| 摘要 |
A channel for measurement of slant range distance to aircrafts with use of the intermodal frequencies and capability of search, formation and processing the aircraft image for a range test complex includes a control element, deflector control unit, pumped laser, longitudinal mode selector with frequency division multiplexing, modified block of deflectors, prisms for the intermodal frequency &Dgr;v, switch for the intermodal frequency &Dgr;vand 2&Dgr;v, transmitting optics, receiving optics, photodetectors, broadband amplifier, modified information block, resonance amplifiers adjusted to respective intermodal frequencies, pulse former, trigger ″1″|″0″, circuit AND, counters (Co), filter with set pass band, detector, differential optics, amplifier, filter, differentiating circuits and rectifiers. After the Co instead of electronic-digital computing machine and display unit for data on slant range R to the aircraft an electronic computer is introduced. |
