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Development of micro motion sensors based on piezoresistive and thermo-resistive effects in silicon

机译:基于压阻和硅的热阻效应的微观运动传感器的开发

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This paper presents our latest results on the designs, fabrication and calibration of two micro accelerometers and a convective based gyroscope, as well as their combination to create a motion sensor for inertial navigation applications. Among the two accelerometers, the first one is a 3-DOF micro accelerometer utilizing piezoresistive effect in single crystal silicon. The sensing structure consists of four sensing-beams surrounding a seismic-mass. Therefore, the sensor is smaller than the cross-beam type accelerometer. The second accelerometer is a dual axis thermal accelerometer, working based on the thermo-resistive effect of silicon thermistors in free convective regime. Since no seismic mass is used, the shock-resistance becomes very high (up to 9.0?06g). The novel structure of the thermistors eliminated up to 93% of stress induced by temperature. The dual-axis gas gyroscope proposed here is working based on the thermo-resistive effect of light-doped silicon thermistor and the force convective heat transfer. The sensor configuration consists of a gas pump and a micro thermistor sensing element, packaged in an aluminum case with overall diameter and length of 14mm and 25mm, respectively. Unlike vibrating gyroscopes reported recently in MEMS-field, our gyroscope has "no" seismic mass; therefore it can eliminate the inherent problems such as fragility, low shock-resistance, squeezed-film air-damping, etc. Moreover, since the driving power for the moving mass is not necessary, the power consumption is also reduced. Finally, an algorithm to process the signal from a system consists of a 3-DOF accelerometer and 3-DOF gyroscope is presented. In this algorithm, quaternion based calculation was applied instead of Euler angles, therefore the problems of singularity or complicated trigonometric calculations can be avoided. The algorithm can be applied for inertial navigation systems (INS).
机译:本文提出了我们在两个微加速度计的设计,制造和校准和基于对流的陀螺仪的设计,制造和校准的最新结果,以及它们的组合,以创建用于惯性导航应用的运动传感器。在两个加速度计中,第一个是在单晶硅中使用压阻效应的3-DOF微加速度计。传感结构包括四个围绕地震块的传感梁组成。因此,传感器小于横梁型加速度计。第二加速度计是双轴热加速度计,基于硅热敏电阻在自由对流状态下的热阻效应。由于没有使用地震块,因此抗冲击性变得非常高(高达9.0?06g)。热敏电阻的新颖结构可消除高达93%的压力诱导的温度。此处提出的双轴气体陀螺仪是基于光掺杂硅热敏电阻和力对流热传递的热阻效应。传感器构造包括气泵和微热敏电阻传感元件,分别封装在铝壳中,分别具有14mm和25mm的整体直径和长度。与最近在MEMS场中报告的振动陀螺仪不同,我们的陀螺仪具有“否”地震块;因此,它可以消除脆弱性,低抗冲击性,挤压膜空气阻尼等固有问题。此外,由于不需要用于移动质量的驱动功率,因此电力消耗也降低。最后,通过系统处理信号的算法包括3-DOF加速度计,并提出了3-DOF陀螺仪。在该算法中,应用了基于四元的计算而不是欧拉角,因此可以避免奇点或复杂三角形计算的问题。该算法可以应用于惯性导航系统(INS)。

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