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Nanosatellite attitude estimation using Kalman-type filters with non-Gaussian noise

Tutkimustuotosvertaisarvioitu

Standard

Nanosatellite attitude estimation using Kalman-type filters with non-Gaussian noise. / Cilden-Guler, Demet; Raitoharju, Matti; Piche, Robert; Hajiyev, Chingiz.

julkaisussa: Aerospace Science and Technology, Vuosikerta 92, 09.2019, s. 66-76.

Tutkimustuotosvertaisarvioitu

Harvard

Cilden-Guler, D, Raitoharju, M, Piche, R & Hajiyev, C 2019, 'Nanosatellite attitude estimation using Kalman-type filters with non-Gaussian noise', Aerospace Science and Technology, Vuosikerta. 92, Sivut 66-76. https://doi.org/10.1016/j.ast.2019.05.055

APA

Cilden-Guler, D., Raitoharju, M., Piche, R., & Hajiyev, C. (2019). Nanosatellite attitude estimation using Kalman-type filters with non-Gaussian noise. Aerospace Science and Technology, 92, 66-76. https://doi.org/10.1016/j.ast.2019.05.055

Vancouver

Cilden-Guler D, Raitoharju M, Piche R, Hajiyev C. Nanosatellite attitude estimation using Kalman-type filters with non-Gaussian noise. Aerospace Science and Technology. 2019 syys;92:66-76. https://doi.org/10.1016/j.ast.2019.05.055

Author

Cilden-Guler, Demet ; Raitoharju, Matti ; Piche, Robert ; Hajiyev, Chingiz. / Nanosatellite attitude estimation using Kalman-type filters with non-Gaussian noise. Julkaisussa: Aerospace Science and Technology. 2019 ; Vuosikerta 92. Sivut 66-76.

Bibtex - Lataa

@article{3fea92ea02884c30a8f318026aa6208c,
title = "Nanosatellite attitude estimation using Kalman-type filters with non-Gaussian noise",
abstract = "In order to control the orientation of a satellite, it is important to estimate the attitude accurately. Time series estimation is especially important in micro and nanosatellites, whose sensors are usually low-cost and have higher noise levels than high end sensors. Also, the algorithms should be able to run on systems with very restricted computer power. In this work, we evaluate five Kalman-type filtering algorithms for attitude estimation with 3-axis magnetometer and sun sensor measurements. The Kalman-type filters are selected so that each of them is designed to mitigate one error source for the unscented Kalman filter that is used as baseline. We investigate the distribution of the magnetometer noises and show that the Student's t-distribution is a better model for them than the Gaussian distribution. We consider filter responses in four operation modes: steady state, recovery from incorrect initial state, short-term sensor noise increment, and long-term increment. We find that a Kalman-type filter designed for Student's t sensor noises has the best combination of accuracy and computational speed for these problems, which leads to a conclusion that one can achieve more improvements in estimation accuracy by using a filter that can work with heavy tailed noise than by using a nonlinearity minimizing filter that assumes Gaussian noise.",
author = "Demet Cilden-Guler and Matti Raitoharju and Robert Piche and Chingiz Hajiyev",
year = "2019",
month = "9",
doi = "10.1016/j.ast.2019.05.055",
language = "English",
volume = "92",
pages = "66--76",
journal = "Aerospace Science and Technology",
issn = "1270-9638",
publisher = "Elsevier",

}

RIS (suitable for import to EndNote) - Lataa

TY - JOUR

T1 - Nanosatellite attitude estimation using Kalman-type filters with non-Gaussian noise

AU - Cilden-Guler, Demet

AU - Raitoharju, Matti

AU - Piche, Robert

AU - Hajiyev, Chingiz

PY - 2019/9

Y1 - 2019/9

N2 - In order to control the orientation of a satellite, it is important to estimate the attitude accurately. Time series estimation is especially important in micro and nanosatellites, whose sensors are usually low-cost and have higher noise levels than high end sensors. Also, the algorithms should be able to run on systems with very restricted computer power. In this work, we evaluate five Kalman-type filtering algorithms for attitude estimation with 3-axis magnetometer and sun sensor measurements. The Kalman-type filters are selected so that each of them is designed to mitigate one error source for the unscented Kalman filter that is used as baseline. We investigate the distribution of the magnetometer noises and show that the Student's t-distribution is a better model for them than the Gaussian distribution. We consider filter responses in four operation modes: steady state, recovery from incorrect initial state, short-term sensor noise increment, and long-term increment. We find that a Kalman-type filter designed for Student's t sensor noises has the best combination of accuracy and computational speed for these problems, which leads to a conclusion that one can achieve more improvements in estimation accuracy by using a filter that can work with heavy tailed noise than by using a nonlinearity minimizing filter that assumes Gaussian noise.

AB - In order to control the orientation of a satellite, it is important to estimate the attitude accurately. Time series estimation is especially important in micro and nanosatellites, whose sensors are usually low-cost and have higher noise levels than high end sensors. Also, the algorithms should be able to run on systems with very restricted computer power. In this work, we evaluate five Kalman-type filtering algorithms for attitude estimation with 3-axis magnetometer and sun sensor measurements. The Kalman-type filters are selected so that each of them is designed to mitigate one error source for the unscented Kalman filter that is used as baseline. We investigate the distribution of the magnetometer noises and show that the Student's t-distribution is a better model for them than the Gaussian distribution. We consider filter responses in four operation modes: steady state, recovery from incorrect initial state, short-term sensor noise increment, and long-term increment. We find that a Kalman-type filter designed for Student's t sensor noises has the best combination of accuracy and computational speed for these problems, which leads to a conclusion that one can achieve more improvements in estimation accuracy by using a filter that can work with heavy tailed noise than by using a nonlinearity minimizing filter that assumes Gaussian noise.

U2 - 10.1016/j.ast.2019.05.055

DO - 10.1016/j.ast.2019.05.055

M3 - Article

VL - 92

SP - 66

EP - 76

JO - Aerospace Science and Technology

JF - Aerospace Science and Technology

SN - 1270-9638

ER -