| 摘要 |
A channel for measurement of angular velocities of aircrafts for a combined laser system includes a control element, deflector control unit, pumped laser, longitudinal mode selector, modified block of deflectors, transmitting optics, receiving optics, photo-detector, broadband amplifier, resonance amplifiers adjusted to respective intermodal frequencies, pulse formers, flip-flops, reversing counters, AND gates, comparison circuits (CC) and Δν– input of reference signals with intermodal frequencies (Δν, 2Δν, 3Δν, 6Δν) from transmitting laser. Additionally optic-electronic module (OEM) is incorporated, this comprises television and infrared channels, and after the CC instead of electronic-computing machines and information display units an electronic computing machine connected to OEM is incorporated. |
