PMI-Based Nonlinear H∞ Estimation of Unknown Sensor Error for INS/GPS Integrated System

被引:10
作者
Zhong, Maiying [1 ]
Guo, Dingfei [1 ]
Guo, Jia [1 ]
机构
[1] Beihang Univ, Sch Instrument Sci & Optoelect Engn, Beijing 100191, Peoples R China
基金
中国国家自然科学基金;
关键词
Sensor error estimation; INS/GPS integrated system; PMI; nonlinear H-infinity estimator; DESCRIPTOR SYSTEMS; KALMAN FILTER; NAVIGATION; DESIGN;
D O I
10.1109/JSEN.2014.2379719
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
This paper deals with the problem of robust estimation for time-varying sensor errors of inertial navigation system (INS) and global positioning system integration. A nonlinear strapdown INS error model is established to describe the behavior of the the integrated system. Under assumptions of time-varying bias and noise being L-2 norm bounded, a robust H-infinity nonlinear estimator by Krein space theory is proposed and, based on this, a proportional and multi-integral H-infinity estimator is developed for simultaneous estimation of the navigation states and sensor errors. Finally, a flight experiment is implemented to show the effectiveness of the proposed method.
引用
收藏
页码:2785 / 2794
页数:10
相关论文
共 32 条
  • [1] Britting K. R., 1971, P GUID CONTR FLIGHT, P16
  • [2] Novel hybrid of strong tracking Kalman filter and wavelet neural network for GPS/INS during GPS outages
    Chen, Xiyuan
    Shen, Chong
    Zhang, Wei-bin
    Tomizuka, Masayoshi
    Xu, Yuan
    Chiu, Kuanlin
    [J]. MEASUREMENT, 2013, 46 (10) : 3847 - 3854
  • [3] Distributed H∞ Filtering for a Class of Markovian Jump Nonlinear Time-Delay Systems Over Lossy Sensor Networks
    Dong, Hongli
    Wang, Zidong
    Gao, Huijun
    [J]. IEEE TRANSACTIONS ON INDUSTRIAL ELECTRONICS, 2013, 60 (10) : 4665 - 4672
  • [4] Predictive Iterated Kalman Filter for INS/GPS Integration and Its Application to SAR Motion Compensation
    Fang, Jiancheng
    Gong, Xiaolin
    [J]. IEEE TRANSACTIONS ON INSTRUMENTATION AND MEASUREMENT, 2010, 59 (04) : 909 - 915
  • [5] UKF for Integrated Vision and Inertial Sensors Based on Three-View Geometry
    Fang, Qiang
    Huang, Sheng Xin
    [J]. IEEE SENSORS JOURNAL, 2013, 13 (07) : 2711 - 2719
  • [6] Kalman and Smooth Variable Structure Filters for Robust Estimation
    Gadsden, Stephen Andrew
    Habibi, Saeid
    Kirubarajan, Thia
    [J]. IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2014, 50 (02) : 1038 - 1050
  • [7] Fault estimation and fault-tolerant control for descriptor systems via proportional, multiple-integral and derivative observer design
    Gao, Z.
    Ding, S. X.
    [J]. IET CONTROL THEORY AND APPLICATIONS, 2007, 1 (05) : 1208 - 1218
  • [8] Gao Z., 2007, P 6 IFAC S FAULT DET, P1039
  • [9] UNIFIED APPROACH TO INERTIAL NAVIGATION SYSTEM ERROR MODELING
    GOSHENMESKIN, D
    BARITZHACK, IY
    [J]. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1992, 15 (03) : 648 - 653
  • [10] Groves PD, 2008, ARTECH HSE GNSS TECH, P3