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考虑SAR图像导航量测特性的SAR/INS组合导航非线性滤波

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  • 南京航空航天大学导航研究中心,南京210016

收稿日期: 2009-10-22

  修回日期: 2010-05-19

  网络出版日期: 2010-07-23

基金资助

国家自然科学基金(No.60904091);航空科学基金(20090852012)资助

Non-linear Filtering for SAR/INS Integrated Navigation Considering SAR Image Navigation Measurement Characteristics

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  • Navigation Research Center, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China

Received date: 2009-10-22

  Revised date: 2010-05-19

  Online published: 2010-07-23

Supported by

熊智,博士,副教授,研究方向:惯性技术、景象匹配辅助导航、天文导航及惯性组合导航等,E-mail:xznuaa@nuaa.edu.cn
刘建业,教授,博导,研究方向:惯性导航、卫星导航、组合导航、导航与控制、车载导航与智能交通等,E-mail:ljyac@nuaa.edu.cn

摘要

SAR/INS组合导航系统中,当SAR量测输出时间间隔较长时,惯性导航得不到及时修正,系统将具有较强的非线性特性,导致常规卡尔曼滤波算法的精度受到影响甚至滤波发散. 为了提高组合导航的精度,该文结合惯性导航系统的非线性模型,设计基于无迹卡尔曼滤波(UKF)解决非等间隔量测修正的SAR/INS组合导航非线性滤波算法,并通过协方差分析对比研究常规卡尔曼滤波和该文算法的性能. 仿真结果验证了该文算法具有更高的精度.

本文引用格式

王丹, 熊智, 陈方, 刘建业 . 考虑SAR图像导航量测特性的SAR/INS组合导航非线性滤波[J]. 应用科学学报, 2010 , 28(4) : 381 -386 . DOI: 10.3969/j.issn.0255-8297.2010.04.009

Abstract

The SAR image navigation system is highly nonlinear when it takes long time to output measurement in the SAR integrated navigation system (SAR/INS), and when the inertial navigation error cannot be modified in time. Using conventional Kalman filtering to deal with the nonlinear system, the filter accuracy is affected and even becomes divergent. In order to improve the integrated navigation precision, based on SAR/INS coupled navigation system and the unscented Kalman filtering (UKF), we propose a UKF algorithm for unequal interval problems, and solve problems of information fusion in SAR/INS. Performances of conventional Kalman filtering and the UKF algorithm are studied in simulation analyses of covariance. The result
demonstrates that the method proposed in this paper produces better filtering precision.

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