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.

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.

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