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A New Silicon Tuning Fork Gyroscope for Aerospace Applications

机译:用于航空航天应用的新型硅调谐叉陀螺

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For several years THALES Aerospace has been developing a silicon micro-machined tuning fork gyroscope for military and civil applications. The targeted performance is: bias and scale factor errors of 10°/h and 500ppm for a range of 1000°/s. The technology is based on Deep Reactive Ion Etching (DRIE) on a SOI wafer. Associated with an in-plane design for the drive and sense modes, this technology leads to a high geometric precision and allows the realization of the sense and the drive mechanical resonators, and trimming elements within a single active layer. Good bias stability is achieved by cancelling the quadrature bias with electrostatic trimming. The signal processing of the gyro is primarily digital and consists of two main closed loops, for controlling the drive and sense modes, and an auxiliary loop for cancelling the quadrature bias. The typical results obtained on a demonstrator of a third generation device are the following: random walk=0.01°/√h, bias instability<0.1°/h, noise of 0.005°/s over 0-50Hz, with a 1000°/s range (adjustable by the electronics), bias and scale factor errors of 8°/h and 28 ppm in the temperature range -25°C, 70°C, linearity error<0.1°/s over 1000°/s. A high g shock test of 20000g has been carried out on a hardened prototype without any observable performance degradation.
机译:几年来,THALES航天已经发展了军用和民用领域的硅微机械音叉陀螺仪。目标性能是:对一系列的1000℃/秒的10℃/小时和500ppm的偏差和比例因子误差。该技术是基于深反应离子蚀刻(DRIE)在SOI晶片上。与面内的设计为驱动和感测模式相关联,该技术导致高的几何精度,并且允许实现感和驱动机械谐振器,和修整单一活性层内的元件。良好的偏置稳定性是通过消除静电微调正交偏置来实现的。陀螺仪的信号处理主要是数字和由两个主要闭合回路中,用于控制驱动和感测模式,以及用于取消所述正交偏置的辅助回路。上的第三产生装置的演示时获得的典型结果如下:随机游走= 0.01°/√h,偏压不稳定<0.1°/ h时,噪声的0.005°/ s以上0-50Hz,具有1000℃/ s的范围(由电子可调),8°/ h的偏差和比例因子误差和28 ppm的温度范围-25°C,70°C,线性误差<0.1°/ s以上1000℃/秒。 20000克的高g冲击测试已经在硬化的原型进行,没有任何可观察到性能下降。

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