A Novel Method to Improve the Accuracy of Low-Cost Gyroscope-Based Attitude Estimation by Fusing Angular Acceleration Sensors

Gyroscope-based attitude estimation system has the problem of attitude drift under long-term operation conditions, which is particularly obvious on low-cost gyroscopes. As a new type of inertial sensor, the angular acceleration sensor can directly sense the angular acceleration of the carrier. The error characteristics and the mechanism by which an angular acceleration sensor is sensitive to changes in attitude are different from those of a gyroscope. Therefore, it is a feasible solution to use angular acceleration data to provide error correction for the gyroscope, thereby improving the accuracy of attitude estimation. In this paper, a novel method is proposed to improve the attitude estimation accuracy of low-cost gyroscope by fusing angular acceleration sensors. Based on the data characteristics of two inertial sensors, two different state variables and corresponding observation variables are designed, and the information fusion of the two sensors is realized through Kalman filtering. A synchronous data acquisition device was designed to conduct experimental verification. The experimental results show that the proposed method can improve the attitude estimation accuracy of low-cost gyroscopes under long-term operation conditions.

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Published
2024-11-01
DOI
https://doi.org/10.1109/cac63892.2024.10865618
Primary Topic
Inertial Sensor and Navigation
Type
article
Field-Weighted Citation Impact
0.00

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article

A Novel Method to Improve the Accuracy of Low-Cost Gyroscope-Based Attitude Estimation by Fusing Angular Acceleration Sensors

Zhiwei Xiong, Chaoyang Zhai, Zhiheng Xiao, Meiling Wang
Inertial Sensor and Navigation
article

A Novel Method to Improve the Accuracy of Low-Cost Gyroscope-Based Attitude Estimation by Fusing Angular Acceleration Sensors

Zhiwei Xiong, Chaoyang Zhai, Zhiheng Xiao, Meiling Wang
article en

Abstract

Gyroscope-based attitude estimation system has the problem of attitude drift under long-term operation conditions, which is particularly obvious on low-cost gyroscopes. As a new type of inertial sensor, the angular acceleration sensor can directly sense the angular acceleration of the carrier. The error characteristics and the mechanism by which an angular acceleration sensor is sensitive to changes in attitude are different from those of a gyroscope. Therefore, it is a feasible solution to use angular acceleration data to provide error correction for the gyroscope, thereby improving the accuracy of attitude estimation. In this paper, a novel method is proposed to improve the attitude estimation accuracy of low-cost gyroscope by fusing angular acceleration sensors. Based on the data characteristics of two inertial sensors, two different state variables and corresponding observation variables are designed, and the information fusion of the two sensors is realized through Kalman filtering. A synchronous data acquisition device was designed to conduct experimental verification. The experimental results show that the proposed method can improve the attitude estimation accuracy of low-cost gyroscopes under long-term operation conditions.

Beijing Institute of Technology (CN)
National Natural Science Foundation of China
Affordable and clean energy
Openalex Percentile: Top 55%
Inertial Sensor and Navigation
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A Novel Method to Improve the Accuracy of Low-Cost Gyroscope-Based Attitude Estimation by Fusing Angular Acceleration Sensors — Zhiwei Xiong, Chaoyang Zhai, et al. · (2024) | TGRS Research Map | TGRS