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Temperature Change Leverage on Performance of MEMS Rotational Motion Sensors

机译:温度变化对MEMS旋转运动传感器性能的影响

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This paper presents and analyze results of simulations of two types MEMS vibratory gyroscopes under the influence of temperature changes. This topic has enormous meaning because temperature variation influences on material properties and geometry of device and thus also on its response. Modelling of MEMS device (which includes solid material)and performing simulations in such environment become more complicated. Moreover, because vibratory microgyroscopes are systems of two forced oscillators (for drive and sense directions)with damping, temperature variation influence also on two important quantities characterizes the device: eigenfrequency and Q-factor. Variation of these values under temperature and graphs are presented in paper for different geometries of gyroscopes. Two geometries (structures)are considered here: with one inertial mass only (common for both drive and sense directions)and with central mass and inertial frame. Both geometries were simulated with two different springs configurations. The material used for gyroscope was Polycrystalline Silicon (known also as Polysilicon), with isotropic properties. Mathematical and Finite Element Models in COMSOL, SIMULINK and Coventor MEMS+ are presented as well as results obtained from simulations. These response results (obtained from simulations for one cycle of temperature range 300-400K)show, that MEMS vibrating gyroscopes material and geometrical parameters are sensitive to change of temperature. The main purpose of this paper is to bring up problem of temperature influence on microgyroscope operation. Obviously, this topic is very complex and here some simplifications are assumed. However, results in such simple model clearly indicate the seriousness of the problem and finding additional devise areas influenced by temperature can cause only further performance degradation. The importance of problem of temperature variation influence is particularly seen at the design stage where shape, details of structure, their location are must be taken into consideration. Results presented here show that each detail of structure can meaningfully degrade performance and should be accurately modeled. Unfortunately, imperfections of structure fabricated device cause that precise accuracy of frequency mode-matching cannot be achieved and temperature fluctuations enhance mode-matching inaccuracies.
机译:本文介绍并分析了两种类型的MEMS振动陀螺仪在温度变化影响下的仿真结果。由于温度变化会影响设备的材料性能和几何形状,因此也会影响其响应,因此该主题意义重大。在这样的环境中,MEMS器件(包括固体材料)的建模和执行仿真变得更加复杂。此外,由于振动微陀螺仪是两个带阻尼的强制振荡器(用于驱动方向和传感方向)的系统,因此温度变化对设备的两个重要量的影响也表征了特征频率和Q因子。这些值在温度和曲线下的变化在纸上给出,用于不同几何形状的陀螺仪。这里考虑两种几何形状(结构):仅具有一个惯性质量(对于驱动方向和感测方向而言都是常见的),以及具有中心质量和惯性框架。两种几何形状均使用两种不同的弹簧配置进行了模拟。用于陀螺仪的材料是具有各向同性特性的多晶硅(也称为多晶硅)。介绍了COMSOL,SIMULINK和Coventor MEMS +中的数学和有限元模型,以及从仿真中获得的结果。这些响应结果(从一个温度范围为300-400K的周期的模拟中获得)表明,MEMS振动陀螺仪的材料和几何参数对温度变化敏感。本文的主要目的是提出温度对微陀螺仪操作的影响问题。显然,该主题非常复杂,在此假定了一些简化。但是,这种简单模型的结果清楚地表明了问题的严重性,找到受温度影响的其他设计区域只会导致性能进一步下降。在设计阶段尤其要注意温度变化影响问题的重要性,在设计阶段必须考虑形状,结构细节及其位置。此处显示的结果表明,结构的每个细节都可能会严重降低性能,因此应进行准确建模。不幸的是,结构制造装置的缺陷导致无法实现频率模式匹配的精确精度,并且温度波动会增强模式匹配的不准确性。

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