| 摘要 |
A channel for measurement of angular velocities of aircrafts for laser measuring system of a range test complex comprises a control element, block for control of deflectors, pumped laser, longitudinal-mode selector, block of deflectors, transmitting optics, receiving optics, photodetector, broadband amplifier, resonance amplifiers adjusted to respective frequencies of inter-mode beats, pulse formers, triggers, circuits AND, resonance counters, comparison circuits (CC) and ∆&ngr;– input of reference signals with frequencies of inter-mode beats (∆&ngr;, 2∆&ngr;, 3∆&ngr;, 6∆&ngr;) from transmitting laser. After CC instead of electronic-digital computing machine and blocks for display of information electronic computer is introduced. |
