Xia Dunzhu, Xu Lei
Key Laboratory of Micro-Inertial Instrument and Advanced Navigation Technology, Ministry of Education, School of Instrument Science and Engineering, Southeast University, Nanjing 210096, China.
Micromachines (Basel). 2017 Oct 16;8(10):310. doi: 10.3390/mi8100310.
A novel fully decoupled micro inertial measurement unit (MIMU) is presented in this paper. The proposed MIMU structure, mostly focusing on the gyroscope unit, is highly symmetrical and can be limited to an area of 10,000 μm × 10,000 μm. Both the tri-axis gyroscope and tri-axis accelerometer structures are fabricated on the same single silicon chip, which can differentially detect three axes' angular velocities and linear accelerated velocities at the same time. By elaborately arranging different decoupling beams, anchors and sensing frames, the drive and sense modes of the tri-axis gyroscope are fully decoupled from each other. Several dynamic models, including decoupling beams with fabrication imperfections, are established for theoretical analysis. The numerical simulation made by MATLAB shows the structural decoupling of three sense modes, and indicates that the key decoupling beams, which affect the quadrature error, can be improved in design. The whole fabrication process, including silicon on glass (SOG) process, dry/wet etching as well as the methods for improving the fabrication quality, is then shown. Experiments for mode frequency and quality factors of four modes (drive, yaw, pitch and roll) have been performed, and are found to be 455 (6950.2 Hz), 66 (7054.4 Hz), 109 (7034.2 Hz) and 107 (7040.5 Hz) respectively. The analysis and experiment both prove that this novel MIMU has the potential value of further intensive investigation.
本文提出了一种新型的完全解耦微惯性测量单元(MIMU)。所提出的MIMU结构主要聚焦于陀螺仪单元,具有高度对称性,面积可限制在10000μm×10000μm。三轴陀螺仪和三轴加速度计结构都制作在同一单晶硅芯片上,能够同时差分检测三个轴的角速度和线性加速度。通过精心布置不同的解耦梁、锚点和传感框架,三轴陀螺仪的驱动模式和传感模式实现了完全解耦。建立了包括具有制造缺陷的解耦梁在内的几种动力学模型进行理论分析。MATLAB进行的数值模拟展示了三种传感模式的结构解耦,并表明影响正交误差的关键解耦梁在设计上可以改进。随后展示了整个制造过程,包括玻璃上硅(SOG)工艺、干法/湿法蚀刻以及提高制造质量的方法。已经对四种模式(驱动、偏航、俯仰和滚动)的模式频率和品质因数进行了实验,发现分别为455(6950.2Hz)、66(7054.4Hz)、109(7034.2Hz)和107(7040.5Hz)。分析和实验均证明这种新型MIMU具有进一步深入研究的潜在价值。