| 摘要 |
Channel for measurement of slant range to aircrafts for laser information and measuring systems with possibility of search and identification of A/C includes control element, block for control of deflectors, laser with pumping, 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;, transmitting optics, receiving optics, photo=detectors, broadband amplifier (BA), resonance amplifiers adjusted to respective frequencies of inter-mode beats, pulse former, trigger "I"I"0", circuit "and", counters, filter with given pass band, detector, differentiated optics, amplifier, filter, differentiating circuits, rectifiers, computer and block for representation of measured information on slant range R to the aircraft (A). After BA there is additionally included multi-functional information block with b – input of signal of tangent component of velocity (angular velocities) of A/C that is measured, for information intercommunication with A/C and, if needed, formation and processing of its image. |
