| 摘要 |
Channel for automated tracking aircrafts in direction has control element, block for control of deflectors, laser with pumping (Lp), deflector block, transmission optics, receiving 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 frequency &Dgr;&ngr;of transmission laser, b- input of signal from channel for evaluation of tangent component of velocity (angular velocities) of aircraft (A) for adjustment of error of coincidence by angles, information block for information communication with A. After Lp multi-channel selector of longitudinal modes is additionally included. |
