Evidence map›Paper›PMID 40572352›Full record

ArticleMicromachines2025

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

Xuyang Zhou, Long Chen, Changhao Sun, Wei Jia, Naixin Yi, Wei Sun

Abstract read
In one paragraph

Article in Micromachines, 2025. The graph could read no effect estimate from its abstract, so it casts no vote on the map. Cited by 3 papers.

0numbers the graph read from it
0cells of the map it votes in
3citing papers in PubMed
–field-weighted citation impact
1 · What the graph read from it

What it found

Each row is one number read from the abstract, on the scale the paper reported it, with its interval. Left of the dashed line favours the treatment, right favours the comparator. Under each row is the sentence it came from. New to these charts? A ten-minute tutorial.

The abstract states no effect estimate the extractor could read, or names no intervention and outcome on the map, so this paper lights no cell and moves no belief. It is still indexed, cited and linked below.

2 · The registry

The trial behind it

Trials whose registry record cites this paper, or whose number appears in the abstract. A trial that started after this paper was published is citing it as background, not reporting it.

Neither the registry nor the abstract names a trial number. If this is a trial report, that itself is worth knowing.

3 · Its place in the literature

Who cites it

3 citing papers in PubMed.

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4 · The record

Corrections and comments

PubMed lists nothing against this paper. Absence here is not a guarantee, only a check that was made.

5 · Who and what money

Authors and funding

6 authors.

Xuyang ZhouSchool of Aerospace Science and Technology, Xidian University, Xi'an 710071, China.ORCID 0000-0002-3245-503X
Long ChenCCTEG Xi'an Research Institute (Group) Co., Ltd., Xi'an 710077, China.
Changhao SunQian Xuesen Laboratory of Space Technology, China Academy of Space Technology, Beijing 100094, China.
Wei Jia365th Research Institute, Northwestern Polytechnical University, Xi'an 710072, China.
Naixin YiSchool of Aerospace Science and Technology, Xidian University, Xi'an 710071, China.
Wei SunSchool of Aerospace Science and Technology, Xidian University, Xi'an 710071, China.

Funding

China College Innovation Fund of Production, Education and Research 2021ZYAO8004National Natural Science Foundation of China 62173330National Natural Science Foundation of China 62371375Shaanxi Key R&D Plan Key Industry Innovation Chain Project 2022ZDLGY03-01Xi'an Science and Technology Plan Project 2022JH-RGZN-0039
6 · The paper itself

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.

Indexed as

attitude estimationerror-state extended Kalman filter (ESKF)magnetic interferenceMEMSmultifunctional payloadsorientation decoupling

Identifiers

PMID40572352
PMCPMC12195543

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Read under generation 80e0d062 · epoch 390. Bibliography from PubMed, PubMed Central and OpenAlex; grants from NIH RePORTER; trial links from ClinicalTrials.gov; estimates, votes and beliefs from the OpenQuestion graph.