Unmanned Aerial Vehicles
Seamless UAV testing technology from real-time virtual testing to physical testing.
Virtual testing enables efficient and safe design, testing and training of UAV control systems. Allows virtual testing throughout the entire development process, from design to verification and validation.
RT Dynamic
  • UAV components library
  • Modular principle of model building
  • Parametric mathematical models of the UAV components
Obstacle Avoidance with Stereo Vision Camera system
To develop real-time autonomous obstacle avoidance problem of the various collisions during the flight through the target path we use simulation system which provides real word data virtually without any actual UAV or Real Cameras. obstacle avoidance calculated according to the obstacle information based on known data or data coming from an onboard detection system in real time form 3 dimensional virtual space.
Target Tracking
Target Tracking is one of important capabilities of the nowadays Unmanned Aerial Vehicles. In the development process physical testing on UAV might me costly and time consuming. To resolve this issue, we developed our simulation system, which includes GPU based PC for the 3D virtual environment and RTC for UAV plant model real time execution. This system allows virtually test Flight control units and onboard video processing devices without harming any actual hardware.
Semi-natural UAV tests
Hybrid technology is an integration of virtual and physical testing in which a model of the environment and vehicle dynamics is combined with the control system of the test bench and the test object. The technology creates a test environment for the physical object and ECU that is close to real-world testing.
A semi-natural simulation of the flight mode of an unmanned aerial vehicle is carried out to confirm the virtual tests of the digital twin. In this case, data about the position of the aircraft in space is simulated, and the glider and its components are full-scale objects.
The engine model is verified in various operating modes as a result of HIL tests.
Developed aerodynamic balance for measuring the thrust vector and thrust of the UAV.
Also, this unit can be installed in a wind tunnel to measure the characteristics of the airframe.