Near-Vertical Attitude Determination Based on Balance Correction

被引:9
作者
Cheng, Weibin [1 ]
Hu, Shaobing [1 ]
Zhang, Mingju [1 ]
Song, Hongwei [1 ]
Zhang, Gong [1 ]
Chen, Yongjun [1 ]
机构
[1] Yangtze Univ, Key Lab Explorat Technol Oil & Gas Resources, Minist Educ, Jingzhou 434023, Peoples R China
基金
中国国家自然科学基金;
关键词
Absolute error; accelerometers; attitude determination; error correction; inertial navigation systems (INS); SELF-CALIBRATION METHOD; ROTATION; TECHNOLOGY; ALGORITHM; ALIGNMENT; FILTER; ANGLE; GYRO;
D O I
10.1109/TIM.2021.3070888
中图分类号
TM [电工技术]; TN [电子技术、通信技术];
学科分类号
0808 ; 0809 ;
摘要
At the near-vertical position, the system error is a major factor lowering the attitude accuracy in the attitude determination system, and correction technology is often used to compensate all kinds of system errors. First, the absolute errors of the computed attitude angle including the measurement error and the correction error are analyzed, and the correction error caused by the correction matrix is emphatically derived and discussed. Then, a novel balance correction method with a non-unit correction matrix is proposed and verified theoretically. Finally, an inertial measurement unit (IMU) is tested for the near-vertical position and corrected with the conventional unit matrix and the proposed balance correction. The experimental results suggest that the balance correction under the near-vertical position can enhance the accuracies of the attitude angles over four times than those with the conventional correction.
引用
收藏
页数:9
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