Vibration Sensitivity of MEMS Tuning Fork Gyroscopes

MEMS tuning fork gyroscopes (TFGs) are known to be relatively immune to vibrations due to their differential operation and common-mode rejection. However, even a perfectly-matched TFG cannot completely eliminate vibrations due to vibration-induced asymmetry and nonlinearity. We select two commonly used gyroscope structures and analyze their vibration characteristics. Both structures employ decoupled sense and drive masses with "Type-A" having an anchored sense mass and "Type-B" having an anchored drive mass. To understand the effects of vibration on these two structures, we performed nonlinear dynamic simulations using MATLAB and SIMULINK. The results show that Type-B structures are insensitive to vibrations (>99% reduction) when compared to Type-A structures. In addition, the simulations reveal the dominant vibration characteristics for each structure.

[1]  F. Ayazi,et al.  High Performance Matched-Mode Tuning Fork Gyroscope , 2006, 19th IEEE International Conference on Micro Electro Mechanical Systems.

[2]  T. Braman,et al.  Designing Vibration and Shock Isolation Systems for Micro Electrical Machined Based Inertial Measurement Units , 2006, 2006 IEEE/ION Position, Location, And Navigation Symposium.

[3]  S. Sherman,et al.  Single-chip surface micromachined integrated gyroscope with 50°/h Allan deviation , 2002, IEEE J. Solid State Circuits.

[4]  M. Palaniapan,et al.  Modal Coupling in Micromechanical Vibratory Rate Gyroscopes , 2006, IEEE Sensors Journal.

[5]  G.A. Geen Progress in integrated gyroscopes , 2004, IEEE Aerospace and Electronic Systems Magazine.

[6]  Seonho Seok,et al.  A study on resonant frequency and Q factor tunings for MEMS vibratory gyroscopes , 2004 .

[7]  R. Ritchie,et al.  High-cycle fatigue of single-crystal silicon thin films , 2001 .