| 摘要 |
Channel for automated tracking of aircrafts by direction for laser information and measuring systems with possibility of identification of A includes control element, block for control of deflectors. Laser with pumping, selector of long modes, 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 for evaluation of tangent component of velocity (angular velocities) of aircraft (A/C) for adjustment of error of coincidence by angles. After BA there is additionally included multi-functional information block for information intercommunication with A/C and if needed its identification. |
