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METHOD OF CALIBRATING RADAR STATION BASED ON RADAR CROSS-SECTION VALUE ON MINISATELLITE WITH REFERENCE REFLECTOR

机译:基于带有参考反射器的微型卫星上雷达截面值的雷达站标定方法

摘要

FIELD: radio engineering, communication.;SUBSTANCE: method includes launching a reflector with a known radar cross-section to the orbit of an artificial earth satellite, irradiating said reflector with radar signals, receiving and measuring amplitude of reflected signals, wherein an angle reflector is transported on-board a minisatellite as a radar cross-section reference to an orbit around the Earth, said angle reflector being made in form of two flat radar-reflecting pivotally connected faces, turned by a fixed angle α which ranges from (90-Δ)° to (90+Δ)°, where Δ is defined from the relationship: 0Δ18λ/a, λ is the wavelength of the calibrated radar station, a is the size of the face angle reflector. Before launching, the angle reflector is placed on the outer side of the end surface of the housing of the minisatellite. The middle of the edge of the angle reflector is arranged coaxial to the centre of the end surface, wherein the faces are oriented such that the bisector of the angle between the faces of the angle reflector in the plane perpendicular to the middle of the edge is aligned with the longitudinal axis of the minisatellite. During flight, GLONASS and/or GPS receivers and an on-board computer are used to determine the position of the centre of mass of the minisatellite relative to the position of the calibrated radar station, the spatial position of the longitudinal axis of the minisatellite relative to the line of sight of the radar station, and a minisatellite orientation system then performs alignment thereof so that the main lobe of the scattering pattern of the angle reflector is directed towards the calibrated radar station, and the maximum of the main lobe of the scattering pattern of the angle reflector coincides with the line of sight of the calibrated radar station. The angle reflector then turns about the bisector of the angle between its faces.;EFFECT: high accuracy of calibrating radar stations.;11 cl, 16 dwg
机译:领域:方法:方法包括向人造地球卫星的轨道发射具有已知雷达横截面的反射器,向其反射雷达信号,接收并测量反射信号的幅度,其中角度反射器雷达是通过微型卫星作为雷达截面运输到地球周围的轨道的,该角反射器由两个平面的,可反射雷达的枢轴连接面构成,并旋转固定角度α,其范围为(90- Δ)°至(90 +Δ)°,其中Δ由以下关系定义:0 <Δ<18λ/ a,λ是校准雷达站的波长,a是面角反射器的尺寸。在发射之前,将角度反射器放置在小卫星外壳端面的外侧。角反射器的边缘的中部与端面的中心同轴地布置,其中,所述面的取向使得在垂直于边缘的中部的平面中,角反射器的面之间的角的平分线为。与小卫星的纵轴对齐。在飞行过程中,使用GLONASS和/或GPS接收器以及机载计算机确定微型卫星质心相对于校准雷达站位置的位置,微型卫星纵轴相对位置的空间位置对准雷达站的视线,然后由微型卫星定向系统进行对准,以使角度反射器的散射图样的主瓣指向校准后的雷达站,并且最大散射主瓣指向角度反射镜的图案与校准雷达站的视线重合。角度反射器然后绕其两面之间的角度的等分线转动。效果:校准雷达站的精度很高; 11 cl,16 dwg

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