| 摘要 |
Channel for measurement of angular velocities of aircrafts with BSPM and capability of identification of A includes control element, block for control of deflectors, laser with pumping, multi-functional selector of longitudinal modes, block of deflectors, transmitting optics, receiving optics, photodetector, broadband amplifier (BA), resonance amplifiers adjusted to respective frequencies of inter-mode beats, pulse formers, triggers "1"|"0", circuits “and”. Reversing counters, comparison circuits, computer and &Dgr;v- input of support signals with frequencies of inter-mode beats (&Dgr;v, 2 &Dgr;v3&Dgr;v, 6 &Dgr;v) from transmission laser. After BA in place of information block multi-functional information block is included, with b – input of signal of tangent component of velocity (angular velocities) of A that is measured. |
