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Improvements relating to radar aerial systems

机译:与雷达空中系统有关的改进

摘要

767,537. Radio direction-finding. BRITISH THOMSON-HOUSTON CO., Ltd. June 21, 1955 [July 2, 1954], No. 19493/54. Class 40(7) Radar equipment of the kind in which error signals are derived so that the aerial system may be maintained i n alignment with the target includes an aerial system consisting of three aerials having overlapping beam patterns symmetrica 1 1 y arranged about an axis and such that comparison of the signals derived from two of the aerials determines an error signal in respect of one plane and comparison of the signal from the third aerial 'and the combined signals from the first two determines a error in a second plane - perpendicular to the first. The aerials may - be waveguide horns arranged as shown at A, B and C and facing out of the plane of the paper; a common focusing lens is placed in front of the horns to give over-' lapping divergent radiation patterns (Fig. 1, not shown). It is shown by means of a mathematical discussion referring to Figs. 2 and 4 (both not shown) that if a, b and c 'are the signals obtained from aerials A, 'B, and C respectively then the azimuth error will be proportional to: and the elevation error to: In the preferred waveguide network for obtaining signals-of these values the signal b is first retarded in phase by 90 degrees .arid then fed to a 3dB coupler X along ,with signal c. The output of the coupler at CSP1/SP is #¢ (c - b) which is the azimuth error divided by #SP3/SP/ 2 . The other output of coupler X is fed to 4.77dB coupler Y along with signal a to give an output at ASP1/SP of #2/3 (a-b/2 - c/2) which is the elevation error divided by the same constant #3/2. It may be noted that the signals fed through a 90 degree phase advancer if required, add at the output B' and that, regarding the network from this end, a transmitter may'be connected at this point to give an equal intensity of transmission from each of the aerials A, B. and C. The error signals at ASP1/SP and CSP1/SP may be combined in a further 3dB coupler to give two output signals either of which represents the resultant error signal in magnitude and phase angle relative to the combined sum signal output at BSP1/SP. (The phase angles of these outputs are measured in opposite directions from the reference.)
机译:767,537。无线电测向。英国汤姆逊·休斯顿有限公司。1955年6月21日[1954年7月2日],编号19493/54。第40(7)类雷达设备,其中可以得出误差信号,以使航空系统保持与目标对齐,该航空系统包括一个由三个天线组成的天线系统,三个天线具有围绕轴线布置的对称波束1 1 y重叠,因此,比较两个天线的信号确定一个平面的误差信号,比较第三天线的信号和前两个天线的组合信号确定第二平面的误差-垂直于第一。天线可能是-如图A,B和C所示排列且面朝纸面之外的波导喇叭;一个普通的聚焦透镜放置在喇叭的前面,以给出重叠的发散辐射图(图1,未显示)。通过参考图1和2的数学讨论来示出。从图2和图4(均未示出)可以看出,如果a,b和c'分别是从天线A,'B和C获得的信号,则方位角误差将与:和仰角误差成比例:在优选的波导网络中为了获得这些值的信号,首先将信号b在相位上延迟90度,然后与信号c一起馈入3dB耦合器X。 C 1 处的耦合器输出为#¢(c-b),即方位角误差除以# 3 / 2。耦合器X的另一输出与信号a一起馈入到4.77dB耦合器Y,以在A 1 的#2/3(ab / 2-c / 2)输出,这是仰角误差除以相同的常数#3/2。可以注意到,如果需要的话,通过90度相位前馈器馈入的信号在输出B'处相加,并且对于从此端开始的网络,可以在此点连接一个发射机,以提供相等的发射强度。 A 1 和C 1 处的误差信号可以在另一个3dB耦合器中组合以提供两个输出信号代表相对于在B 1 输出的组合和信号的幅度和相位角的所得误差信号。 (这些输出的相角是在与基准相反的方向上测量的。)

著录项

  • 公开/公告号GB767537A

    专利类型

  • 公开/公告日1957-02-06

    原文格式PDF

  • 申请/专利权人 THE BRITISH THOMSON - HOUSTON COMPANY LIMITED;

    申请/专利号GB19540019493

  • 发明设计人 MILNE KENNETH;

    申请日1954-07-02

  • 分类号G01S1/02;G01S13/44;

  • 国家 GB

  • 入库时间 2022-08-23 22:12:31

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