Estimating Conservative Error Bounds for INS Output Error

被引:0
|
作者
Gebre-Egziabher, Demoz [1 ]
机构
[1] Univ Minnesota, Dept Aerosp Engn & Mech, Minneapolis, MN 55455 USA
来源
PROCEEDINGS OF THE 27TH INTERNATIONAL TECHNICAL MEETING OF THE SATELLITE DIVISION OF THE INSTITUTE OF NAVIGATION (ION GNSS 2014) | 2014年
关键词
D O I
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中图分类号
TP7 [遥感技术];
学科分类号
081102 ; 0816 ; 081602 ; 083002 ; 1404 ;
摘要
This paper examines the problem of estimating conservative error bounds of inertial navigation systems when they are used as part of an integrated navigation system designed around a low cost inertial measurement unit (automotive/commerical grade). This is done by recasting the inertial navigation error equations for low cost sensors in a form which allows proving that the time update equations can be statistically overbounded. The resulting overbounds, however, are shown to be overly conservative.
引用
收藏
页码:2062 / 2068
页数:7
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