Poster abstract: Precision improvement of aircrafts attitude estimation through gyro sensors data fusion in a redundant inertial measurement unit

T. Grigorie, R. Botez
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Abstract

The paper presents a redundant strap-down attitude system which uses three miniaturized gyro sensors linear clusters in the inertial detection unit. The data from the sensors in each of the three clusters are fused by using a statistical method based on the minimum variance method, in order to improve the useful angular speed signal measured by the detection unit.
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摘要:利用冗余惯性测量单元中陀螺传感器数据融合提高飞机姿态估计精度
提出了一种冗余捷联姿态系统,该系统在惯性检测单元中采用了3个微型化陀螺仪线性簇。采用基于最小方差法的统计方法对三组传感器的数据进行融合,以提高检测单元测得的有用角速度信号。
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