| 摘要 |
Channel for measurement of slant range distance to aircrafts with additional scanning and possibility of identification of A includes control element, block for control of deflectors, laser with pumping, multi-channel selector of long modes, prisms for frequency of inter-mode beats &Dgr;&ngr;, modified block of deflectors, switch for frequencies of inter-mode beats &Dgr;&ngr;and 2&Dgr;&ngr;, transmission optics, receiving optics, photodetectors, broadband amplifier (BA), resonance amplifiers adjusted to respective frequencies of inter-mode beats, pulse former, trigger "1"|"0", circuit “and”, counters, filter with given pass band, detector, differential optics, amplifier, filter, differential circuits, rectifiers, computer and block for representation of measuring information on slant range R to aircraft. After BA instead of information block multi-functional information block is included with b – input of signal of tangent component of velocity (angular velocities) of aircraft that is measured. |
