DETECT
Small Low-Altitude Targets
Site sensors must acquire and maintain useful target information for FPV, rotary-wing and other low-slow-small unmanned aircraft.
Low-Altitude Airspace Protection
Counter-UAS
Interception Operations
Operational integration for low-altitude FPV, rotary-wing and other low-slow-small unmanned-aircraft threats. The documented workflow connects external sensing and command-area calculation with portable guided dispatch, autonomous search and configured terminal interception.
Externally Cued6 InterceptorsPortable 13 kg PackageSemi & Full Autonomous
4 km+
Documented control radius
300 m+
Onboard identification distance
3 min+
Aircraft endurance
13 kg
Complete package incl. launch box
Operational Context
Close the Sensor-to-Response Gap
The application is not a standalone detection network. It is a portable interception layer that depends on timely external target cues, a defined command handoff and a controlled response area.
CONNECT
Command Handoff
The upper-level command system converts the available track into an estimated intercept area that can be used by the handheld controller.
RESPOND
Portable Interception
A selected aircraft is dispatched toward the estimated area for autonomous search and the configured terminal interception task.
Documented Mission Chain
From External Cue to Terminal Search
The sequence below mirrors the supplied system brief and separates external detection and command functions from the portable interceptor package.
STEP 01External sensor input
External Detection
Radar or electro-optical reconnaissance equipment acquires airborne-target information and passes the cue to the upper-level command system.
STEP 02External C2 function
Intercept-Area Calculation
The upper-level command-and-control system calculates an estimated intercept area from the available target track.
STEP 03System guidance stage
Guided Dispatch
The handheld intelligent controller dispatches and guides a high-speed UAV toward the calculated intercept area.
STEP 04Aircraft terminal stage
Autonomous Search & Intercept
The aircraft searches within the estimated area and performs the configured terminal interception task.
Mission Configuration
One Documented Three-Part Package
INTERCEPT× 6
6-Inch High-Speed UAV
Compact four-rotor intercept aircraft with aerodynamic shaping, semi-autonomous and fully autonomous control modes, and cooperative-control support.
- 1.2 kg maximum takeoff weight
- 150 g+ payload capacity
- 4 km+ documented control radius
COMMAND× 1
5.5-Inch Handheld Controller
High-brightness mission terminal running Flymate intelligent-control software for planning, cooperative control and rapid target-tracking actions.
- Mission planning interface
- Multi-aircraft cooperative control
- Tracking and terminal-action shortcuts
DEPLOY× 1
Launch-and-Storage Box
Integrated transport, information-extension and charging carrier with internal launch rails and powered standby support.
- Six-aircraft storage architecture
- Rail-assisted rapid deployment
- Integrated charging and standby support
Integration Boundary
Radar, electro-optical reconnaissance equipment and the upper-level command-and-control system are external integration elements. They are not listed as part of the documented 13 kg three-part package.
Deployment Planning
Three Integration Profiles
These are planning profiles, not completed customer deployments or effectiveness claims. Each project requires a site-specific concept of operations and controlled acceptance testing.
PROFILE 01
Fixed-Site Low-Altitude Protection
Connect existing site radar or electro-optical detection with an upper-level command system and a nearby portable interceptor package.
- Define sensor-to-controller handoff
- Plan launch-box placement and access
- Establish the permitted response area
PROFILE 02
Mobile Response Team
Use the 13 kg complete package as a relocatable response element while external sensing and command resources provide target cues.
- Confirm communications continuity
- Verify aircraft charge and standby state
- Predefine safe dispatch sectors
PROFILE 03
Layered Perimeter Integration
Position the system as an interception layer within a broader perimeter-security design rather than as a standalone detection network.
- Map responsibility across sensor and C2 layers
- Define track-quality thresholds
- Document escalation and authorization steps
Acceptance Framework
Validate the Complete Mission Chain
Procurement acceptance should prove interfaces and responsibilities from external detection through controlled terminal behavior, not just validate individual component power-on.
Request Integration Review01
Radar or electro-optical target information is handed off to the designated upper-level command system.
02
The command system produces an intercept-area estimate that can be received by the handheld controller.
03
The controller dispatches and guides the selected aircraft to the planned mission area.
04
Autonomous search behavior is evaluated within an approved and controlled test volume.
05
Aircraft storage, charging, powered standby and rail-assisted exit are checked as one deployment sequence.
06
End-to-end drills define authorization, abort, recovery and post-mission inspection responsibilities.
Application Questions
Counter-UAS Deployment FAQ
What threat types is this application intended to address?
The supplied brief positions the system against low-altitude FPV, rotary-wing and other low-slow-small unmanned aircraft. Final suitability depends on target characteristics, sensor coverage, engagement policy and site-specific testing.
Does the documented 13 kg package include radar or electro-optical sensors?
No. The documented package comprises six high-speed UAVs, one handheld controller and one launch-and-storage box. Radar, electro-optical reconnaissance equipment and the upper-level command-and-control system are external cueing and integration elements.
How does a target cue become an interception task?
External sensors acquire target information, the upper-level command system calculates an estimated intercept area, the handheld controller dispatches the aircraft, and the aircraft performs autonomous search and the configured terminal task within that area.
Which aircraft-control modes are described?
The product brief describes semi-autonomous and fully autonomous control modes, plus multi-aircraft cooperative-control functions in the handheld software. The selected mode should be governed by the approved concept of operations and local rules.
Which values define the application planning envelope?
The completed source fields include a 4 km+ control radius, 300 m+ onboard target-identification distance, 3 min+ endurance and 13 kg complete-system weight. The product page remains the authoritative location for the full specification set and speed definitions.
What should be validated before deployment?
Acceptance planning should cover sensor handoff, command-system output, controller guidance, aircraft search behavior, charging and standby readiness, launch sequence, communications, authorization and controlled end-to-end drills.
Related Planning Paths