Attitude Measurement for High-Spinning Projectile with a Hollow MEMS IMU Consisting of Multiple Accelerometers and Gyros.

Sensors (Basel) · 2019 · PMC6515412 · PMID 30991707

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showed a trendno p-value reported

The roll angle error during the whole flight test is about 7°, and the error showed a trend of divergence.

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