MECHANISM ANALYSIS AND SYSTEM IDENTIFICATION OF THE QUADRATURE ERROR IN MEMS GYROSCOPE
This paper discusses error mechanism and experimental system identification of the quadrature error present in Tsinghua University MEMS vibratory rate gyroscopes. The magnitude and stability of the quadrature error are both of concern because they corrupt the measurement of the actual input rate. The stiffness matrix of suspension beams and a three-mode dynamics model of gyroscope structure are developed and the analysis demonstrates that structure imperfections result in the quadrature error, which is generally considerably larger than Coriolis-induced rate signal. The gyroscope dynamics and structure parameters are identified by modal experiment and frequency responsefunction matrix. The experiment results from twenty gyroscope samples demonstrate that structure imperfections are main reasons resulting in the quadrature bias of the gyroscope, including anis-elasticity of suspension beams, and stiffness coupling between drive axis and sense axis. The identified structure parameters will also contribute to future laser trimming for reducing the quadrature error of gyroscope.
micromachined gyroscope quadrature error structure imperfections system identification
Jun Yang ZhongYu Gao Rong Zhang ZhiYong Chen Bin Zhou
Department of Precision Instruments and Mechanology, Tsinghua University, Beijing 10084, China
国际会议
海南三亚
英文
2007-01-10(万方平台首次上网日期,不代表论文的发表时间)