Torque model verification for the GOCE satellite
The modeling of torques acting on satellites is essential for the design of satellite attitude control systems. The GOCE satellite, equipped with accurate accelerometers, star trackers and GPS receivers, presents an opportunity to validate these models. Although the forces on GOCE and other accelero...
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Published in | Advances in space research Vol. 62; no. 5; pp. 1114 - 1136 |
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Main Authors | , , , , |
Format | Journal Article |
Language | English |
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Elsevier Ltd
01.09.2018
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Abstract | The modeling of torques acting on satellites is essential for the design of satellite attitude control systems. The GOCE satellite, equipped with accurate accelerometers, star trackers and GPS receivers, presents an opportunity to validate these models. Although the forces on GOCE and other accelerometer-carrying missions have been extensively analyzed in the past, a similar analysis has so far not yet been made for the torques.
In this paper, we present a set of torque models for the GOCE satellite. It consists of six main parts: (1) magnetic torquer actuators, (2) aerodynamic torque, (3) gravity gradient torque, (4) solar radiation pressure torque, (5) thruster torque, and (6) passive magnetic torque. The magnetic properties of the payload are approximated using a parametrization, of which the parameters are estimated from the observation data.
Based on data recorded during selected spacecraft events, the model for the control torques can be validated and error sources are identified in the other models. The models perform best in roll and pitch, where the standard deviation is reduced to 15.2% and 2.1% of the standard deviation of the control torque around those axes respectively. In yaw the standard deviation is significantly larger at 30.5%. The remaining differences between models and observations show magnetic signatures due to electric currents and signatures of aerodynamic model errors. The latter correspond well with an increase in thermosphere density and wind speed with increased geomagnetic activity. The pitch torque is found to be a potential source of vertical wind data. |
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AbstractList | The modeling of torques acting on satellites is essential for the design of satellite attitude control systems. The GOCE satellite, equipped with accurate accelerometers, star trackers and GPS receivers, presents an opportunity to validate these models. Although the forces on GOCE and other accelerometer-carrying missions have been extensively analyzed in the past, a similar analysis has so far not yet been made for the torques.
In this paper, we present a set of torque models for the GOCE satellite. It consists of six main parts: (1) magnetic torquer actuators, (2) aerodynamic torque, (3) gravity gradient torque, (4) solar radiation pressure torque, (5) thruster torque, and (6) passive magnetic torque. The magnetic properties of the payload are approximated using a parametrization, of which the parameters are estimated from the observation data.
Based on data recorded during selected spacecraft events, the model for the control torques can be validated and error sources are identified in the other models. The models perform best in roll and pitch, where the standard deviation is reduced to 15.2% and 2.1% of the standard deviation of the control torque around those axes respectively. In yaw the standard deviation is significantly larger at 30.5%. The remaining differences between models and observations show magnetic signatures due to electric currents and signatures of aerodynamic model errors. The latter correspond well with an increase in thermosphere density and wind speed with increased geomagnetic activity. The pitch torque is found to be a potential source of vertical wind data. |
Author | Visser, Pieter N.A.M. Doornbos, Eelco N. de Visser, Coen C. Visser, Tim Fritsche, Bent |
Author_xml | – sequence: 1 givenname: Tim surname: Visser fullname: Visser, Tim email: t.visser-1@tudelft.nl organization: Delft University of Technology, Faculty of Aerospace Engineering, Kluyverweg 1, 2629 HS Delft, The Netherlands – sequence: 2 givenname: Eelco N. surname: Doornbos fullname: Doornbos, Eelco N. email: e.n.doornbos@tudelft.nl organization: Delft University of Technology, Faculty of Aerospace Engineering, Kluyverweg 1, 2629 HS Delft, The Netherlands – sequence: 3 givenname: Coen C. surname: de Visser fullname: de Visser, Coen C. email: c.c.devisser@tudelft.nl organization: Delft University of Technology, Faculty of Aerospace Engineering, Kluyverweg 1, 2629 HS Delft, The Netherlands – sequence: 4 givenname: Pieter N.A.M. surname: Visser fullname: Visser, Pieter N.A.M. email: p.n.a.m.visser@tudelft.nl organization: Delft University of Technology, Faculty of Aerospace Engineering, Kluyverweg 1, 2629 HS Delft, The Netherlands – sequence: 5 givenname: Bent surname: Fritsche fullname: Fritsche, Bent email: b.fritsche@htg-hst.de organization: Hyperschall Technologie Göttingen GmbH, Katlenburg-Lindau, Germany |
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Cites_doi | 10.1016/j.asr.2015.05.038 10.2514/1.A32348 10.2514/1.40940 10.1016/j.asr.2014.06.033 10.1007/s00190-011-0498-3 10.1007/s00190-017-1042-x 10.5047/eps.2013.08.003 10.1007/BF03321184 10.2514/3.20626 10.2514/1.37539 10.1016/j.asr.2012.03.011 10.2514/1.A32677 10.1007/s00190-011-0500-0 10.2514/1.48114 10.1002/2016JA023688 10.1002/2016SW001562 |
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Keywords | Satellite torque modeling Satellite aerodynamics Magnetic attitude control Gravity field and steady-state Ocean Circulation Explorer (GOCE) |
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Res.: Space Phys. doi: 10.1002/2016JA023688 contributor: fullname: Dhadly – ident: 10.1016/j.asr.2018.06.025_b0065 – volume: 15 start-page: 558 issue: 4 year: 2017 ident: 10.1016/j.asr.2018.06.025_b0095 article-title: New density estimates derived using accelerometers on-board the CHAMP and GRACE satellites publication-title: Space Weather doi: 10.1002/2016SW001562 contributor: fullname: Mehta |
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SubjectTerms | Gravity field and steady-state Ocean Circulation Explorer (GOCE) Magnetic attitude control Satellite aerodynamics Satellite torque modeling |
Title | Torque model verification for the GOCE satellite |
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