GMM-Based Adaptive Extended Kalman Filter Design for Satellite Attitude Estimation under Thruster-Induced Disturbances.

Kim, Taeho; Zewge, Natnael S; Bang, Hyochoong; Yoon, Hyosang

Kim, Taeho; Zewge, Natnael S; Bang, Hyochoong; Yoon, Hyosang.

Afiliación

Kim T; Department of Aerospace Engineering, Korea Advanced Institute of Science and Technology, 201 Daehak-ro, Yuseong-gu, Daejeon 34141, Republic of Korea.
Zewge NS; Department of Aerospace Engineering, Korea Advanced Institute of Science and Technology, 201 Daehak-ro, Yuseong-gu, Daejeon 34141, Republic of Korea.
Bang H; Department of Aerospace Engineering, Korea Advanced Institute of Science and Technology, 201 Daehak-ro, Yuseong-gu, Daejeon 34141, Republic of Korea.
Yoon H; Department of Aerospace Engineering, Korea Advanced Institute of Science and Technology, 201 Daehak-ro, Yuseong-gu, Daejeon 34141, Republic of Korea.

Sensors (Basel) ; 23(9)2023 Apr 23.

Article en En | MEDLINE | ID: mdl-37177418

Palabras clave

Gaussian mixture model; adaptive extended Kalman filter; blurred star image; non-Gaussian noise; satellite attitude estimation; thruster-induced disturbance

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Texto completo: 1 Colección: 01-internacional Base de datos: MEDLINE Tipo de estudio: Prognostic_studies Idioma: En Revista: Sensors (Basel) Año: 2023 Tipo del documento: Article Pais de publicación: Suiza

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