Rapid alignment method based on local observability analysis for strapdown inertial navigation system

被引:36
|
作者
Gao, Shesheng [1 ]
Wei, Wenhui [1 ]
Zhong, Yongmin [2 ]
Feng, Zhihua [1 ]
机构
[1] Northwestern Polytech Univ, Sch Automat, Xian 710072, Peoples R China
[2] RMIT Univ, Sch Aerosp Mech & Mfg Engn, Melbourne, Vic, Australia
关键词
Strapdown inertial navigation system; Rapid transfer alignment; Local observability; Observability matrix; Condition number and robust adaptive filter; GPS/INS;
D O I
10.1016/j.actaastro.2013.10.003
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper presents a new method for rapid transfer alignment of strapdown inertial navigation system (SINS) by combining the local observability concept with robust adaptive filtering. The system state and observation models are simplified to analyze the observability of the SINS attitude error. Based on the simplified models, the observability matrix and its condition number are constructed to determine the observability degree of SINS during the process of rapid transfer alignment. On the basis of the local obsersability analysis, a robust adaptive filter is developed to estimate the attitude angle error for SINS rapid transfer alignment. Simulation experiments and comparison analysis have been conducted, demonstrating that the proposed method cannot only effectively measure the local observability of SINS, but it can also enhance the performance of SINS rapid transfer alignment and reduce the alignment time. (C) 2013 IAA. Published by Elsevier Ltd. All rights reserved.
引用
收藏
页码:790 / 798
页数:9
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