Xu Xiangming, Xiao Dingbang, Li Wenyin, Xu Qiang, Hou Zhanqiang, Wu Xuezhong
College of Mechatronics Engineering and Automation, National University of Defense Technology, Changsha 410073, China.
Sensors (Basel). 2017 Dec 11;17(12):2870. doi: 10.3390/s17122870.
This paper reports a dual-butterfly structure gyroscope based on the traditional butterfly structure. This novel structure is composed of two butterfly structures, each of which contains a main vibrational beam, four proof masses, and a coupling mechanism. The coupling mechanism in this proposed structure couples the two single butterfly structures and keeps the driving mode phases of the two single butterfly gyroscopes exactly opposite, increasing the double difference of traditional butterfly gyroscopes to a quad difference, which has the potential advantage of improving bias instability and g-sensitivity. The gyroscope was fabricated using a standard microfabrication method and tested in laboratory conditions. The experimental results show a Q-factor of 10,967 in driving mode and there were two peaks in the frequency responses curve of sensing direction due to unavoidable fabrication errors. Scale factor and bias instability were also measured, reaching a scale factor of 10.9 mV/°/s and a bias instability of 10.7°/h, according to the Allan Variance curve.
本文报道了一种基于传统蝶形结构的双蝶形结构陀螺仪。这种新颖的结构由两个蝶形结构组成,每个蝶形结构包含一个主振动梁、四个检测质量块和一个耦合机构。该结构中的耦合机构将两个单蝶形结构耦合在一起,并使两个单蝶形陀螺仪的驱动模式相位恰好相反,将传统蝶形陀螺仪的双差提高到四差,这具有提高偏置不稳定性和重力灵敏度的潜在优势。该陀螺仪采用标准微加工方法制造,并在实验室条件下进行测试。实验结果表明,驱动模式下的品质因数为10967,由于不可避免的制造误差,传感方向的频率响应曲线中有两个峰值。还测量了比例因子和偏置不稳定性,根据阿伦方差曲线,比例因子达到10.9 mV/°/s,偏置不稳定性达到10.7°/h。