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A First-Order Differential Data Processing Method for Accuracy Improvement of Complementary Filtering in Micro-UAV Attitude Estimation

机译:微型无人机姿态估计中互补滤波精度提高的一阶差分数据处理方法

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摘要

There are many algorithms that can be used to fuse sensor data. The complementary filtering algorithm has low computational complexity and good real-time performance characteristics. It is very suitable for attitude estimation of small unmanned aerial vehicles (micro-UAVs) equipped with low-cost inertial measurement units (IMUs). However, its low attitude estimation accuracy severely limits its applications. Though, many methods have been proposed by researchers to improve attitude estimation accuracy of complementary filtering algorithms, there are few studies that aim to improve it from the data processing aspect. In this paper, a real-time first-order differential data processing algorithm is proposed for gyroscope data, and an adaptive adjustment strategy is designed for the parameters in the algorithm. Besides, the differential-nonlinear complementary filtering (D-NCF) algorithm is proposed by combine the first-order differential data processing algorithm with the basic nonlinear complementary filtering (NCF) algorithm. The experimental results show that the first-order differential data processing algorithm can effectively correct the gyroscope data, and the Root Mean Square Error (RMSE) of attitude estimation of the D-NCF algorithm is smaller than when the NCF algorithm is used. The RMSE of the roll angle decreases from 1.1653 to 0.5093, that of the pitch angle decreases from 2.9638 to 1.5542, and that of the yaw angle decreases from 0.9398 to 0.6827. In general, the attitude estimation accuracy of D-NCF algorithm is higher than that of the NCF algorithm.
机译:有许多算法可用于融合传感器数据。互补滤波算法具有较低的计算复杂度和良好的实时性能特征。它非常适用于配备了低成本惯性测量单元(IMU)的小型无人机(micro-UAV)的姿态估计。然而,其低姿态估计精度严重限制了其应用。尽管研究人员提出了许多方法来提高互补滤波算法的姿态估计精度,但很少有研究从数据处理方面进行改进。本文提出了一种实时的陀螺仪数据一阶差分数据处理算法,并针对该算法中的参数设计了自适应调整策略。此外,将一阶差分数据处理算法与基本的非线性互补滤波(NCF)算法相结合,提出了差分非线性互补滤波(D-NCF)算法。实验结果表明,一阶差分数据处理算法可以有效地校正陀螺仪数据,与使用NCF算法相比,D-NCF算法姿态估计的均方根误差(RMSE)较小。侧倾角的RMSE从1.1653减小到0.5093,俯仰角的RMSE从2.9638减小到1.5542,并且偏航角的RMSE从0.9398减小到0.6827。通常,D-NCF算法的姿态估计精度高于NCF算法。

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