| 摘要 |
Channel for measurement of radial velocity of aircrafts with possibility of identification of A for LVS has control element, block for control of deflectors, laser with pumping, selector of long modes, block of deflectors, trsansmission optics, reception optics, photodetector, broadband amplifier (SP), counters, mixers, filters, formers of measuring pulses, decoder, phase auto-adjustment of frequency at frequency of inter-mode beats, control generator, support generator with support frequency, computer, block for representation of information and- input of support frequencyfrom laser-transmitter. After SP there is additionally included block for identification with b – entering signal from channel of measurement of tangent component of rate (angular velocities) of aircraft. |
