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Development of a Prototype Miniature Silicon Microgyroscope

机译:原型微型硅微陀螺仪的开发

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摘要

A miniature vacuum-packaged silicon microgyroscope (SMG) with symmetrical and decoupled structure was designed to prevent unintended coupling between drive and sense modes. To ensure high resonant stability and strong disturbance resisting capacity, a self-oscillating closed-loop circuit including an automatic gain control (AGC) loop based on electrostatic force feedback is adopted in drive mode, while, dual-channel decomposition and reconstruction closed loops are applied in sense mode. Moreover, the temperature effect on its zero bias was characterized experimentally and a practical compensation method is given. The testing results demonstrate that the useful signal and quadrature signal will not interact with each other because their phases are decoupled. Under a scale factor condition of 9.6 mV/°/s, in full measurement range of ± 300 deg/s, the zero bias stability reaches 15°/h with worse-case nonlinearity of 400 ppm, and the temperature variation trend of the SMG bias is thus largely eliminated, so that the maximum bias value is reduced to one tenth of the original after compensation from -40 °C to 80 °C.
机译:设计了具有对称和解耦结构的微型真空封装硅微型陀螺仪(SMG),以防止驱动模式和感测模式之间意外耦合。为了确保较高的谐振稳定性和强大的抗干扰能力,在驱动模式下采用了包括基于静电力反馈的自动增益控制(AGC)环路的自激振荡闭环电路,而双通道分解和重构闭环则采用在感应模式下应用。此外,还对温度对其零偏压的影响进行了实验表征,并给出了一种实用的补偿方法。测试结果表明,有用信号和正交信号不会相互影响,因为它们的相位是分离的。在比例因子条件为9.6 mV / ° / s的情况下,在±300度/ s的整个测量范围内,零偏压稳定性达到15 ° / h,情况下非线性为400 ppm,从而大大消除了SMG偏置的温度变化趋势,从而使最大偏置值从-40 ° C补偿到80后降低到原始值的十分之一° C。

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