| 摘要 |
Channel for measurement of angular velocities of aircrafts with possibility of formation and processing of image of A for AMF includes control element, block for control of deflectors, laser woith pumping (Ln), block of deflectors, transmission optics, receiving optics, photodetector, broadband amplifier (BA), resonance amplifiers adjusted to respective frequencies of inter-mode beats, pulse formers, triggers, circuits “and”, resonance counters, comparison circuits, computer and blocks for representation of information, &Dgr;&ngr;– input of support signals with frequencies of inter-mode beats (&Dgr;&ngr;, 2&Dgr;&ngr;, 3&Dgr;&ngr;, 6&Dgr;&ngr;) from transmission laser. After Ln modified selector of longitudinal modes is additionally included and after PB block for formation of image is additionally included. |
