| 摘要 |
Channel of automated following aircrafts by direction with additional scanning for LVS includes control element, block for control of deflectors, laser with pumping, selector of long modes (SLM), transmission optics, reception optics, photo detector, broadband amplifier, resonance amplifiers adjusted to respective frequencies of inter-mode bits, detectors, filters, pulse formers, triggers ("1"|"0"), circuits “and”, delay lines, counters, digital-analog transformers, low frequency filters, amplifiers (filters) of error signal, executive mechanisms, electronic-digital computer and a – input of support signal with frequencyof transmission laser, b – input of signal from channel for evaluation of tangent component of velocity (angular velocities) of aircraft for adjustment of error of coincidence by angles. After SLM modified block of deflectors is additionally included. |
