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Method and device for optimising the accuracy of the positioning and/or reduction of the integrity risk of a receiver in a global satellite navigation system

机译:用于优化全球卫星导航系统中的接收机的定位精度和/或降低其完整性风险的方法和设备

摘要

The method involves determining a deviation error for satellites (RF1-RF4), where the error is dependent on a system parameter, and geometrical adjustment of the satellites relative to a receiver (E). The error is determined from another deviation error by error projection in a coordinate system of the receiver. A value of the parameter is determined by a preset parameter value, and another value is determined by a modified parameter value. The modified parameter value is modified with respect to the preset value such that a small error of the modified value is accepted as true. An independent claim is also included for a device for optimizing accuracy of position determination and/or for reducing integrity risk of a receiver in a global satellite navigation system.
机译:该方法包括确定卫星的偏差误差(RF1-RF4),其中误差取决于系统参数,以及卫星相对于接收机的几何调整(E)。通过在接收器的坐标系中的误差投影从另一个偏差误差确定该误差。该参数的值由预设参数值确定,而另一个值由修改后的参数值确定。相对于预设值修改修改后的参数值,使得修改值的小误差被接受为是。还包括针对在全球卫星导航系统中用于优化位置确定的准确性和/或用于降低接收机的完整性风险的设备的独立权利要求。

著录项

  • 公开/公告号EP2154544B1

    专利类型

  • 公开/公告日2017-06-21

    原文格式PDF

  • 申请/专利权人 AIRBUS DS GMBH;

    申请/专利号EP20090010025

  • 发明设计人 DAUBRAWA JULIAN;VON KRÜGER JAN M.W. DR.;

    申请日2009-08-04

  • 分类号G01S19/08;G01S19/20;G01S19/42;

  • 国家 EP

  • 入库时间 2022-08-21 14:06:58

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