the target after release: not less than 0.6 meters;

Target weight: not exceeding 0.4kg (excluding infrared source);

Target rope tensile strength: meets the requirements for unmanned aerial vehicle towing and target flight.