Autonomous fault detection and removal using GPS carrier phase

被引：33

作者：

Pervan, BS ^{[1
]}

Lawrence, DG ^{[1
]}

Parkinson, BW ^{[1
]}

机构：

[1] Stanford Univ, Dept Aeronaut & Astronaut, Stanford, CA 94305 USA

来源：

IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS | 1998年 / 34卷 / 03期

基金：

美国国家航空航天局;

关键词：

This work was supported by the Federal Aviation Administration and the National Aeronautics and Space Administration;

D O I：

10.1109/7.705896

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

This paper is focused on the use of carrier phase measurements and parity space methodology to investigate the limits of high-integrity and high-continuity satellite-based navigation performance. In this regard, a new algorithm for receiver autonomous fault detection and removal is developed with the specific goal of attaining the high levels of integrity and continuity required for aircraft precision approach and landing applications. Fault detection and removal algorithm performance is demonstrated through analysis and simulation, and the results of tests using deliberately induced failures in raw night data are presented.

引用

页码：897 / 906

页数：10

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