UXT Systems · Unmanned Technologies

Research and Development of Unmanned Systems, AI Models, Counter-UAS and Jet Turbines

UXT Systems conducts research and development on key technologies for unmanned aerial and ground systems. The focus is on integrated system architectures, embedded artificial intelligence, multi-sensor methods for drone detection, and the integration of compact jet turbines into unmanned platforms.

Unmanned jet-powered drone with delta wings, top view
  • SystemsConcept to flight testing
  • Onboard AIReal-time inference on board
  • C-UASMulti-sensor detection
  • Jet TurbinesTurbine engines for UAS

Research & Development

Research Areas: System Architecture, Artificial Intelligence, Counter-UAS and Jet Turbines

At UXT Systems, platform, algorithms, sensors and engines are developed as one integrated system – from the concept phase to flight testing.

  • 01

    Architecture and Integration of Unmanned Aerial and Ground Systems

    The performance of an unmanned system is determined at the interfaces between its components. We therefore design airframe, powertrain, power supply, flight control, sensors and data link together from the outset, implement new concepts on test vehicles and verify them step by step in laboratory, ground and flight tests. A key research focus is robust navigation in environments where GNSS is degraded or unavailable.

    System Architecture · Test Vehicles · PX4 · ArduPilot · GNSS-Denied Navigation · Sensor Fusion

  • 02

    Onboard Artificial Intelligence for Unmanned Systems

    Autonomy requires a system to perceive and interpret its environment independently – even when the link to the ground control station is degraded or lost entirely. We develop neural network models for object detection, classification and scene understanding and optimize them for deployment on energy-efficient edge hardware. They are evaluated against defined metrics for detection performance, latency and robustness to real-world, noisy sensor data.

    Computer Vision · Edge Inference · Model Optimization · Sensor Fusion · Autonomy

  • 03

    Counter-UAS: Detection, Tracking and Classification of Non-Cooperative Drones

    Small unmanned aircraft operate at low altitude and low speed with a minimal signature – characteristics that make them considerably harder to detect. We investigate how complementary sensing principles – RF detection, radar, electro-optical and infrared imaging, and acoustics – can be fused into a reliable common operating picture. AI-based classification methods help to reliably distinguish drones from birds and other clutter.

    Counter-UAS · RF · Radar · EO/IR · Sensor Fusion · Common Operating Picture

  • 04

    Jet Turbines for High-Speed Unmanned Aircraft

    Electric motors can achieve high flight speeds and long ranges only to a limited extent. Compact jet turbines give unmanned platforms a significantly extended performance envelope. Our work covers the aerodynamic and structural design of the airframe, the design of the fuel system, the integration of the engine control unit with autopilot and telemetry, and thermal management. Validation proceeds in stages, from the engine test stand to flight testing.

    Jet Turbines · ECU Integration · Fuel System · Thermal Management · Test Stand

Technologies

Technologies and Components for Unmanned Systems

  • Flight Control

    Open autopilot platforms such as PX4 and ArduPilot as the basis for custom control and mission functions.

  • Edge Computing

    High-performance companion computers for real-time image processing and AI inference on board.

  • Sensor Fusion

    State estimation from IMU, GNSS, LiDAR and camera data for precise and robust navigation.

  • LiDAR & Camera

    Three-dimensional environment perception as the basis for GNSS-independent navigation.

  • EO/IR & Radar

    Complementary sensors for detecting small targets with a low signature.

  • Data Link

    Telemetry and video transmission via radio, cellular networks or optical fiber.

  • Jet Turbines

    Compact turbine engines with an electronic engine control unit (ECU).

  • Test Stand

    Instrumented measurement of thrust, exhaust gas temperature and fuel consumption prior to flight testing.

Contact

You can reach us by phone or email.

+49 151 25318678