Control for the Space Tether System Motion
This paper proposed a study of a spatial tether system (STS), composed by two satellite (a main satellite and a subsatellite), with the objective of developing a control system in which the motion of the subsatellite is limited in the orbital plane of the main satellite. The linear quadratic regulat...
Main Authors: | , , |
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Format: | Article |
Language: | English |
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Instituto de Aeronáutica e Espaço (IAE)
2020-11-01
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Series: | Journal of Aerospace Technology and Management |
Subjects: | |
Online Access: | http://www.jatm.com.br/ojs/index.php/jatm/article/view/1147/865 |
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author | Maria Cecilia Zanardi Paola da Rosa Prado Leandro Baroni |
author_facet | Maria Cecilia Zanardi Paola da Rosa Prado Leandro Baroni |
author_sort | Maria Cecilia Zanardi |
collection | DOAJ |
description | This paper proposed a study of a spatial tether system (STS), composed by two satellite (a main satellite and a subsatellite), with the objective of developing a control system in which the motion of the subsatellite is limited in the orbital plane of the main satellite. The linear quadratic regulator (LQR) method is used to implement this control, which is an optimal control with state
feedback to predict the linearization of the equations of motion to calculate the feedback gain, using the resolution of Riccati equation. The results show an effective control, with the motion of the subsatellite limited only to the stretch of the cable that links
both satellites. However, it is necessary to introduce an auxiliary torque, since the linearized equation associated with the second variation of the angle out of the plan does not have a term independent of the state vector. |
first_indexed | 2024-04-14T03:18:23Z |
format | Article |
id | doaj.art-ab0b68c5b05f4b799988cf7d9a2dde03 |
institution | Directory Open Access Journal |
issn | 1984-9648 2175-9146 |
language | English |
last_indexed | 2024-04-14T03:18:23Z |
publishDate | 2020-11-01 |
publisher | Instituto de Aeronáutica e Espaço (IAE) |
record_format | Article |
series | Journal of Aerospace Technology and Management |
spelling | doaj.art-ab0b68c5b05f4b799988cf7d9a2dde032022-12-22T02:15:23ZengInstituto de Aeronáutica e Espaço (IAE)Journal of Aerospace Technology and Management1984-96482175-91462020-11-0112se105116http://dx.doi.org/10.5028/jatm.cab.1157Control for the Space Tether System MotionMaria Cecilia Zanardi0Paola da Rosa Prado1Leandro Baroni2Universidade Federal do ABCUniversidade Federal do ABCUniversidade Federal do ABCThis paper proposed a study of a spatial tether system (STS), composed by two satellite (a main satellite and a subsatellite), with the objective of developing a control system in which the motion of the subsatellite is limited in the orbital plane of the main satellite. The linear quadratic regulator (LQR) method is used to implement this control, which is an optimal control with state feedback to predict the linearization of the equations of motion to calculate the feedback gain, using the resolution of Riccati equation. The results show an effective control, with the motion of the subsatellite limited only to the stretch of the cable that links both satellites. However, it is necessary to introduce an auxiliary torque, since the linearized equation associated with the second variation of the angle out of the plan does not have a term independent of the state vector.http://www.jatm.com.br/ojs/index.php/jatm/article/view/1147/865spatial tether systemcontrollqr method |
spellingShingle | Maria Cecilia Zanardi Paola da Rosa Prado Leandro Baroni Control for the Space Tether System Motion Journal of Aerospace Technology and Management spatial tether system control lqr method |
title | Control for the Space Tether System Motion |
title_full | Control for the Space Tether System Motion |
title_fullStr | Control for the Space Tether System Motion |
title_full_unstemmed | Control for the Space Tether System Motion |
title_short | Control for the Space Tether System Motion |
title_sort | control for the space tether system motion |
topic | spatial tether system control lqr method |
url | http://www.jatm.com.br/ojs/index.php/jatm/article/view/1147/865 |
work_keys_str_mv | AT mariaceciliazanardi controlforthespacetethersystemmotion AT paoladarosaprado controlforthespacetethersystemmotion AT leandrobaroni controlforthespacetethersystemmotion |