Adaptive Robust Minimum Error Entropy Unscented Kalman Filter for Satellite Attitude Estimation

被引:4
|
作者
Qian, Huaming [1 ]
Chu, Shuai [2 ]
Zhao, Di [3 ]
机构
[1] Harbin Engn Univ, Sch Intelligence Syst Sci & Engn, Harbin 150000, Peoples R China
[2] Harbin Engn Univ, Sch Intelligence Syst Sci & Engn, Harbin 150000, Peoples R China
[3] Harbin Engn Univ, Sch Intelligence Syst Sci & Engn, Harbin 150000, Peoples R China
基金
中国国家自然科学基金;
关键词
CORRENTROPY; VISION;
D O I
10.1061/(ASCE)AS.1943-5525.0001456
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
In recent years, the Kalman filter based on the minimum error entropy (MEE) criterion has been proposed, which outperforms the traditional Kalman filter in the presence of non-Gaussian noise. In practical applications, the estimated performance of the MEE unscented Kalman filter (MEE-UKF) algorithm is influenced by the kernel bandwidth (KB). In addition, it may be unstable in numerical computation. This paper proposes an adaptive robust MEE unscented Kalman filter (AMEE-UKF) to address the problem of instability in numerical computation. In addition, by setting an adaptive factor to optimize the MEE-UKF, an appropriate value of the KB can be obtained adaptively. The high accuracy and robustness of the AMEE-UKF were demonstrated by the simulation experiments. (C) 2022 American Society of Civil Engineers.
引用
收藏
页数:12
相关论文
共 50 条
  • [1] Robust Power System State Estimation With Minimum Error Entropy Unscented Kalman Filter
    Dang, Lujuan
    Chen, Badong
    Wang, Shiyuan
    Ma, Wentao
    Ren, Pengju
    IEEE TRANSACTIONS ON INSTRUMENTATION AND MEASUREMENT, 2020, 69 (11) : 8797 - 8808
  • [2] Adaptive Tuning of the Unscented Kalman Filter for Satellite Attitude Estimation
    Soken, Halil Ersin
    Sakai, Shin-ichiro
    JOURNAL OF AEROSPACE ENGINEERING, 2015, 28 (03)
  • [3] Robust attitude estimation using an adaptive unscented Kalman filter
    Chiella, Antonio C. B.
    Teixeira, Bruno O. S.
    Pereira, Guilherme A. S.
    2019 INTERNATIONAL CONFERENCE ON ROBOTICS AND AUTOMATION (ICRA), 2019, : 7748 - 7754
  • [4] Robust adaptive unscented Kalman filter for attitude estimation of pico satellites
    Hajiyev, Chingiz
    Soken, Halil Ersin
    INTERNATIONAL JOURNAL OF ADAPTIVE CONTROL AND SIGNAL PROCESSING, 2014, 28 (02) : 107 - 120
  • [5] Robust double gain unscented Kalman filter for small satellite attitude estimation
    Cao, Lu
    Yang, Weiwei
    Li, Hengnian
    Zhang, Zhidong
    Shi, Jianjun
    ADVANCES IN SPACE RESEARCH, 2017, 60 (03) : 499 - 512
  • [6] Robust unscented Kalman filter for nanosat attitude estimation
    Daero Lee
    George Vukovich
    Regina Lee
    International Journal of Control, Automation and Systems, 2017, 15 : 2161 - 2173
  • [7] Robust Unscented Kalman Filter for Nanosat Attitude Estimation
    Lee, Daero
    Vukovich, George
    Lee, Regina
    INTERNATIONAL JOURNAL OF CONTROL AUTOMATION AND SYSTEMS, 2017, 15 (05) : 2161 - 2173
  • [8] Attitude determination for satellite using adaptive unscented Kalman filter
    Xiao L.
    Wang S.-J.
    Chang L.
    Zhou M.-L.
    Guangxue Jingmi Gongcheng/Optics and Precision Engineering, 2021, 29 (03): : 637 - 645
  • [9] Adaptive Unscented Kalman Filter with Multiple Fading Factors for Pico Satellite Attitude Estimation
    Soken, Halil Ersin
    Hajiyev, Chingiz
    RAST 2009: PROCEEDINGS OF THE 4TH INTERNATIONAL CONFERENCE ON RECENT ADVANCES IN SPACE TECHNOLOGIES, 2009, : 541 - 546
  • [10] Quaternion-Based Robust Attitude Estimation Using an Adaptive Unscented Kalman Filter
    Chiella, Antonio C. B.
    Teixeira, Bruno O. S.
    Pereira, Guilherme A. S.
    SENSORS, 2019, 19 (10):