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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

周卫东, 蔡佳楠, 孙龙, 等 . GPS/SINS超紧组合导航系统可观测性分析[J]. 北京航空航天大学学报, 2013, 39(9): 1157-1162.
引用本文: 周卫东, 蔡佳楠, 孙龙, 等 . GPS/SINS超紧组合导航系统可观测性分析[J]. 北京航空航天大学学报, 2013, 39(9): 1157-1162.
Zhou Weidong, Cai Jianan, Sun Long, et al. Observability analysis of GPS/SINS ultra-tightly coupled system[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(9): 1157-1162. (in Chinese)
Citation: Zhou Weidong, Cai Jianan, Sun Long, et al. Observability analysis of GPS/SINS ultra-tightly coupled system[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(9): 1157-1162. (in Chinese)

GPS/SINS超紧组合导航系统可观测性分析

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

Observability analysis of GPS/SINS ultra-tightly coupled system

  • 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.

     

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出版历程
  • 收稿日期:  2012-10-11
  • 网络出版日期:  2013-09-30

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