发明名称 INTEGRITY OF DIFFERENTIAL GPS CORRECTIONS IN NAVIGATION DEVICES USING MILITARY TYPE GPS RECEIVERS
摘要 A method and apparatus for calculating corrections to a navigation solution based on differential GPS data includes receiving GPS ephemeris from at least three GPS satellites. A PVT solution is resolved from the GPS ephemeris. The PVT solution includes a Circular Error Probable (CEP). Differential GPS data for calculating the corrections to the PVT solution is received. A corrected PVT solution is then based upon the differential GPS data. The corrected PVT solution is compared to an area defined by the CEP. Where the corrected PVT solution is not within the area, the corrected PVT solution is rejected in favor of the PVT solution for determining an accurate navigational solution.
申请公布号 US2009322598(A1) 申请公布日期 2009.12.31
申请号 US20080147410 申请日期 2008.06.26
申请人 HONEYWELL INTERNATIONAL, INC. 发明人 FLY BRIAN E.;MORGAN KENNETH S.;WAID JAMES D.;IGNAC MARTIN P.
分类号 G01S5/14 主分类号 G01S5/14
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