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AIRPLANE LANDING METHOD USING A SATELLITE NAVIGATION SYSTEM AND A LANDING SYSTEM BASED THEREON

机译:利用卫星导航系统的飞机着陆方法及基于该方法的着陆系统

摘要

The invention can be used for aeroplane navigation. Said invention makes it possible to increase the accuracy and reliability of the determination of aeroplane coordinates. The inventive aeroplane landing method consists in determining differential corrections of pseudoranges measured on board the airplane with respect to satellites, in additionally taking into account the errors induced by the mirror reflection of signals transmitted by satellites, in pre-drawing, on a local monitoring and correcting station, the volume distribution diagram of a predictable ground-borne multipath propagation error variance, in inputting said diagram into a ground-borne database, in continuously comparing the predictable ground-borne multipath propagation error variance and the actual measured ground-borne multipath propagation error variance by selecting a maximum value therefrom, in determining the root mean square value of the ground-borne pseudorange multipath propagation error and in transmitting it to the aeroplane, wherein said method also consists in pre-drawing the diagram of the volume distribution of the airborne multipath propagation error variance, in continuously, by means of the airborne database, determining the airborne multipath propagation error variance taking into account the angular orientation of the aeroplane in relation to the current position of each satellite, in simultaneously calculating the airborne multipath propagation pseudorange error using the predictable airborne multipath propagation error as the current airborne multipath propagation error, in determining the total pseudorange error variance as the sum of the ground-borne and airborne pseudorange multipath propagation error variances for each satellite and in using the common pseudorange variances of all the satellites for calculating the refined coordinates of the aeroplane and for increasing the determination reliability therefor. A system forcarrying out said method is also disclosed.
机译:本发明可以用于飞机导航。所述发明使得可以提高确定飞机坐标的准确性和可靠性。本发明的飞机着陆方法在于,在预绘制时,在本地监测和预测中,另外考虑由卫星发射的信号的镜面反射引起的误差,从而确定在飞机上相对于卫星测量的伪距的差分校正。校正站,将可预测的地面多径传播误差方差的体积分布图输入到地面数据库中,连续比较可预测的地面多径传播误差方差和实际测得的地面多径传播误差通过从中选择一个最大值,确定地面伪距多径传播误差的均方根值并将其传输到飞机上来确定误差方差,其中,所述方法还包括预先绘制该误差方差的体积分布图机载多径传播误差方差,连续因此,借助机载数据库,在使用可预测的机载多径传播同时计算机载多径传播伪距误差的同时,考虑飞机相对于每个卫星当前位置的角向,确定机载多径传播误差方差误差作为当前的机载多径传播误差,确定总伪距误差方差为每个卫星的地面和机载伪距多径传播误差方差之和,并使用所有卫星的公共伪距方差来计算精确坐标为了提高确定的可靠性。还公开了用于执行所述方法的系统。

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