and , which is input to the PAA beam control unit and calculated at the selected bank angle Ψj, and arbitrary angle of deviation of beam from normal θoi from the entire possible range of the beam deviation for the particular PAA by formulas , which makes it possible, by azimuth scanning ASRD from central angle (-θoi), at the same time to measure horizontal cross-sections of both difference RPs, where their measured angular coordinates of minima coincide on all angles of deviation of the beam from the normal θoi, after which all measurements are repeated at other selected CAR angle angles, and after installation of fairing and corresponding measurements by the same as before its installation, roll angles and angles of deviation of beam from normal, according to changed angular coordinates of minima in cross-sections of difference RP of PAA-fairing system corresponding components of direction-finding error in coordinates αx and αy, applied by fairing at corners Ψj, θoi installation of the PAA-fairing system can be calculated using the formulas:; ,;where: is component of direction-finding error introduced by fairing by angle αx when installing the PAA beam by coordinates θ=θoi; Ψ=Ψj, – component of direction-finding error introduced by fairing, by angle αy during PAA beam setting by coordinates θ=θoi, Ψ=Ψj, θoi – one of arbitrarily set current values of spatial angle between the direction of the PAA beam installation and the normal to its opening, on which, before the fairing installation, the measured minima of the horizontal sections of the difference diagrams coincide, Ψj – current preset value of the PAA bank angle relative to the horizontal plane of the azimuth scanning of the antenna support-rotary device, θai – measured, after installation of fairing, actual angle of minimum horizontal cross-section of difference azimuth diagram during installation of PAA beam by coordinates θ=θoi; Ψ=Ψj, θyi – measured, after installation of fairing, actual angle of minimum horizontal cross-section of difference elevation diagram during installation of PAA beam by coordinates θ=θoi; Ψ=Ψj.;EFFECT: disclosed is a method of measuring direction-finding errors of a radar antenna dome system.;1 cl, 4 dwg"/> METHOD OF MEASURING DIRECTION-FINDING ERRORS OF A RADAR ANTENNA DOME SYSTEM
首页> 外国专利> METHOD OF MEASURING DIRECTION-FINDING ERRORS OF A RADAR ANTENNA DOME SYSTEM

METHOD OF MEASURING DIRECTION-FINDING ERRORS OF A RADAR ANTENNA DOME SYSTEM

机译:雷达天线罩系统定向误差的测量方法

摘要

FIELD: radar ranging and radio navigation.;SUBSTANCE: invention relates to radar engineering. Method is based on measurement of the angular displacement of the spatial position of the minimum formed by the difference RP of the antenna at given angles of its rotation in azimuth and roll and determination of direction-finding errors depending on these angles. Before installation of fairing azimuth plane of scanning of antenna support-rotary device (ASRD) with roll installed on it at angle Ψj phased antenna array, is adjusted in such a way that the azimuthal plane of scanning of the antenna support-rotary device coincides with the horizontal plane, after which the phased antenna array beam is set according to the coordinates and , which is input to the PAA beam control unit and calculated at the selected bank angle Ψj, and arbitrary angle of deviation of beam from normal θoi from the entire possible range of the beam deviation for the particular PAA by formulas , which makes it possible, by azimuth scanning ASRD from central angle (-θoi), at the same time to measure horizontal cross-sections of both difference RPs, where their measured angular coordinates of minima coincide on all angles of deviation of the beam from the normal θoi, after which all measurements are repeated at other selected CAR angle angles, and after installation of fairing and corresponding measurements by the same as before its installation, roll angles and angles of deviation of beam from normal, according to changed angular coordinates of minima in cross-sections of difference RP of PAA-fairing system corresponding components of direction-finding error in coordinates αx and αy, applied by fairing at corners Ψj, θoi installation of the PAA-fairing system can be calculated using the formulas:; ,;where: is component of direction-finding error introduced by fairing by angle αx when installing the PAA beam by coordinates θ=θoi; Ψ=Ψj, – component of direction-finding error introduced by fairing, by angle αy during PAA beam setting by coordinates θ=θoi, Ψ=Ψj, θoi – one of arbitrarily set current values of spatial angle between the direction of the PAA beam installation and the normal to its opening, on which, before the fairing installation, the measured minima of the horizontal sections of the difference diagrams coincide, Ψj – current preset value of the PAA bank angle relative to the horizontal plane of the azimuth scanning of the antenna support-rotary device, θai – measured, after installation of fairing, actual angle of minimum horizontal cross-section of difference azimuth diagram during installation of PAA beam by coordinates θ=θoi; Ψ=Ψj, θyi – measured, after installation of fairing, actual angle of minimum horizontal cross-section of difference elevation diagram during installation of PAA beam by coordinates θ=θoi; Ψ=Ψj.;EFFECT: disclosed is a method of measuring direction-finding errors of a radar antenna dome system.;1 cl, 4 dwg
机译:雷达测距和无线电导航技术领域本发明涉及雷达工程。该方法基于天线在给定的方位角和侧倾旋转角度下天线的差RP所形成的最小值的空间位置的角位移的测量,并基于这些角度确定方向误差。在安装天线支撑旋转设备(ASRD)的整流罩扫描方位角平面之前,应将其以roll j 相控天线阵的角度安装在其上,以使天线支撑旋转装置与水平面重合,然后根据坐标设置相控天线阵列波束。和<图像文件=“ 00000033.JPG” he =“ 5” imgContent =“ undefined” imgFormat =“ JPEG” wi =“ 8” />,将其输入到PAA光束控制单元并进行计算在选定的倾斜角Ψ j 处,并且通过公式,这可以通过从中心角(-θ oi < / sub>),在同一ti可以测量两个不同RP的水平横截面,其中它们测量的最小值角坐标在光束与法线θ oi 的所有偏离角度上均重合,然后在其他选定位置重复所有测量根据PAA整流罩系统差RP的横截面中最小值的变化角度坐标,根据安装后整流罩的CAR角和安装整流罩后的相应测量以及与安装前相同的相应测量,滚动角度和光束偏离法线的角度通过在角 j ,θ oi <处的光洁度应用的坐标α x 和α y 中的测向误差的相应分量/ Sub> PAA整流系统的安装可以使用以下公式计算: ,;其中:是在通过坐标θ=θ oi 安装PAA光束时,由于角度αx的整流而引入的测向误差分量; Ψ=Ψ j ,<图像文件=“ 00000037.JPG” he =“ 6” imgContent =“ undefined” imgFormat =“ JPEG” wi =“ 11” /> –定位错误的组成部分在PAA光束设置过程中,通过整流罩,角度αy通过坐标θ=θ oi ,Ψ=Ψ j ,θ oi 引入–任意之一设置PAA梁安装方向与其开口法线之间的空间角度的当前值,在整流罩安装之前,差示图的水平截面的测得最小值重合为, j –相对于天线支撑旋转设备方位扫描水平面的PAA倾斜角的当前预设值θ ai –在安装整流罩后,测量最小水平交叉点的实际角度用坐标θ=θ oi 的PAA梁安装过程中的差方位角图剖面; Ψ=Ψ j ,θ yi –在安装整流罩后,通过坐标θ=测得的PAA梁安装过程中差高程图的最小水平横截面的实际角度的测量值θ oi ; FF =Ψ j 。;效果:公开了一种测量雷达天线穹顶系统的测向误差的方法。; 1 cl,4 dwg

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