| 摘要 |
Channel for automated tracking of aircrafts by direction for laser information and measuring systems with additional possibilities includes control element, block for control of deflectors, laser with pumping, selector of long modes, modified block of deflectors, transmitting optics, receiving optics, photo-detector, broadband amplifier (BA), resonance amplifiers adjusted to respective frequencies of inter-mode beats, detectors, filters, pulse formers, triggers ("1"I"0"), circuits "and", delay lines, counters, digital-analog transformers, low frequency filters, amplifiers (filters) of error signal, executive mechanisms, computer and a – input of support signal with frequency &Dgr;vof transmitting laser, b – input of signal from channel of evaluation of tangent component of velocity (angular velocities) of aircraft (A/C) for adjustment of error of coincidence by angles. After BA modified information block is additionally included for information intercommunication with A/C and if needed formation and processing of its image. |
