一种导航级Si-MEMS陀螺仪

S. Koenig, S. Rombach, W. Gutmann, A. Jaeckle, C. Weber, M. Ruf, D. Grolle, J. Rende
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引用次数: 15

摘要

诺斯罗普·格鲁曼LITEF有限公司(NG LITEF)于2003年开始开发具有深度反应离子蚀刻(DRIE)的MEMS陀螺仪芯片。在此基础上,设计了6自由度微机电系统(MEMS)微型化惯性测量单元(μIMU)。在从早期MEMS IMU原型成功转移到批量生产后,NG LITEFs μIMU多年来一直可用,在角度随机漫步(ARW)为0.15°/√(h)的指定4°/h偏置复合误差。最近收到了基于MEMS的姿态航向参考系统(AHRS) LCR-350B的欧洲技术标准订单(ETSO),因此NG LITEF能够向全球航空电子直升机和固定翼市场提供第一个纯MEMS的AHRS。NG LITEFs μIMU的概念是基于三个单陀螺仪模块。为了减少从μIMU中央信号处理板到单个模块的信号线数量,选择了少电极的MEMS陀螺仪芯片概念。这种方法的主要缺点之一是电气操作方案的高度复杂性,利用几个辅助控制回路在少数电极上复用。由于μIMU的高复杂度和信号处理,对计算能力有很高的要求。去年,NG LITEF进行了一项研究,旨在通过优化现有的电气操作方案来提高性能。由于这些活动,在不重新设计MEMS陀螺仪芯片的情况下,ARW和偏置误差显著降低。目前,单轴陀螺仪的温度偏置模型误差为0.25°/h,偏置不稳定性< 0.03°/h, ARW低于0.025°/√h。本文涵盖了与改进操作方案相关的偏置和ARW的改进,以及对下一个MEMS陀螺仪改进和NG LITEF计划的进一步MEMS陀螺仪开发活动的展望。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Towards a navigation grade Si-MEMS gyroscope
Northrop Grumman LITEF GmbH (NG LITEF) started the development of MEMS gyroscope chips with Deep Reactive Ion Etching (DRIE) in 2003. In parallel a 6 degree of freedom (DOF) micro electro mechanical system (MEMS) miniaturized inertial measurement unit (μIMU), based on these MEMS gyroscope chips and MEMS accelerometer chips also processed with DRIE, was designed. After successful transfer from early MEMS IMU prototypes to series production, NG LITEFs μIMU is available since many years with a specified 4°/h bias composite error at an angular random walk (ARW) of 0.15 °/√(h). Recently an European Technical Standard Order (ETSO) for the MEMS based Attitude Heading Reference System (AHRS) LCR-350B was received, so that NG LITEF is able to supply the first purely MEMS based AHRS worldwide to the avionic helicopter and fixed-wing market.The concept of NG LITEFs μIMU is based on three single gyroscope modules. In order to reduce the number of signal lines from the central signal processing board of the μIMU to the single modules, a MEMS gyro chip concept with only a few electrodes was selected. One of the major drawbacks of this approach is the high complexity of the electrical operation scheme, utilizing several auxiliary control loops multiplexed over the small number of electrodes.Due to the high complexity and the signal processing in the μIMU, a high level of computing power is required. In the last year NG LITEF has conducted research in order to improve the performance simply by optimizing the existing electrical operation scheme. As a result of these activities, ARW and bias error were reduced significantly without redesign of the MEMS gyroscope chips. Today, a single axis gyroscope performance of the order of 0.25 °/h bias model error over temperature, bias instability < 0.03 °/h and an ARW of below 0.025 °/√h can be presented.The paper covers the improvement in bias and ARW associated with the improved operation scheme as well as an outlook to the next MEMS gyro improvements and further MEMS gyro development activities planned at NG LITEF.
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