首页> 外国专利> A method for detecting and direction finding RADAR

A method for detecting and direction finding RADAR

机译:一种雷达定位测向方法

摘要

method u043eu0431u043du0430u0440u0443u0436u0435u043du0438u00a0 and u043fu0435u043bu0435u043du0433u043eu0432u0430u043du0438u00a0 radio signals, u0437u0430u043au043bu044eu0447u0430u044eu0449u0438u0439u0441u00a0 reception signals by u043du0435u043du0430u043fu0440u0430u0432u043bu0435u043du043du044bu0445 antennas comprising n - u044du043bu0435u043cu0435u043du0442u043du0443u044e u0430u043du0442u0435u043du043du0443u044e bars measured at the terminals of integrated antenna and radio signals, convert them into the angular range of the first u043fu043eu0440u00a0u0434u043au0430, determining the maximum u0437u043du0430u0447u0435u043du0438u00a0 and coordinates his u043cu043eu0434u0443u043bu00a0 square.with the transformation of the angular range of the first u043fu043eu0440u00a0u0434u043au0430 u0432u044bu043fu043eu043bu043du00a0u044eu0442 formula;where is the u043au043eu043cu043fu043bu0435u043au0441u043du0430u00a0 amplitude signals at the output of n th antenna, n = 1, 2,...n is the number of antennas, n, (,) - raid phases signal field u0440u0430u0441u043fu043eu043bu043eu0436u0435u043du0438u00a0 antennas, the angles of arrival of radio waves in the horizontal and the vertical plane (u043cu043du0438u043c u0430u00a0 unit u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0, after u0438u0437u043cu0435u0440u0435u043du0438u00a0 complex amplitude signals, u043eu043fu0440u0435u0434u0435u043bu00a0u044eu0442 their average cumulative antenna powerthe angular range of the first u043fu043eu0440u00a0u0434u043au0430 transforming the coordinates of the maximum in the angular spectrum of the second u043fu043eu0440u00a0u0434u043au0430, u043eu043fu0440u0435u0434u0435u043bu00a0u044eu0442 coordinates and the importance of maxim smart grid it u043cu043eu0434u0443u043bu00a0 which and the value of maximum angular range of the first u043fu043eu0440u00a0u0434u043au0430 square u043cu043eu0434u0443u043bu00a0 u043du043eu0440u043cu0438u0440u0443u044eu0442 at high power, and on the basis of normalization and the coordinates u0441u0443u0434u00a0u0442 maximums of radio signals and the corners of their parish.in this u043du043eu0440u043cu0438u0440u043eu0432u0430u043du043du044bu0435 u0437u043du0430u0447u0435u043du0438u00a0 maximums squares modules u0441u0443u043cu043cu0438u0440u0443u044eu0442 angular spectra and compared with the first threshold, above which no u043eu043fu0440u0435u0434u0435u043bu00a0u044eu0442 dmv u0443u0442u0441u0442u0432u0438u0435 radio signalsotherwise, u043eu043fu0440u0435u0434u0435u043bu00a0u044eu0442 relevant result u0432u044bu0447u0438u0442u0430u043du0438u00a0 of unit amount of maximums squares modules angular spectra result from fundamental units u0432u044bu0447u0438u0442u0430u043du0438u00a0 u043du0438u00a0 maximum angular range of the first u043fu043eu0440u00a0u0434u043au0430 square u043cu043eu0434u0443u043bu00a0 received treatment, and compared with the second threshold, the exceeding of which are available on the u0434u043du043eu0433u043e signal, otherwise the two radio signalswith the transformation of the angular range of the second u043fu043eu0440u00a0u0434u043au0430 u0432u044bu043fu043eu043bu043du00a0u044eu0442 formula;where is the u043du043eu0440u043cu0438u0440u043eu0432u0430u043du043du0430u00a0 radiation pattern antenna bars in the orientation in the direction of the maximum angular range of the first time u043cu043eu0434u0443u043bu00a0 square u00a0u0434u043au0430 and u0437u043du0430u0447u0435u043du0438u00a0 thresholds set by the criterion of neumann - pearson, u0438u0441u0445u043eu0434u00a0 u0432u0435u0440u043eu00a0u0442u043du043eu0441u0442u0438 of a false alarm, the quantity of u0440u0430u0441u043fu043eu043bu043eu0436u0435u043du0438u00a0 antennas, it the wave u0438u0437u043bu0443u0447u0435u043du0438u00a0 and the specified error u043fu0435u043bu0435u043du0433u043eu0432u0430u043du0438u00a0.
