GPS/SINS超紧组合导航系统可观测性分析

周卫东; 蔡佳楠; 孙龙; 郑兰

GPS/SINS超紧组合导航系统可观测性分析

哈尔滨工程大学自动化学院, 哈尔滨 150001

基金项目: 国家自然科学基金资助项目(60834005)

详细信息

作者简介:
周卫东(1966-),男,江苏宜兴人,教授,zhouweidong@hrbeu.edu.cn.

中图分类号: V249.3
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- 被引次数: 0
出版历程
- 收稿日期: 2012-10-11
- 网络出版日期: 2013-09-30

Observability analysis of GPS/SINS ultra-tightly coupled system

College of Automation, Harbin Engineering University, Harbin 150001, China

摘要

摘要: 系统状态的可观测性决定了系统的滤波精度.目前,分析系统状态可观测性的主要方法是针对线性系统的,其中奇异值分解(SVD,Singular Value Decomposition)法可以对系统进行事前分析,并且计算简单,成为广泛使用的方法之一.然而集中滤波结构的全球定位系统/捷联惯性导航系统(GPS/SINS,Global Positioning System/Strapdown Inertial Navigation System)超紧组合模型的量测方程是非线性的,对非线性系统进行可观测性分析是非常困难的.针对这个问题,推导出了超紧组合模型线性的量测方程,并证明了该模型满足分段定常系统(PWCS,Piece-Wise Constant System)定理;使用奇异值分解法对其做可观测性仿真,并对实验结果做了全面分析.结果表明:系统状态的可观测性受载体运动状态影响,载体机动性越强,可观测的状态越多,可观测性越高.
- 超紧组合 /
- 分段线性定常系统 /
- 可观测性 /
- 奇异值分解
Abstract: The filter precision depends on the observability of system states. Various approaches were proposed to analyze the observability of the linear system states. Among those approaches, singular value decomposition (SVD) was commonly used to analyze the system beforehand owing to its computational simplicity. However, the measurement equation of global positioning system/strapdown inertial navigation systems (GPS/SINS) ultra-tightly coupled system based on the concentrated filter structure was nonlinear, which made it difficult to analysis the system observability. To solve this problem a linear measurement equation was derived. This GPS/SINS ultra-tightly coupled system model was proved to satisfy the piece-wise constant system (PWCS) theorem and the states' observability of the system were calculated based on the theory of SVD. The results show that the observability of states is affected by the maneuverability of carrier. The stronger maneuverability is, the more observable states are, the higher observability is.
- ultra-tightly coupled /
- piece-wise constant system (PWCS) /
- observability /
- singular value decomposition (SVD)

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参考文献(1)

[1] 王丹力,张洪钺.几种可观测性分析方法及在惯导中的应用[J].北京航空航天大学学报,1999,25(3):342-346 Wang Danli,Zhang Hongyue.Methods for the analysis of observability and their application to INS initial alignment [J].Journal of Beijing University of Aeronautics and Astronautics,1999, 25(3):342-346 (in Chinese) [2] Ham F M,Brown R G.Observability,eigenvalues,and Kalman filtering[J].IEEE Transactions on Aerospace and Electronic Systems,1983,19(2):269-273 [3] Goshen-Meskin D,Bar-Itzhack I Y.Observability analysis of piece-wise constant systems (part II):application to inertial navigation in-flight alignment [J].IEEE Transactions on Aerospace and Electronic Systems,1992,28(4):1068-1075 [4] 万德钧,房建成.惯性导航初始对准[M].南京:东南大学出版社,1998:100-109 Wan Dejun,Fang Jiancheng.Initial alignment of inertial navigation [M].Nanjing:Southeast Press,1998:100-109(in Chinese) [5] Tang Yonggang,Wu Yuanxin,Wu Meiping,et al.INS/GPS integration:global observability analysis [J].IEEE Transactions on Vehicular Technology,2009,58(3):1129-1142 [6] 刘飞,胡小毛,翁海娜,等.SINS/GPS紧耦合系统可观测性分析[J].天津大学学报,2011,44(5):393-395 Liu Fei,Hu Xiaomao,Weng Haina,et al.Observability analysis of SINS/GPS tightly coupled system[J].Journal of Tianjin University,2011,44(5):393-395(in Chinese) [7] Lu Hongqian,Li Mingming,Chen Zhengmin,et al.Observability of geomagnetism/GPS/SINS integration during maneuvers[C]//2011 3rd International Conference on Advanced Computer Control.Harbin,China:Harbin Institute of Technology,2011:604-609 [8] 张涛.GPS/SINS超紧组合导航系统的关键技术研究[D].哈尔滨:哈尔滨工程大学自动化学院,2010 Zhang Tao.The key techniques of ultra-tightly integrated GPS/SINS navigation systems[D].Harbin:College of Automation,Harbin Engineering University,2010 (in Chinese) [9] Babu R,Wang Jinling.Ultra-tight GPS/INS/PL integration:a system concept and performance analysis [J].GPS Solut,2009,13:75-82 [10] Babu R.Ultra-tight integration of GPS/pseudolites/INS:system design and performance analysis[D].Australia:The University of New South Wales,2006 [11] 格雷沃尔.惯性导航组合[M].2版.北京:电子工业出版社,2011 Grewal M S.Global positioning systems inertial navigation,and integration [M].2nd ed.Beijing:Publishing House of Electronics Industry,2011(in Chinese) [12] Babu R,Wang Jinling,Rao G.Analysis of ultra-tight GPS/INS integrated system for navigation performance[C]//IEEE International Conference on Signal Processing,Communications and Networking,Madras Institute of Technology.Chennai,India:Anna University,2008:234-237 [13] 高帅和.分布式GPS/SINS超紧组合架构下的信号处理和信息融合技术研究[D].哈尔滨:哈尔滨工程大学自动化学院,2012 Gao Shuaihe.Research on signal processing and information fusion under distributed ultra-tight GPS/SINS integrated architecture[D].Harbin:College of Automation,Harbin Engineering University,2012 (in Chinese)

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