| 摘要 |
Channel for measurement of slant range to aircrafts with additional possibilities includes control element, block for control of deflectors, laser with pumping, selector of long modes (SLM), prisms for frequency of inter-mode beats &Dgr;vM, switch for frequencies of inter-mode beats &Dgr;vM and 2&Dgr;vM, transmission optics, receiving optics, photodetectors, broadband amplifier, information block, resonance amplifiers adjusted to respective frequencies of inter-mode beats, pulse former, trigger "1"|"0", circuit “and”, counters, filter with given transmission band, detector, differential optics, amplifier, filter, differentiated chains, rectifiers, electronic-digital computer and block for representation of measuring information on slant range R to aircraft. After SLM modified block of deflectors is additionally included. |
