| 摘要 |
Channel for measurement of radial velocity of aircrafts with possibility of formation and processing image of A for LVS has control element, block for control of deflectors, laser with pumping (Ln), block of deflectors, transmission optics, receiving optics, photodetector, broadband amplifier (SP), resonance amplifiers adjusted to respective frequencies of inter-mode beats, pulse formers, circuits “and”, counters, mixers, filters, formers of measure pulses, decoder, phase auto-adjustment of frequency at frequency of inter-mode beats, control generator, support generator with support frequency &Dgr;&ngr;, computer, block for representation of information and &Dgr;&ngr;– input of support frequency (&Dgr;&ngr;) from laser-transmitter. After Ln there is additionally included modified selector of long modes and after SP block for formation of image is additionally included. |
