Development of a vibrational error model of a hemispherical resonator gyroscope

2018 25th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS) Pub Date : 2018-05-01 DOI:10.23919/icins.2018.8405894

R. Ermakov, E. N. Skripal, D. Kondratov, A. L’vov, A. Seranova, D. E. Gutsevich

引用次数: 4

Abstract

A mathematical model of vibration error for a hemispherical resonator gyroscope is considered. The expression for the resonator standing wave precession coefficient under the conditions of base vibration is obtained.

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半球形谐振陀螺仪振动误差模型的建立

建立了半球形谐振陀螺仪振动误差的数学模型。得到了基振条件下谐振腔驻波进动系数的表达式。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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来源期刊

2018 25th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS)

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