Adaptive Kalman filtering for spacecraft attitude estimation

被引：0
|
作者：
Li, Wei [1 ]
Liu, Meihong [1 ]
Gong, Deren [1 ]
Duan, Dengping [1 ]
机构：
[1] Institute of Aerospace Science and Technology, Shanghai Jiao Tong University, Shanghai 200240, Rm. 2115, Aerospace Building, No. 800, Dongchuan Road
来源：
Journal of Aeronautics, Astronautics and Aviation | 2013年 / 45卷 / 01期
关键词：
Adaptive Kalman filter; Attitude estimation; Spacecraft;
D O I：
10.6125/12-1112-713
中图分类号：
学科分类号：
摘要：
An adaptive Kalman filter (AKF) algorithm is proposed to model and approximation errors in this work. The adaptive algorithm for model and approximation errors is attained by using an upper bound for the state error prediction covariance matrix. The proposed adaptive filter algorithm has been tested in attitude estimation using gyroscope and star tracker sensors for single spacecraft in flight simulations. Simulation results demonstrate the superior performance of the proposed filter as compared to the standard Kalman filter.
引用
收藏
页码：45 / 50
页数：5
相关论文
共 50 条
  • [1] Adaptive Huber-based Kalman filtering for spacecraft attitude estimation
    Li, Wei
    Liu, Meihong
    Duan, Dengping
    TRANSACTIONS OF THE INSTITUTE OF MEASUREMENT AND CONTROL, 2014, 36 (06) : 828 - 836
  • [2] Adaptive robust cubature Kalman filtering for satellite attitude estimation
    Zhenbing QIU
    Huaming QIAN
    Guoqing WANG
    Chinese Journal of Aeronautics , 2018, (04) : 806 - 819
  • [3] Adaptive robust cubature Kalman filtering for satellite attitude estimation
    Qiu, Zhenbing
    Qian, Huaming
    Wang, Guoqing
    CHINESE JOURNAL OF AERONAUTICS, 2018, 31 (04) : 806 - 819
  • [4] Adaptive robust maximum correntropy cubature Kalman filter for spacecraft attitude estimation
    Chu, Shuai
    Qian, Huaming
    Yan, Shuya
    Ding, Peng
    ADVANCES IN SPACE RESEARCH, 2023, 72 (08) : 3376 - 3385
  • [5] Robust adaptive smooth variable structure Kalman filter for spacecraft attitude estimation
    Liu, Ruixia
    Liu, Ming
    Duan, Guangren
    Cao, Xibin
    AEROSPACE SCIENCE AND TECHNOLOGY, 2024, 144
  • [6] Adaptive Robust Nonlinear Filtering for Spacecraft Attitude Estimation Based on Additive Quaternion
    Qiu, Zhenbing
    Huang, Yulong
    Qian, Huaming
    IEEE TRANSACTIONS ON INSTRUMENTATION AND MEASUREMENT, 2020, 69 (01) : 100 - 108
  • [7] GNSS attitude estimation based on adaptive Kalman filtering using phase measurement
    Zhang, Siyu
    Chang, Guobin
    Chen, Chao
    Zhang, Laihong
    Zhu, Ting
    IET RADAR SONAR AND NAVIGATION, 2020, 14 (05) : 747 - 754
  • [8] Unscented kalman filtering for SINS attitude estimation
    Zhao, Lin
    Nie, Qi
    Guo, Qiufen
    2007 IEEE INTERNATIONAL CONFERENCE ON CONTROL AND AUTOMATION, VOLS 1-7, 2007, : 2720 - 2724
  • [9] Nonlinear filtering for sequential spacecraft attitude estimation with real data: Cubature Kalman Filter, Unscented Kalman Filter and Extended Kalman Filter
    Garcia, R. V.
    Pardal, P. C. P. M.
    Kuga, H. K.
    Zanardi, M. C.
    ADVANCES IN SPACE RESEARCH, 2019, 63 (02) : 1038 - 1050
  • [10] Iterated Unscented Kalman Filter for Spacecraft Attitude Estimation
    Qian, Huaming
    Qiu, Zhenbing
    2018 37TH CHINESE CONTROL CONFERENCE (CCC), 2018, : 4557 - 4562
12345