机译:方法 u043e u0431 u043d u0430 u0440 u0443 u0436 u0435 u043d u043d u0438 u00a0和 u043f u0435 u043b u0435 u043d u0433 u043e u043e u0432 u0430 u043d u0438 u00a0信号, u0437 u0430 u043a u043b u044e u0447 u0430 u044e u0449 u0438 u0439 u0441 u00a0通过 u043d u0435 u043d u0430 u043f u0440 u0430 u0432 u043b u0435接收信号 u043d u043d u044b u0445包含n个天线- u044d u043b u0435 u043c u0435 u043d u0442 u043d u0443 u044e u0430 u043d u0442 u0432 u0435 u043d u043d u043d u0443 u044e在集成天线和无线电信号的端子处,将它们转换为第一个 u043f u043e u0440 u00a0 u0434 u043a u0430的角度范围,确定最大 u0437 u043d u0430 u0447 u0435 u043d u0438 u00a0,并通过转换第一个 u043f u043e u0440 u00a0 u0434 u043a u0430 u0432 u043b u043b u043c u043e u0434 u0434 u0433 u043e u043b u043d u00a0 u044e u0442公式; u043a u043e u043c u043f u043b u0435在哪里 u043a u0441 u043d u0430 u00a0第n个天线输出处的幅度信号,n = 1、2,... n是天线的数量n,(,)-突袭相位信号场 u0440 u0430 u0441 u043f u043e u043b u043e u0436 u0435 u043d u0438 u00a0天线,水平和垂直平面中无线电波的到达角度( u043c u043d u0438 u043c u0430 u00a0单元 u043e u0442 u043b u0438 u0447 u0430 u044e u0449 u0438 u0439 u0441 u0040,在 u0438 u0437 u043c u0435 u0440 u0435 u043d u043d u0438 u00a0复振幅信号之后, u043e u043f u0440 u0435 u0434 u0435 u043b u00a0 u044e u0442它们的平均累积天线功率第一个 u043f u043e u0440 u00a0 u0434 u043a u0430的角度范围将最大坐标转换为 u043f u043e u0440 u00a0 u0434 u043a u0430, u043e u043f u0440 u0435 u0434 u0435 u043b u00a0 u044e u0442的角度光谱及其maxim智能网格的重要性u043c u043e u0434 u0443 u043b u00a0其中和maxi的值第一个 u043f u043e u0440 u00a0 u0434 u043a u0430平方的最小角度范围 u043c u043e u0434 u0443 u043b u00a0 u043d u043e u0440 u043c u0438 u0440 u0443 u044e u0442在高功率下并基于归一化和无线电信号的坐标 u0441 u0443 u0434 u00a0 u0442的最大值以及其教区的拐角。在此 u043d u043e u0440 u043c u0438 u0440 u043e u0432 u0430 u043d u043d u044b u0435 u0437 u043d u0430 u0447 u0435 u043d u0438 u00a0最大平方模块 u0441 u0443 u043c u043c u0438 u0440 u0443 u044角度频谱并与第一个阈值进行比较,在此阈值以上没有无线电信号 u043e u043f u0440 u0435 u0434 u0435 u043b u00a0 u044e u0442 dmv u0443 u0442 u0441 u0442 u0432 u0432 u0438 u0435 u043e u043f u0440 u0435 u0434 u0435 u043b u00a0 u044e u044e u0442相关结果 u0432 u044b u0447 u0438 u0442 u0430 u043d u043d u0438 u00a0单位最大平方模块角光谱结果来自基本单位 u0432 u044b u0447 u0438 u0442 u0430 u043d u0438 u00a0 u043d u0438 u00a0第一个 u043f u043e u0440 u00a0 u0434 u043a u0430方形 u043c u043e u0434 u0433 u0433 u043b u00a0的最大角度范围,并与第二个阈值进行比较,第二个阈值超过了第二个阈值,否则两个无线电信号具有第二个 u043f u043e u0440 u00a0 u0434 u043a u0430 u0432 u044b u043f u043e u043b u043d u00a0 u044e u0442公式;哪里是 u043d u043e u0440 u043c u0438 u0440 u0440 u043e u0432 u0430 u043d u043d u0430 u00a0辐射方向图天线棒的方向为首次最大角度范围的方向 u043c u043e u0434 u0443 u043b u00a0正方形 u00a0 u0434 u043a u0430和 u0437 u043d u0430 u0447 u0435 u043d u0438 u00a0通过neumann准则设置的阈值, u0438 u0441 u0445 u043e u0434 u00a0 u0432 u0435 u0440 u043e u00a0 u0442 u043d u043d u043e错误的u0441 u0442 u0438警报,数量为 u0440 u0430 u0441 u043f u043e u043b u043e u0436 u0435 u043d u0438 u00a0天线,即波 u0438 u0437 u043b u0443 u0447 u0435 u043d u043d u0438 u00a0和指定的错误 u043f u0435 u043b u0435 u043d u0433 u043e u0432 u0430 u043d u0438 u00a0。

相似文献

  • 专利
  • 外文文献
  • 中文文献
获取专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号