Analysis of error for a rotating strap-down inertial navigation system with fibro gyro

Yue yang Ben; Yong li Chai; Wei Gao; Feng Sun

doi:10.1007/s11804-010-1028-z

Analysis of error for a rotating strap-down inertial navigation system with fibro gyro

Yue yang Ben
, Yong li Chai^*
, Wei Gao
, Feng Sun

^*Corresponding author for this work

Harbin Engineering University

Research output: Contribution to journal › Article › peer-review

32 Scopus citations

Abstract

The error equation of a rotating inertial navigation system was introduced. The effect of the system's main error source (constant drift of gyro and zero bias of accelerometer) under rotating conditions for the system was analyzed. Validity of theoretical analysis was shown via simulation, and that provides a theoretical foundation for a rotating strap-down inertial navigation system during actual experimentation and application.

Original language	English
Pages (from-to)	419-424
Number of pages	6
Journal	Journal of Marine Science and Application
Volume	9
Issue number	4
DOIs	https://doi.org/10.1007/s11804-010-1028-z
State	Published - Dec 2010
Externally published	Yes

Keywords

error analysis
fibro gyro
rotating strap-down inertial navigation

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10.1007/s11804-010-1028-z

Cite this

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title = "Analysis of error for a rotating strap-down inertial navigation system with fibro gyro",

abstract = "The error equation of a rotating inertial navigation system was introduced. The effect of the system's main error source (constant drift of gyro and zero bias of accelerometer) under rotating conditions for the system was analyzed. Validity of theoretical analysis was shown via simulation, and that provides a theoretical foundation for a rotating strap-down inertial navigation system during actual experimentation and application.",

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doi = "10.1007/s11804-010-1028-z",

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AU - Ben, Yue yang

AU - Chai, Yong li

AU - Gao, Wei

AU - Sun, Feng

PY - 2010/12

Y1 - 2010/12

N2 - The error equation of a rotating inertial navigation system was introduced. The effect of the system's main error source (constant drift of gyro and zero bias of accelerometer) under rotating conditions for the system was analyzed. Validity of theoretical analysis was shown via simulation, and that provides a theoretical foundation for a rotating strap-down inertial navigation system during actual experimentation and application.

AB - The error equation of a rotating inertial navigation system was introduced. The effect of the system's main error source (constant drift of gyro and zero bias of accelerometer) under rotating conditions for the system was analyzed. Validity of theoretical analysis was shown via simulation, and that provides a theoretical foundation for a rotating strap-down inertial navigation system during actual experimentation and application.

KW - error analysis

KW - fibro gyro

KW - rotating strap-down inertial navigation

UR - https://www.scopus.com/pages/publications/78649689047

U2 - 10.1007/s11804-010-1028-z

DO - 10.1007/s11804-010-1028-z

M3 - 文章

AN - SCOPUS:78649689047

SN - 1671-9433

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EP - 424

JO - Journal of Marine Science and Application

JF - Journal of Marine Science and Application

IS - 4

ER -

Analysis of error for a rotating strap-down inertial navigation system with fibro gyro

Abstract

Keywords

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