OG-40

The system consists of a ground control station and an unmanned fixed-wing aircraft with proprietary avionics and a flight control system that allows performing flight in case of GNSS signal absence or spoofing. The aircraft can be used with a pneumatic launching system and a parachute or with a wheeled chassis that allows conventional take-off and landing. The aircraft can be equipped with an electric motor or an internal combustion engine. The system has been widely tested in practical applications.