基于真实飞行试验场景的双装备MEMS IMU评估

IEEE/ION Position Location and Navigation Symposium : [proceedings]. IEEE/ION Position Location and Navigation Symposium Pub Date : 2010-05-04 DOI:10.1109/PLANS.2010.5507129

M. Becker, U. Bestmann, A. Schwithal, P. Hecker, R. Bott, P. Kohl, S. Knedlik, H. Scheyer, E. V. Hinuber

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引用次数: 4

摘要

在提出的工作中研究的惯性测量单元(IMU)分别由两组(可选三组)不同的MEMS加速度计和陀螺仪组成。两套安装在一个外壳，因此受到相同的校准程序。这些双传感器组的不同组合可以用来利用互补的传感器特性，例如测量范围，分辨率和噪声特性，以及从机载应用中的冗余中受益。

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Evaluation of a double equipped MEMS IMU based on real flight trial scenarios

The Inertial Measurement Unit (IMU) investigated within the presented work consists of two (optional three) dissimilar sets of MEMS accelerometers and gyros, respectively. Both sets are mounted in one enclosure and thus are subject to the same calibration procedure. Different combinations of these dual sensor sets can be used to exploit the complementary sensor properties, e.g. measurement range, resolution and noise characteristics as well as to benefit from redundancy in airborne applications.

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IEEE/ION Position Location and Navigation Symposium : [proceedings]. IEEE/ION Position Location and Navigation Symposium

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