An Improved In-Motion Alignment Method for SINS/GPS With the Sliding Windows Integration

被引:1
|
作者
Xu, Xiang [1 ]
Zheng, Xuehe [2 ]
Li, Yao [3 ]
Yao, Yiqing [3 ]
Zhou, Hui [1 ]
Zhu, Lihua [4 ]
机构
[1] Nanjing Univ Sci & Technol, Sch Automat, Nanjing 210094, Peoples R China
[2] Second Acad China Aerosp Sci & Ind Corp Ltd, Beijing 100854, Peoples R China
[3] Southeast Univ, Key Lab Micro Inertial Instrument & Adv Nav Techn, Minist Educ, Nanjing 210096, Peoples R China
[4] Nanjing Univ Sci & Technol, Sch Mech Engn, Nanjing 210094, Peoples R China
基金
中国国家自然科学基金;
关键词
Strapdown inertial navigation system (SINS); global positioning system (GPS); in-motion alignment method; sliding windows operation; SINS/DVL;
D O I
10.1109/TVT.2023.3263835
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, an improved in-motion alignment method for SINS/GPS integration is proposed. The alignment errors, which are caused by the maneuvering of the vehicle and the accumulated errors of inertial sensor errors, are suppressed. Firstly, the traditional in-motion alignment method for SINS/GPS integration is reviewed, and the existing problems, which are accumulated errors in the observed vectors, are investigated. To address these problems, a sliding windows operation for vector observation optimization is proposed. The derivation for the calculation of the new vector observations is given in detail. Using the new vector observations, the accumulated errors, which are existing in the observed vectors, are weakened. Thus, the alignment results are more stable whenever any maneuvering of the vehicle. Lastly, the simulation and field tests are designed for verification of the proposed method. Compared with the currently popular methods, the alignment errors are converged to a small value quickly.
引用
收藏
页码:12491 / 12499
页数:9
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