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Intelligent Counter-UAS System

Low-Altitude Threat
Interception System

A portable system designed to counter low-altitude FPV, rotary-wing and other low-slow-small unmanned aircraft. It combines high-speed interceptors, handheld control and launch storage with radar or electro-optical cueing for a rapid deployment, autonomous search and autonomous interception workflow.

6-UAV SystemRadar / EO CueingSemi & Full Autonomous13 kg Complete System
Request System BriefCounter-UAS Applications
6-inch high-speed Counter-UAS interceptor from the supplied product brief
6
Interceptors
4 km+
Control Radius
300 m+
Recognition
3 min+
Endurance
System Composition

One Portable Three-Part System

The documented package combines intercept aircraft, mission control and launch support in a complete 13 kg system.

6-Inch High-Speed UAV
01 / INTERCEPT× 6

6-Inch High-Speed UAV

A compact four-rotor interceptor with aerodynamic shaping, semi-autonomous and fully autonomous control modes, and swarm-controller support for coordinated missions.

  • 1.2 kg maximum takeoff weight
  • 150 g+ payload capacity
  • 4 km+ control radius
5.5-Inch Handheld Controller
02 / COMMAND× 1

5.5-Inch Handheld Controller

A high-brightness handheld terminal running Flymate intelligent-control software for mission planning, cooperative control and rapid target-tracking actions.

  • High-brightness display
  • Multi-aircraft cooperative control
  • Target tracking and mission shortcuts
Launch-and-Storage Box
03 / DEPLOY× 1

Launch-and-Storage Box

An integrated transport, information-extension and charging carrier with internal launch rails and powered standby support for stored aircraft.

  • Six-aircraft storage architecture
  • Rail-assisted rapid deployment
  • Integrated power management
Source-Backed Parameters

Core Technical Specifications

These values reproduce the completed fields in the supplied product brief. Draft placeholders and unfilled table cells have been excluded.

Speed Definition

The specification table lists 30 m/s strike speed and 40 m/s flight speed. The high-speed-UAV feature page separately states an instantaneous top speed of up to 180 km/h.

Technical Data Dossier · Supplied Brief
Maximum Takeoff Weight
High-speed UAV
1.2 kg
Payload Capacity
High-speed UAV
150 g+
Maximum Strike Speed
Mission profile
30 m/s
108 km/h
Maximum Flight Speed
Flight profile
40 m/s
144 km/h
Endurance
High-speed UAV
3 min+
Control Radius
System link
4 km+
Target Identification Distance
Onboard recognition
300 m+
Complete System Weight
System level
13 kg
Including launch box
Subsystem Capabilities

Aircraft, Control and Launch Support

Three integrated functions · one portable package
Six-inch high-speed interceptor UAV
6-Inch High-Speed UAV

Aerodynamic Interceptor Architecture

The four-rotor platform adds aerodynamic shaping for a documented instantaneous top speed of up to 180 km/h. Semi-autonomous and fully autonomous control modes support different mission-control requirements.

180 km/h
Instantaneous top speed
2
Control modes
Swarm
Strategy execution
5.5-inch handheld intelligent controller

5.5-Inch Handheld Controller

  • High-brightness mission display
  • Flymate planning and cooperative-control software
  • Rapid target tracking and terminal-action shortcuts
  • Swarm-controller group strategy execution
Launch-and-storage box equipment illustration supplied in the product brief

Launch-and-Storage Box

  • Information-interaction extension carrier
  • Integrated aircraft charging support
  • Internal rails for rapid post-start exit
  • Powered standby during carriage and mission waiting
Cooperative Guidance

Sensor-to-Intercept Mission Chain

External detection, intercept-area calculation, guided dispatch and autonomous terminal search form the documented operational sequence.

Original cooperative-guidance workflow diagram from the supplied Counter-UAS product brief
Original workflow diagram · supplied product brief · paired with English sequence
STEP 01

External Detection

Radar and electro-optical reconnaissance equipment acquire airborne-target information.

STEP 02

Intercept-Area Calculation

The upper-level command-and-control system calculates an estimated intercept area.

STEP 03

Guided Dispatch

The handheld controller dispatches and guides the high-speed UAV to the intercept area.

STEP 04

Autonomous Search & Intercept

The aircraft searches for the target and executes the configured interception task.

Multiple Incoming Targets

For multiple incoming aircraft, the documented swarm controller uses optical and radar-derived target features to allocate an engagement strategy and assign time-separated tasks within the estimated intercept area.

Related Mission Planning

Counter-UAS Applications

Operational context for low-altitude drone threats

Perimeter Security & Patrol

Connect airspace monitoring with site-protection planning

Mission Scenarios

Illustrative configuration and acceptance frameworks

SOURCE-BACKED FAQ

Intelligent Counter-UAS System Questions

Answers are limited to the supplied product brief.

The supplied product brief identifies low-altitude FPV drones, rotary-wing drones and other low-slow-small unmanned aircraft as the intended target set.

The documented system composition is six 6-inch high-speed UAVs, one 5.5-inch handheld controller and one launch-and-storage box. The complete system weight, including the launch box, is listed as 13 kg.

Radar or electro-optical equipment supplies target information to an upper-level command-and-control system. That system calculates an estimated intercept area and passes it to the handheld controller, which guides the interceptor to the area for autonomous target search and interception.

The high-speed UAV supports semi-autonomous control and fully autonomous automatic control. The system also uses a swarm controller to support coordinated group-strategy execution for multiple incoming targets.

They describe different conditions. The main parameter table lists 30 m/s maximum strike speed and 40 m/s maximum flight speed. A separate high-speed-UAV feature page states an instantaneous top speed of up to 180 km/h after aerodynamic shaping.

The box integrates transport and storage, information interaction extension, charging support, internal launch rails for rapid exit after motor start, and power management for aircraft standby while carried or awaiting a mission.

Configuration Review

Request the System Technical Brief

Discuss external sensor interfaces, mission-control workflow, system composition and acceptance requirements with the engineering team.

Request System Brief