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CHANNEL FOR MEASUREMENT OF ANGULAR RATE OF AIRCRAFTS WITH ADDITIONAL SCANNING AND POSSIBILITY OF IDENTIFICATION OF A

机译:用附加扫描和识别A的可能性测量角速度的渠道。

摘要

Channel for measurement of angular rate of aircrafts with additional scanning and possibility of identification of A includes control element, block for control of deflectors, laser with pumping, multi-functional selector of long modes, modified block of deflectors, transmission 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 v input of support signals with frequencies of inter-mode beats (v, 2v, 3v, 6v) from transmission laser. After BA instead of information block multi-functional information block is included with b input of signal of tangent component of velocity (angular velocities) of aircraft that is measured.
机译:具有附加扫描功能和可能识别A的飞机角速度测量通道,包括控制元件,用于控制偏转器的模块,带泵浦的激光器,长模式的多功能选择器,经过改进的偏转器模块,传输光学器件,接收光学器件,光电检测器,宽带放大器(BA),已根据模间差拍的各个频率进行调整的谐振放大器,脉冲形成器,触发器“ 1” |“ 0”,电路,以及反向计数器,比较电路,计算机和具有频率的支持信号的v输入传输激光的模式间节拍(v,2v,3v,6v)的变化在b而不是信息块之后,多功能信息块包括在b的输入中,该b是所测量的飞机速度(角速度)的切线分量信号。

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