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Terrestrial satellite navigation reinforcement system and availability prediction method

机译:地面卫星导航加固系统及可用性预测方法

摘要

In order to improve the availability of a ground type satellite navigation reinforcement system, the present invention is provided with: a worst case ionospheric delay amount difference calculation unit which calculates a worst case ionospheric delay amount difference table for a ground system and an onboard system; a differential correction value calculation unit which creates usable satellite information; a geometric screening unit which guarantees that an error experienced by the onboard system will not exceed a protection level, regardless of which satellite set of positioning satellites is used by the onboard system; an availability prediction unit which creates availability loss information if the protection level when all usable satellites are used exceeds an alert limit; and an eliminated satellite determination unit which eliminates a prescribed number of positioning satellites from the positioning satellites included in the usable satellite information to calculate an eliminated satellite indicator, excludes from the positioning satellites included in the usable satellite information the positioning satellite which was eliminated when the eliminated satellite indicator was minimized, and using the result therefrom as usable satellite update information, causes the geometric screening unit to calculate an integrity parameter.
机译:为了提高地面型卫星导航增强系统的可用性,本发明具有:最坏情况电离层延迟量差计算单元,其计算地面系统和机载系统的最坏情况电离层延迟量差表;以及差分校正值计算单元,其创建可用的卫星信息;几何筛选单元,无论船载系统使用哪种卫星定位卫星,都可确保该船载系统遇到的错误不会超过保护水平;可用性预测单元,如果使用所有可用卫星时的保护级别超过警报限制,则该可用性预测单元将创建可用性损失信息;消除卫星确定单元,从所述可用卫星信息中包括的定位卫星中消除规定数量的定位卫星,以计算消除卫星指示符,从所述可用卫星信息中包括的定位卫星中排除在被消除的卫星指示符被最小化,并且将其结果用作可用的卫星更新信息,使得几何筛选单元计算完整性参数。

著录项

  • 公开/公告号JP6741005B2

    专利类型

  • 公开/公告日2020-08-19

    原文格式PDF

  • 申请/专利权人 日本電気株式会社;

    申请/专利号JP20170526182

  • 发明设计人 鈴木 和史;

    申请日2016-06-29

  • 分类号G01S19/15;G01S19/28;G01S19/07;G01S19/43;G01C21/20;

  • 国家 JP

  • 入库时间 2022-08-21 11:35:11

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