Ding Xukai, Li Hongsheng, Ni Yunfang, Sang Pengcheng
School of Instrument Science and Engineering, Southeast University, Nanjing 210096, China.
Sensors (Basel). 2015 Jan 22;15(2):2453-72. doi: 10.3390/s150202453.
This paper presents a study of the frequency response and the scale-factor of a tuning fork micro-gyroscope operating at atmospheric pressure in the presence of an interference sense mode by utilizing the approximate transfer function. The optimal demodulation phase (ODP), which is always ignored in vacuum packaged micro-gyroscopes but quite important in gyroscopes operating at atmospheric pressure, is obtained through the transfer function of the sense mode, including the primary mode and the interference mode. The approximate transfer function of the micro-gyroscope is deduced in consideration of the interference mode and the ODP. Then, the equation describing the scale-factor of the gyroscope is also obtained. The impacts of the interference mode and Q-factor on the frequency response and the scale-factor of the gyroscope are analyzed through numerical simulations. The relationship between the scale-factor and the demodulation phase is also illustrated and gives an effective way to find out the ODP in practice. The simulation results predicted by the transfer functions are in close agreement with the results of the experiments. The analyses and simulations can provide constructive guidance on bandwidth and sensitivity designs of the micro-gyroscopes operating at atmospheric pressure.
本文利用近似传递函数,对在大气压力下存在干涉敏感模式时工作的音叉微陀螺仪的频率响应和比例因子进行了研究。通过包括主模式和干涉模式在内的敏感模式传递函数,获得了在真空封装微陀螺仪中常被忽略但在大气压力下工作的陀螺仪中相当重要的最佳解调相位(ODP)。考虑干涉模式和ODP,推导了微陀螺仪的近似传递函数。然后,还得到了描述陀螺仪比例因子的方程。通过数值模拟分析了干涉模式和品质因数对陀螺仪频率响应和比例因子的影响。还阐述了比例因子与解调相位之间的关系,并给出了在实际中找出ODP的有效方法。传递函数预测的模拟结果与实验结果非常吻合。这些分析和模拟可为大气压力下工作的微陀螺仪的带宽和灵敏度设计提供建设性指导。