| 摘要 |
A channel for measurement of attitude rates of aircrafts with capability of aircraft identification for a combined laser system includes a control element, unit for control of deflectors, pumped laser, longitudinal mode selector, block of deflectors, transmitting optics, receiving optics, photo-detector, broadband amplifier, resonance amplifiers adjusted to respective intermodal frequencies, pulse formers, flip-flops, down counters, AND gates, comparison circuits, electronic computing machine, identification unit and- input of reference signals with intermodal frequencies (,,,) from transmitting laser, b – input of the signal from the channel for measurement of aircraft circumferential velocity (attitude rates). Additionally an optical-electronic module is incorporated, this comprises television and infrared channels. |
