The Quaternion-Based Attitude Error for the Nonlinear Error Model of the INS

被引:12
|
作者
Zhu, Tiangao [1 ]
Liu, Yong [1 ]
Li, Wenkui [1 ]
Li, Kailong [1 ]
机构
[1] Naval Univ Engn, Dept Nav Engn, Wuhan 430033, Peoples R China
基金
中国国家自然科学基金;
关键词
Nonlinear error model; quaternion; attitude error; INS; NAVIGATION SYSTEM; INITIAL ALIGNMENT; KALMAN FILTER; CALIBRATION;
D O I
10.1109/JSEN.2021.3118039
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
In this paper, the quaternion of b-frame based nonlinear error model is proposed for the INS. According to the definition of the attitude error, the quaternion of b-frame based nonlinear error model has been derived by additive and multiplicative relationship. Then, a discussion and analysis is made to compare the proposed model in additive and multiplicative relationship with the quaternion of n-frame based nonlinear error model. In addition, an analysis and comparsion of b-frame and n-frame based nonlinear error model is made to have a theoretical justification to describe why b-frame is superior to n-frame based nonlinear error model. Finally, field tests are carried out to access the performance of the quaternion of b-frame and n-frame based nonlinear error model in the additive and multiplicative relationship for the INS.
引用
收藏
页码:25782 / 25795
页数:14
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