GMM-Based Adaptive Extended Kalman Filter Design for Satellite Attitude Estimation under Thruster-Induced
Taeho Kim1, Natnael S Zewge1, Hyochoong Bang1
1Department of Aerospace Engineering, Korea Advanced Institute of Science and Technology, 201 Daehak-ro, Yuseong-gu, Daejeon 34141, Republic of Korea.
Sensors (Basel, Switzerland)
|May 13, 2023
Summary
This study introduces a Gaussian Mixture Model-adaptive Extended Kalman Filter (GMM-EKF) to improve satellite attitude estimation. The GMM-EKF enhances star image centroid measurements, achieving a 30% performance improvement during station-keeping maneuvers.
Area of Science:
- Aerospace Engineering
- Control Systems
- Signal Processing
Background:
- Star trackers are crucial for satellite attitude determination, but maneuvering causes defocused star images and degrades centroid measurement accuracy.
- Geostationary satellite station-keeping maneuvers, involving thruster misalignment and impulsive torque, induce non-Gaussian noise in star images, complicating attitude estimation.
- Traditional Extended Kalman Filters (EKF) struggle with non-Gaussian noise, leading to inaccurate star vector outcomes.
Purpose of the Study:
- To develop and evaluate an improved filtering method for accurate satellite attitude estimation, specifically addressing non-Gaussian measurement noise during maneuvers.
- To enhance the prediction of measurement vectors by incorporating a Gaussian Mixture Model (GMM) within an adaptive Extended Kalman Filter framework.
Main Methods:
- Implementation of an adaptive Extended Kalman Filter (EKF) to predict measurement vectors using predicted states.
- Integration of a Gaussian Mixture Model (GMM) to assign weighting parameters to Gaussian densities, improving measurement vector prediction.
- Simulation-based performance comparison between the proposed GMM-EKF and the standard EKF for attitude estimation.
Main Results:
- The GMM-EKF demonstrated superior performance compared to the standard EKF in satellite attitude estimation.
- A significant 30% improvement in attitude estimation performance was achieved using the GMM-EKF.
- The GMM-EKF effectively handles non-Gaussian noise inherent in star images during satellite maneuvers.
Conclusions:
- The GMM-EKF offers a more robust and accurate approach for attitude estimation in geostationary satellites undergoing station-keeping maneuvers.
- This method provides a viable solution for mitigating the adverse effects of non-Gaussian measurement noise on attitude determination.
- The enhanced prediction capabilities of the GMM-EKF make it an attractive alternative for improving satellite navigation and control.
Keywords:
Gaussian mixture modeladaptive extended Kalman filterblurred star imagenon-Gaussian noisesatellite attitude estimationthruster-induced disturbanceMore Related Videos
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