In-Motion Alignment Method of SINS Under the Geographic Latitude Uncertainty

被引:8
作者
Sun, Jin [1 ,2 ]
Yang, Jie [3 ,4 ]
Gui, Guan [3 ]
Sari, Hikmet [3 ]
机构
[1] Nanjing Univ Posts & Telecommun, Sch Internet Things, Nanjing 210003, Peoples R China
[2] Shanghai Jiao Tong Univ, State Key Lab Ocean Engn, Shanghai 200240, Peoples R China
[3] Nanjing Univ Posts & Telecommun, Coll Telecommun & Informat Engn, Nanjing 210003, Peoples R China
[4] Xian Univ Posts & Telecommun, Shaanxi Key Lab Informat Commun Network & Sceur, Xian 710121, Peoples R China
基金
美国国家科学基金会; 中国博士后科学基金;
关键词
Estimation; Compass; Gravity; Wavelet transforms; Accelerometers; Vibrations; Heuristic algorithms; In-motion compass alignment; strapdown inertial navigation system (SINS); external velocity; latitude estimation; wavelet filtering; AIDED SINS; FILTER;
D O I
10.1109/TVT.2022.3201903
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
Initial alignment is vital to the strapdown inertial navigation system (SINS), and the in-motion initial alignment is a critical stage for underwater vehicles. In order to realize the in-motion alignment of the SINS under the geographic latitude uncertainty, we propose a latitude estimation method based on wavelet filtering. The external reference velocity is introduced, and the parameter adjustment strategy of the compass alignment control loop under different maneuvering modes is designed to improve the alignment accuracy. Firstly, the influence of line motion on the compass alignment is analyzed, and the in-motion compass alignment scheme of SINS based on the assistance of the external velocity is designed. Then, the error analysis is carried out by using the transfer function of the compass alignment loop. Moreover, the influence of different maneuverability on alignment accuracy is discussed. Finally, the setting strategy of control parameters of the compass alignment loop under different maneuvering modes is put forward. Simulation results are reported to validate the latitude estimation and in-motion alignment performance of the proposed method.
引用
收藏
页码:125 / 135
页数:11
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