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METHOD OF DETERMINING COORDINATES OF AN AIRCRAFT IN A SATELLITE-PSEUDO-SATELLITES MULTI-POSITION SURVEILLANCE SYSTEM

机译:确定卫星-伪卫星-多位置监视系统中飞机坐标的方法

摘要

FIELD: radio equipment.;SUBSTANCE: invention relates to radio engineering and can be used in airspace monitoring systems to determine aircraft coordinates (AC) using AC navigation signals of global navigation satellite system (GNSS) and pseudo-satellite signals (PS) for illumination. In the method of determining coordinates of an aircraft in a satellite-pseudo-satellite multi-position surveillance system comprising N satellites with coordinates xj, yj, zj, j = 1, 2 …, N, M pseudo-satellite with coordinates xj, yj, zj, j = N+1, N+2 …, N+M, and receiver with coordinates xP, yP, zP, in radio visibility zone of which there is an aircraft with the desired coordinates x, y, z, aircraft coordinates are determined based on measurements on scattered signals of distances Rj along propagation path "j-th navigation satellite, pseudosatellite – aircraft –receiver" using direct solution of system of corresponding non-linear equations for calculation of coordinates.;EFFECT: high accuracy of determining coordinates of an aircraft in a satellite-pseudo-satellites multi-position surveillance system.;1 cl, 1 dwg
机译:技术领域:本发明涉及无线电工程,并且可以在空域监视系统中使用全球导航卫星系统(GNSS)的AC导航信号和用于照明的伪卫星信号(PS)来确定飞机坐标(AC)。 。在确定卫星-伪卫星多位置监视系统中的飞机坐标的方法中,该系统包括N个卫星,坐标为x j ,y j ,z j ,j = 1,2…,N,M个伪卫星,坐标为x j ,y j ,z j ,j = N + 1,N + 2…,N + M,并且接收者的坐标为x P ,y P ,z P ,在无线电能见度区域中,有一架具有所需坐标x,y,z的飞机,飞机坐标是根据沿传播路径“第j个导航卫星”的距离R j 的散射信号的测量结果确定的,伪卫星–飞机–接收器”,使用相应非线性方程式系统的直接解来计算坐标。;效果:在卫星-伪卫星多位置监视系统中确定飞机坐标的高精度。1cl 1 dwg

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