TY - GEN
T1 - Attitude determination system based on vector observations for satellites experiencing sun-eclipse phases
AU - Cordova-Alarcon, J. Rodrigo
AU - Mendoza-Barcenas, Mario A.
AU - Solis-Santome, Arturo
N1 - Publisher Copyright:
© Springer International Publishing Switzerland 2015.
PY - 2015
Y1 - 2015
N2 - Due to mission requirements, fault detection and isolation protocols or budget restrictions, a satellite is required to use most reliable attitude determination hardware, such as magnetometers and sun sensors, in order to keep 3-axis attitude information available during its complete orbit. However, satellites experiencing sun-eclipse phases, sun sensors become no operational. In this paper, we propose an attitude determination system which provide 3-axis attitude information in both sun and eclipse phases, considering vector observations acquired from sun and magnetic measurements. To compensate the unavailability of sun sensors during eclipse phase, two variations of innovation processes merged into the Extended Kalman Filters are proposed. In order to keep the accuracy of attitude estimation process during eclipse mode, angular rates must be accurately estimated during sun phase. To solve this issue, rough angular rate information is calculated based on previous attitude information calculated by Gauss-Newton method, which fuse magnetic and sun sensor data. Numerical simulation results show the performance of the proposed attitude determination system, considering the use of vector measurement hardware with different precision degree.
AB - Due to mission requirements, fault detection and isolation protocols or budget restrictions, a satellite is required to use most reliable attitude determination hardware, such as magnetometers and sun sensors, in order to keep 3-axis attitude information available during its complete orbit. However, satellites experiencing sun-eclipse phases, sun sensors become no operational. In this paper, we propose an attitude determination system which provide 3-axis attitude information in both sun and eclipse phases, considering vector observations acquired from sun and magnetic measurements. To compensate the unavailability of sun sensors during eclipse phase, two variations of innovation processes merged into the Extended Kalman Filters are proposed. In order to keep the accuracy of attitude estimation process during eclipse mode, angular rates must be accurately estimated during sun phase. To solve this issue, rough angular rate information is calculated based on previous attitude information calculated by Gauss-Newton method, which fuse magnetic and sun sensor data. Numerical simulation results show the performance of the proposed attitude determination system, considering the use of vector measurement hardware with different precision degree.
KW - Gauss-Newton method
KW - Kalman filter
KW - Satellite attitude determination
UR - http://www.scopus.com/inward/record.url?scp=84928252574&partnerID=8YFLogxK
U2 - 10.1007/978-3-319-09858-6_8
DO - 10.1007/978-3-319-09858-6_8
M3 - Contribución a la conferencia
AN - SCOPUS:84928252574
T3 - Mechanisms and Machine Science
SP - 75
EP - 85
BT - Multibody Mechatronic Systems - Proceedings of the MUSME Conference, 2014
A2 - Martinez, Eusebio Eduardo Hernández
A2 - Ceccarelli, Marco
PB - Kluwer Academic Publishers
T2 - 5th International Symposium on Multibody Systems and Mechatronics, MUSME 2014
Y2 - 21 October 2014 through 24 October 2014
ER -