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
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