 | Optical-electronic system Lanner-A (NV5-0101)Lanner-A (NV5-0101) is an autonomous gyrostabilized optical-electronic observation device. The device is an air-borne system for subsonic aviation and is designed for 24-hour and all-weather survey of the lower hemisphere (observation of surface and above-water objects) through television and infrared imaging channels. |
 | Optical-electronic system Lanner-MThe system Lanner-M is designed for aircraft of the Russian Emergency Ministry. |
 | Optical-electronic system Lanner-VThe optical-electronic system Lanner-V is specially designed to be installed on helicopters. Gyroplatform of the system has been improved with optical units for protection against the inherent excessive vibrations of helicopters. Lanner-V is designed for 24-hour and all-weather surveillance of the lower hemisphere (observation of surface and above-water objects) through television and infrared imaging channels. |
 | Optical-electronic system Laggar-DLaggar-D is to be installed on unmanned aircrafts, helicopters, aerostats and airships; it is designed for downward visibility (monitoring on-land and above-water objects) through a television camera. |
 | Two-axle gyro-stabilized suspension systemTwo-axle gyro-stabilized suspension system (GSS) for radar antennas of helicopter. GSS stabilizes antenna system and protects it from external impacts (shocks, vibrations, etc.) that, in its turn, significantly increases operational accuracy of radar system. |
 | Three-axle gyro-stabilized suspension systemThree-axle gyro-stabilized suspension system (GSS) is intended for use in the stabilized antenna system of radar station of the side looking, installed on the unmanned aerial vehicle (UAV). GSS provides control and stabilization of the side looking antenna, and protects it from external influences (blows, vibrations, etc.). |
