首页> 外国专利> CHANNEL FOR MEASUREMENT OF SLANT RANGE TO AIRCRAFTS WITH MULTIFUNCTIONAL LONGITUDINAL MODE SELECTOR AND POSSIBILITY OF AIRCRAFT IDENTIFICATION FOR LASER INFORMATION AND MEASURING SYSTEM OF A LAUNCH-SITE TEST COMPLEX

CHANNEL FOR MEASUREMENT OF SLANT RANGE TO AIRCRAFTS WITH MULTIFUNCTIONAL LONGITUDINAL MODE SELECTOR AND POSSIBILITY OF AIRCRAFT IDENTIFICATION FOR LASER INFORMATION AND MEASURING SYSTEM OF A LAUNCH-SITE TEST COMPLEX

机译:多功能纵向模式选择器对飞机斜距的测量通道以及飞机发射场和测试场的激光信息和测量系统的飞机识别的可能性

摘要

A channel for measurement of slant range to aircrafts with multifunctional longitudinal mode selector and possibility of aircraft identification for laser information and measuring system of a launch-site test complex comprises a control element, block for control of deflectors, pumped laser, multifunctional longitudinal mode selector, prisms for frequency of inter-mode beats vand 2v, transmitting optics, receiving optics, photo-detectors, broad band amplifier, multi-functional information block with b input of signal of tangent component of velocity (angular velocities) of the aircraft that is measured, resonance amplifiers adjusted to respective frequencies of inter-mode beats, pulse formers, trigger "1"|"0", circuit AND, counters (C), filter with given pass band, detector, differential optics, amplifier, filter, differentiating circuits, rectifiers and a block for representation of measuring information on slant range R to the aircraft. After the C instead of electronic-digital computing machine a computer is included.
机译:带有多功能纵向模式选择器的飞机倾斜距离测量通道,以及用于飞机信息的激光信息识别和发射场测试综合体测量系统的通道,包括控制元件,用于偏转器的控制块,泵浦激光,多功能纵向模式选择器,用于模间拍频2v频率的棱镜,发射光学器件,接收光学器件,光电探测器,宽带放大器,多功能信息块,其中b表示飞机的速度(角速度)的切线分量的输入。测量,将谐振放大器调整为互模拍频的各个频率,脉冲形成器,触发“ 1” |“ 0”,电路AND,计数器(C),具有给定通带的滤波器,检测器,差分光学器件,放大器,滤波器,微分电路,整流器和用于表示飞机倾斜范围R上的测量信息的模块。在C之后而不是电子数字计算机中,包括一台计算机。

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