Highly Accurate Attitude Estimation of Unmanned Aerial Vehicle Payloads Using Low-Cost MEMS.

IF 3 3区 工程技术 Q2 CHEMISTRY, ANALYTICAL
Micromachines Pub Date : 2025-05-27 DOI:10.3390/mi16060632
Xuyang Zhou, Long Chen, Changhao Sun, Wei Jia, Naixin Yi, Wei Sun
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引用次数: 0

Abstract

Low-cost MEMS sensors are widely utilized in UAV platforms to address attitude estimation problems due to their compact size, low power consumption, and cost-effectiveness. Diverse UAV payloads pose new challenges for attitude estimation, such as magnetic interference environments and high dynamic environments. In this paper, we propose a hierarchical decoupled attitude estimation algorithm, termed HDAEA. Initially, a novel hierarchical decoupling approach is introduced for the attitude and angle representation of the direction cosine matrix, enabling the representation of angles in a new manner. This method reduces the data dimensionality and nonlinearity of observation equations. Furthermore, a magnetic interference identification algorithm is proposed to compute the magnetic interference intensity accurately and quantitatively. Combining the quantified errors of estimated state variables, an error model for magnetic interference and attitude angles in high-dynamic environments is constructed. Subsequently, the proposed error model is employed to calibrate the hierarchical decoupled angles using accelerometer and magnetometer measurements, effectively mitigating the impact of magnetic interference on the calculation of pitch angles and roll angles. Moreover, the integration of the proposed hierarchical decoupled attitude estimation algorithm with the error-state extended Kalman filter reduces system nonlinearity and minimizes linearization errors. Experimental results demonstrate that HDAEA exhibits significantly improved attitude estimation accuracy of UAV payloads.

基于低成本MEMS的无人机有效载荷高精度姿态估计。
低成本MEMS传感器因其体积小、功耗低、成本效益高而广泛应用于无人机平台,解决姿态估计问题。不同的无人机载荷对姿态估计提出了新的挑战,如磁干扰环境和高动态环境。本文提出了一种分层解耦姿态估计算法,称为HDAEA。首先,对方向余弦矩阵的姿态和角度表示引入了一种新的分层解耦方法,使角度表示成为一种新的方式。该方法降低了观测方程的数据维数和非线性。在此基础上,提出了一种磁干扰识别算法,以准确定量地计算磁干扰强度。结合状态变量估计的量化误差,建立了高动态环境下磁干扰与姿态角的误差模型。随后,利用该误差模型对加速度计和磁强计测量的分层解耦角进行标定,有效地减轻了磁干扰对俯仰角和滚转角计算的影响。此外,将层次解耦姿态估计算法与误差状态扩展卡尔曼滤波相结合,降低了系统的非线性,使线性化误差最小化。实验结果表明,该方法显著提高了无人机有效载荷的姿态估计精度。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
Micromachines
Micromachines NANOSCIENCE & NANOTECHNOLOGY-INSTRUMENTS & INSTRUMENTATION
CiteScore
5.20
自引率
14.70%
发文量
1862
审稿时长
16.31 days
期刊介绍: Micromachines (ISSN 2072-666X) is an international, peer-reviewed open access journal which provides an advanced forum for studies related to micro-scaled machines and micromachinery. It publishes reviews, regular research papers and short communications. Our aim is to encourage scientists to publish their experimental and theoretical results in as much detail as possible. There is no restriction on the length of the papers. The full experimental details must be provided so that the results can be reproduced.
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