An Efficient Nonlinear Filter for Spacecraft Attitude Estimation
Increasing the computational efficiency of attitude estimation is a critical problem related to modern spacecraft, especially for those with limited computing resources. In this paper, a computationally efficient nonlinear attitude estimation strategy based on the vector observations is proposed. Th...
Saved in:
| Main Authors: | Bing Liu, Zhen Chen, Xiangdong Liu, Fan Yang |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
Wiley
2014-01-01
|
| Series: | International Journal of Aerospace Engineering |
| Online Access: | http://dx.doi.org/10.1155/2014/540235 |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
Efficiency of Hysteresis Rods in Small Spacecraft Attitude Stabilization
by: Assal Farrahi, et al.
Published: (2013-01-01) -
Implementation of a Differential Geometric Filter for Spacecraft Formation Orbit Estimation
by: Shu Ting Goh, et al.
Published: (2012-01-01) -
Estimation of Spacecraft Angular Velocity Based on the Optical Flow of Star Images Using an Optimized Kalman Filter
by: Jiaqian Si, et al.
Published: (2024-12-01) -
Electrodynamic Attitude Stabilization of a Spacecraft in an Elliptical Orbit
by: Maksim A. Klyushin, et al.
Published: (2024-11-01) -
Inter-Spacecraft Rapid Transfer Alignment Based on Attitude Plus Angular Rate Matching Using Q-Learning Kalman Filter
by: Kai Xiong, et al.
Published: (2025-04-01)