Centralized fault-tolerant Kalman filter for integrated navigation

被引:0
|
作者
Zhao L. [1 ]
Kang Y. [1 ]
Cheng J. [1 ]
Wu M. [1 ]
机构
[1] College of Intelligent Systems Science and Engineering, Harbin Engineering University, Harbin
关键词
Adaptive factor; Adaptive filter; Centralized filter; Equivalent weight function; Fault-tolerant filter; Integrated navigation; Quality evaluation; Ramp errors;
D O I
10.11990/jheu.201912061
中图分类号
学科分类号
摘要
The traditional centralized Kalman filter employed by integrated navigation systems with multi-source information is unable to limit the ramp measurement error. In this paper, a fault-tolerant Kalman filter (FTKF), which takes the prior probability distribution into account, is proposed based on the maximum likelihood estimation to restrain step errors, impulse errors, and ramp errors. The quality evaluation method and function are designed to evaluate the measurement availability and the equivalent weight function and adaptive factor are constructed based on the quality evaluation information. By adjusting the weight of measurement information, the influence of gross measurement error including slope noise on the filtering accuracy and reliability is limited and fault-tolerant filtering is realized. The algorithm is applied to the multi-sensor integrated navigation system for simulation and verification. The simulation results show that, when employed by an integrated navigation system, the proposed FTKF can limit the measurement outliers, including step errors, impulse errors, and ramp errors, and improve the filter accuracy and reliability. Copyright ©2021 Journal of Harbin Engineering University.
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页码:845 / 850
页数:5
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  • [1] BIBULI M, PASCOAL A, RIDAO P, Et al., Introduction to the special section on navigation, control, and sensing in the marine environment, Annual reviews in control, 40, pp. 127-128, (2015)
  • [2] XIONG Zhi, SHAO Hui, HUA Bing, Et al., An improved fault tolerant federated filter with fault isolation, Acta aeronautica et astronautica sinica, 36, 3, pp. 929-938, (2015)
  • [3] HAN Qiang, LI Baoguo, CHEN Kechuan, The Improvement two levels of fault detection algorithm based on the consistency between the measurement of federal filter, Navigation and control, 16, 3, pp. 61-65, (2017)
  • [4] LI Shengnan, MEI Jinsong, QU Qiang, Et al., Research on SINS/GPS/CNS fault-tolerant integrated navigation system with air data system assistance, 2016 IEEE Chinese Guidance, Navigation and Control Conference, pp. 2366-2370, (2016)
  • [5] BHATTI U I, OCHIENG W Y, FENG Shaojun, Performance of rate detector algorithms for an integrated GPS/INS system in the presence of slowly growing error, GPS solutions, 16, 3, pp. 293-301, (2012)
  • [6] WANG Qi, XU Xiaosu, Application of fault-tolerant technology to integrated navigation system of underwater vehicle, Journal of Chinese inertial technology, 16, 2, pp. 167-170, (2008)
  • [7] ALLERTON D J, JIA Huamin, A review of multisensor fusion methodologies for aircraft navigation systems, The journal of navigation, 58, 3, pp. 405-417, (2005)
  • [8] ZHAO Lin, KANG Yingyao, CHENG Jianhua, Et al., A fault-tolerant polar grid SINS/DVL/USBL integrated navigation algorithm based on the centralized filter and relative position measurement, Sensors, 19, 18, (2019)
  • [9] FAN Xiaoliang, Research on integrated navigation algorithm of SINS/DVL based on adaptive filtering, (2018)
  • [10] GAO Shesheng, SONG Feibiao, JIANG Weiwei, Robust adaptive model predictive filtering algorithm and application to integrated navigation, Journal of Chinese inertial technology, 19, 6, pp. 701-705, (2011)