Turbulence Error Modeling and Restriction for Satellite Attitude Determination System Based on Improved Maximum Correntropy Kalman Filter

Turbulence Error Modeling and Restriction for Satellite Attitude Determination System Based on Improved Maximum Correntropy Kalman Filter

In the process of satellite attitude determination, satellites or sensors themselves often encounter a variety of turbulence influences due to the complexity of space environments. Such influences can lead to the mutation and non-Gaussian noises for the attitude determination system. To solve these...

Full description

Bibliographic Details
Main Authors: Jiongqi Wang, Yuyun Chen, Bowen Hou, Bowen Sun, Jian Peng, Zhangming He
Format: Article
Language:English
Published: IEEE 2019-01-01
Series:IEEE Access
Subjects:
Satellite attitude
star tracker
turbulence influence
fading factor
maximum correntropy filter
accuracy analysis
Online Access:https://ieeexplore.ieee.org/document/8848495/

Internet

https://ieeexplore.ieee.org/document/8848495/

Similar Items