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Radiogoniometers to find the direction of the waves at very high frequency or ultra high frequency

机译:射线测角仪可在非常高的频率或超高的频率下找到波的方向

摘要

1,060,704. Radio direction finding. MARCONI CO. Ltd. Jan. 24, 1966 [March 2, 1965], No. 8944/65. Heading H4D. A radio direction finder is designed to be less susceptible to changes in polarization of the incoming wave by having a rotating aerial system comprising one aerial receptive only to horizontally polarized waves and one aerial receptive only to vertically polarized waves and alternately switching the outputs of the two aerials to a receiver at a rate high in relation to the rotational rate of the aerial system, such that in the detected output of the receiver, momentary variations in the output of one aerial due to changes in incoming wave polarization are averaged out with the output of the other aerial, and allows a normal phase comparison between the envelope of the detected receiver output and a reference signal in synchronism with the rotation of the aerial system. The system may comprise, Fig. 1, a connected dipole D1 with a parasitic reflector D2, spaced by a quarter wavelength, and susceptible only to vertically polarized waves, and a connected loop L 1 with a parasitic loop L 2 susceptible only to horizontally polarized waves. The aerial system is rotated by a motor M about an axis MS on the end of an arm B at a rate of 1 rev./sec. The polar diagram of each aerial is a cardiod, and signals with sinusoidally varying amplitudes are induced in respective rotary transformer secondaries C 1 and C 2 . The signals from the two aerials are fed to a switching system S which switches the signals to a receiver R alternately at a rate of 1À5 kc./s. The form of the input signal to the receiver R for a polarization direction of 45 degrees is shown in Fig. 2 (not shown). The receiver detects its input signal and passes the resulting envelope to one input of a phase detector PD. The other input is fed by a generator G, coupled to the motor M. The output of the phase detector is fed to a direction indicator I. Although the aerial system can be rotated about an axis passing through the middle thereof, a larger, more accurate base line is simulated by the rotational method described. A second aerial system may be provided rotating with that shown and diametrically opposite thereto, one dealing with V.H.F. waves and the other with U.H.F. waves. Although separate rotary transformers, switching systems &c. would normally be used for each aerial system, a common phase detector, indicator and generator, may be used.
机译:1,060,704。无线电定向。 MARCONI CO.Ltd.1966年1月24日[1965年3月2日],编号8944/65。标题H4D。无线电定向仪的设计使其旋转天线系统包括一个仅接收水平极化波的天线和一个仅接收垂直极化波的天线,并交替切换两者的输出,从而使其不易受到入射波极化变化的影响天线以相对于天线系统的旋转速率较高的速率到达接收器,以便在接收器的检测到的输出中,将由于入射波极化变化而导致的一个天线的输出的瞬时变化与输出进行平均天线的旋转,并允许与天线系统的旋转同步地在检测到的接收器输出的包络和参考信号之间进行正常相位比较。在图1中,该系统可以包括:连接的偶极子D1,其具有寄生反射器D2,其间隔为四分之一波长,并且仅对垂直极化波敏感;以及连接的环路L 1,其具有寄生环路L 2,仅对水平极化敏感。波浪。空中系统通过电机M绕臂B末端上的轴MS以1转/秒的速度旋转。每个天线的极坐标图是一个心形,并且在各个旋转变压器次级C 1和C 2中感应出振幅呈正弦变化的信号。来自两个天线的信号被馈送到交换系统S,该交换系统以1-5 kc./s的速率交替地将信号交换到接收器R。在图2中示出了针对偏振方向为45度的到接收器R的输入信号的形式(未示出)。接收器检测其输入信号,并将得到的包络传递到相位检测器PD的一个输入。另一个输入由耦合到电动机M的发电机G馈送。相位检测器的输出馈给方向指示器I。尽管天线系统可以绕通过其中间的轴旋转,但更大,更大通过所述旋转方法模拟精确的基线。可以提供一个第二天线系统,该第二天线系统与所示的天线系统旋转并在直径上相对地旋转,其中一个与V.H。波浪和另一个与U.H.F.波浪。尽管是单独的旋转变压器,开关系统&c。通常将其用于每个航空系统,可以使用通用的相位检测器,指示器和发生器。

著录项

  • 公开/公告号FR1471303A

    专利类型

  • 公开/公告日1967-03-03

    原文格式PDF

  • 申请/专利权人 MARCONI CO LTD;THE MARCONI COMPANY LIMITED;

    申请/专利号FR19660051680

  • 发明设计人

    申请日1966-03-02

  • 分类号G01S1/02;G01S3/14;

  • 国家 FR

  • 入库时间 2022-08-23 14:02:22

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