发明名称 Integrity method for differential corrections
摘要 The invention includes a method of calculating corrections to a navigation solution based on accurate data, comprising: receiving GNSS ephemeris, clock models and other navigation information from at least three GNSS satellites; performing pseudo-ranging to the GNSS satellites; resolving a PVT solution from the GNSS ephemeris, clock models and other navigation information and the pseudo range measurements the PVT solution including a statistical measure; receiving differential GNSS data for calculating the corrections to the PVT solution calculating a corrected PVT solution based upon the differential GNSS data; comparing the corrected PVT solution to an region defined by the statistical measure; and rejecting the corrected PVT solution where the corrected PVT solution is not within the region.
申请公布号 EP2418515(A1) 申请公布日期 2012.02.15
申请号 EP20100007560 申请日期 2010.07.21
申请人 ASTRIUM GMBH 发明人 TRAUTENBERG, HANS L., DR.
分类号 G01S19/20;G01S19/41 主分类号 G01S19/20
代理机构 代理人
主权项
地址