| 摘要 |
Channel for measurement of slant range to aircrafts with use of frequencies of intermodal beats and additional scanning includes control element, block for control of deflectors, laser with pumping (Ln), prisms for frequency of intermodal beats, switch for frequencies of intermodal beatsand, transfer optics, receiving optics, photo-detectors, broadband amplifier, information block, resonance amplifiers adjusted to respective frequencies of intermodal beats, pulse former, trigger "1"|"0", circuit “and”, counters, filter with given transmission band, detector, differential optics, amplifier, filter, differential circuits, rectifiers, computer and block for representation of measured information on slant range R to deflectors. |
