An eight-position self-calibration method for a dual-axis rotational Inertial Navigation System

被引:74
|
作者
Zheng, Zhichao [1 ]
Han, Songlai [2 ]
Zheng, Kefei [3 ]
机构
[1] Huazhong Univ Sci & Technol, Wuhan Natl Lab Optoelect, Sch Optoelect Sci & Engn, Wuhan 430074, Peoples R China
[2] Natl Univ Def Technol, Coll Optoelect Sci & Engn, Changsha 410073, Hunan, Peoples R China
[3] Unitalen Attorneys Law, Beijing 100004, Peoples R China
基金
中国国家自然科学基金;
关键词
Inertial navigation; Inertial measurement unit; Calibration; Kalman filter; G-dependent bias; OBSERVABILITY; DESIGN;
D O I
10.1016/j.sna.2015.05.002
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
An eight-position self-calibration method for a dual-axis rotational Inertial Navigation System (INS) is provided in this paper. By experiencing two more positions with tilt attitudes than those experienced in a conventional six-position method, not only constant biases, scale factor errors, and misalignment errors, but also g-dependent biases can be calibrated. Field tests indicate that, after the calibration and compensation of the g-dependent biases, both a latitude error and a longitude error remain within a small range over time. In contrast, by using the conventional six-position method, a latitude error is several times larger and a longitude error diverges rapidly over time. Compared with the six-position method, accuracy of the dual-axis rotational INS is significantly improved more than 50% by the eight-position self-calibration method. The self-calibration method is feasible both in static and over a ship at the dockside. (C) 2015 Elsevier B.V. All rights reserved.
引用
收藏
页码:39 / 48
页数:10
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