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Motion equations of hemispherical resonator and analysis of frequency split caused by slight mass non-uniformity
作者姓名:Yan HUO  Shunqing REN  Guoxing YI  Changhong WANG
作者单位:Space Control and Inertial Technology Research Centre,Harbin Institute of Technology
摘    要:The mass non-uniformity of hemispherical resonator is one of reasons for frequency split, and frequency split can cause gyroscope to drift. Therefore, it is of great significance to analyze the relationship between mass non-uniformity and frequency split, which can provide a theoretical basis for mass balance of imperfect resonator. The starting point of error mechanism analysis for gyroscope is the motion equations of resonator. Firstly, based on the Kirchhoff-Love hypothesis in the elastic thi...

收稿时间:28 May 2019

Motion equations of hemispherical resonator and analysis of frequency split caused by slight mass non-uniformity
Yan HUO,Shunqing REN,Guoxing YI,Changhong WANG.Motion equations of hemispherical resonator and analysis of frequency split caused by slight mass non-uniformity[J].Chinese Journal of Aeronautics,2020,33(10):2660-2669.
Institution:Space Control and Inertial Technology Research Centre, Harbin Institute of Technology, Harbin 150080, China
Abstract:The mass non-uniformity of hemispherical resonator is one of reasons for frequency split, and frequency split can cause gyroscope to drift. Therefore, it is of great significance to analyze the relationship between mass non-uniformity and frequency split, which can provide a theoretical basis for mass balance of imperfect resonator. The starting point of error mechanism analysis for gyroscope is the motion equations of resonator. Firstly, based on the Kirchhoff-Love hypothesis in the elastic thin shell theory, the geometric deformation equations of resonator are deduced. Secondly, the deformation energy equation of resonator is derived according to the vibration mode and relationship between the stress and strain of hemispherical thin shell. Thirdly, the kinetic energy equation of resonator is deduced by the Coriolis theorem. Finally, the motion equations of resonator are established by the Lagrange mechanics principle. The theoretical values of precession factor and natural frequency are calculated by the motion equations, which are substantially consistent with the ones by the finite element method and practical measurement, the errors are within a reasonable range. Simultaneously, the varying trend of natural frequency with respect to the geometrical and physical parameters of resonator by the motion equations is consistent with that by the finite element analysis. The above conclusions prove the correctness and rationality of motion equations. Similarly, the motion equations of resonator with mass non-uniformity are established by the same modeling method in case of ignoring the input angular rate and damping, and the state equations with respect to the velocity and displacement of vibration system are derived, then two natural frequencies are solved by the characteristic equation. It is concluded that one of reasons for frequency split is the 4th harmonic of mass non-uniformity, and thus much attention should be paid to minimizing the 4th harmonic of mass non-uniformity in the course of mass balancing for imperfect resonator.
Keywords:Hemispherical resonator  Lagrange mechanics principle  Theory of elastic thin shell  Motion equations  Mass non-uniformity  Frequency split
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