| 摘要 |
Channel for measurement of radial velocity of aircrafts for LIVS with possibility of search and identification of A includes control element, block for control of deflectors, laser with pumping, selector of long modes, modified block of deflectors, transmission optics, receiving optics, photo-detector, broadband amplifier (BA), resonance amplifiers adjusted to respective frequencies of intermodal beats, pulse formers, circuit “and”, counter, mixers, filter, former of measuring 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 measuring information on radial velocity R' of aircraft (A) and 6&Dgr;&ngr;– input of support frequency (6&Dgr;&ngr;) from transmission laser (Ln+SPM). After BA additionally is included multi-functional information block with b – input of signal of tangent component of velocity (angular velocities( of A that is measured, for information intercommunication with A, and of its identification in case if needed. |
