SkyNav UAV flight tests with liquid payload and interference

The first test was performed at a wind speed of 8-9 m/s. A 990 g liquid payload was attached to the UAV. As you can see, the liquid did not fill the tank completely, so the UAV was subject to disruptions related to the movement of the liquid. Additional disruptions were introduced to the system by violent impacts of the UAV. Later in the flight, the SkyNav stabilizer was tested for the impact of violent maneuvers. As you can see in the film, the SkyNav stabilizer coped very well with all disruptions.e

The second test was similarly performed at a wind speed of 8-9 m/s. A line was attached to the UAV to generate interference. The interference was generated by strong tugs on the line. As you can see in the film, the SkyNav stabilizer coped very well with all interference.