| 摘要 |
Channel for measurement of angular velocities of aircrafts that has control element, block for control of deflectors, pumped laser (Ln), deflector block, transfer optics, receiving optics, photo-detector, broadband amplifier, information block, resonance amplifiers adjusted to respective frequencies of inter-mode beats, pulse formers, triggers "1"|"0", of circuit "AND", reversing counters, comparison circuits, electronic-digital computer and Dnm– input of support signals with frequencies of inter-mode bits (Dnm, 2 Dnm, 3 Dnm, 6 Dnm) from transmitting laser. After Ln multi-0channel selector of longitudinal modes is additionally included. |
