Dynamic error modeling of silicon micromechanical gyroscope and system simulation

Jian Li Li; Min Du; Fan Hong Chen

Dynamic error modeling of silicon micromechanical gyroscope and system simulation

Jian Li Li^*
, Min Du
, Fan Hong Chen

^*此作品的通讯作者

仪器科学与光电工程学院

Institute of Disaster Prevention Science and Technology
Beijing University of Chemical Technology

科研成果: 期刊稿件 › 文章 › 同行评审

1 引用（Scopus）

摘要

In order to improve the anti-jamming ability and precision of MEMS gyroscope, the physical causes of error were analyzed. The dynamic error mathematical model was constructed using the dynamic theory and analytic method. The dynamic error of micro strap-down inertial navigation system was obtained through the test of calibration and compensation. The feasibility of project which the system used to anti-tank missile was verified through system simulation method.

源语言	英语
页（从-至）	567-569
页数	3
期刊	Xitong Fangzhen Xuebao / Journal of System Simulation
卷	20
期	3
出版状态	已出版 - 5 2月 2008

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引用此

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title = "Dynamic error modeling of silicon micromechanical gyroscope and system simulation",

abstract = "In order to improve the anti-jamming ability and precision of MEMS gyroscope, the physical causes of error were analyzed. The dynamic error mathematical model was constructed using the dynamic theory and analytic method. The dynamic error of micro strap-down inertial navigation system was obtained through the test of calibration and compensation. The feasibility of project which the system used to anti-tank missile was verified through system simulation method.",

keywords = "Dynamic error, Dynamic theory, Micro Electromechanical System (MEMS) gyroscope, Modeling, Simulation",

author = "Li, \{Jian Li\} and Min Du and Chen, \{Fan Hong\}",

year = "2008",

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language = "英语",

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AU - Li, Jian Li

AU - Du, Min

AU - Chen, Fan Hong

PY - 2008/2/5

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N2 - In order to improve the anti-jamming ability and precision of MEMS gyroscope, the physical causes of error were analyzed. The dynamic error mathematical model was constructed using the dynamic theory and analytic method. The dynamic error of micro strap-down inertial navigation system was obtained through the test of calibration and compensation. The feasibility of project which the system used to anti-tank missile was verified through system simulation method.

AB - In order to improve the anti-jamming ability and precision of MEMS gyroscope, the physical causes of error were analyzed. The dynamic error mathematical model was constructed using the dynamic theory and analytic method. The dynamic error of micro strap-down inertial navigation system was obtained through the test of calibration and compensation. The feasibility of project which the system used to anti-tank missile was verified through system simulation method.

KW - Dynamic error

KW - Dynamic theory

KW - Micro Electromechanical System (MEMS) gyroscope

KW - Modeling

KW - Simulation

UR - https://www.scopus.com/pages/publications/40049092319

M3 - 文章

AN - SCOPUS:40049092319

SN - 1004-731X

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SP - 567

EP - 569

JO - Xitong Fangzhen Xuebao / Journal of System Simulation

JF - Xitong Fangzhen Xuebao / Journal of System Simulation

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ER -

Dynamic error modeling of silicon micromechanical gyroscope and system simulation

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