Robust H-infinity CKF/KF hybrid filtering method for SINS alignment

被引:30
|
作者
Zhang, Lei [1 ]
Yang, Chun [1 ]
Chen, Qingwei [1 ]
Yan, Fei [1 ]
机构
[1] Nanjing Univ Sci & Technol, Sch Automat, Nanjing 210094, Jiangsu, Peoples R China
基金
中国国家自然科学基金;
关键词
H filters; Kalman filters; inertial navigation; nonlinear filters; nonlinear estimation; decomposition; statistical analysis; robust H-infinity CKF-KF hybrid filtering method; SINS alignment; in-motion alignment; strapdown inertial navigation system; misalignment angle; nonlinear filtering method; cubature Kalman filter; RHCHF; unscented Kalman filter; statistical property; IN-FLIGHT ALIGNMENT; PERFORMANCE EVALUATION; INITIAL ALIGNMENT; CUBATURE; ATTITUDE; VEHICLE;
D O I
10.1049/iet-smt.2016.0133
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
This study concerns the in-motion alignment in the strapdown inertial navigation system (SINS) with large misalignment angles. As the non-linear filtering method applied in the alignment model is quite computer intensive, which has a significant impact on the alignment accuracy and speed. To solve this problem, a robust H-infinity cubature Kalman filter (CKF)/KF hybrid filter (RHCHF) is proposed to lower the computational burden and strengthen the robustness. By virtue of the idea of model decomposition, the RHCHF could estimate the non-linear and linear parts of alignment model, respectively. Through the introduction of robust factor to adjust the filter parameters, it can ensure the accuracy reliably. The comparisons of the simulation and vehicle experiment demonstrate that the RHCHF could achieve the results at a significantly lower expense than the unscented Kalman filter, and obtain a high accuracy even when the statistical property of noise is uncertain or the outliers of measurement occur occasionally.
引用
收藏
页码:916 / 925
页数:10
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