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Fixed-time rendezvous control of spacecraft with a tumbling target under loss of actuator effectiveness

Boyan Jiang, Qinglei Hu, Michael Friswell

IEEE Transactions on Aerospace and Electronic Systems, Volume: 52, Issue: 4, Pages: 1576 - 1586

Swansea University Author: Michael Friswell

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DOI (Published version): 10.1109/TAES.2016.140406

Abstract

This paper investigates the fixed-time fault-tolerant control problem of spacecraft rendezvous and docking with a freely tumbling target in the presence of external disturbance and thruster faults. More specifically, based on the attitude of the target spacecraft, a line-of-sight coordinate frame is...

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Published in: IEEE Transactions on Aerospace and Electronic Systems
ISSN: 0018-9251
Published: 2016
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URI: https://cronfa.swan.ac.uk/Record/cronfa31364
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first_indexed 2016-12-06T20:37:50Z
last_indexed 2018-12-05T04:45:17Z
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spelling 2018-12-04T09:06:08.9107953 v2 31364 2016-12-06 Fixed-time rendezvous control of spacecraft with a tumbling target under loss of actuator effectiveness 5894777b8f9c6e64bde3568d68078d40 Michael Friswell Michael Friswell true false 2016-12-06 FGSEN This paper investigates the fixed-time fault-tolerant control problem of spacecraft rendezvous and docking with a freely tumbling target in the presence of external disturbance and thruster faults. More specifically, based on the attitude of the target spacecraft, a line-of-sight coordinate frame is defined first, and the dynamical equations relative to the tumbling target are derived to describe the relative position (not six degrees of freedom). Then two fixed-time position controllers are proposed to guarantee that the closed-loop system is stable in finite time in the sense of a fixed-time concept, even in the presence of simultaneous external disturbance and thruster faults. Numerical simulations illustrate that the chaser spacecraft can successfully perform the rendezvous using the proposed controllers. Journal Article IEEE Transactions on Aerospace and Electronic Systems 52 4 1576 1586 0018-9251 31 8 2016 2016-08-31 10.1109/TAES.2016.140406 COLLEGE NANME Science and Engineering - Faculty COLLEGE CODE FGSEN Swansea University 2018-12-04T09:06:08.9107953 2016-12-06T13:31:49.7885026 Faculty of Science and Engineering School of Engineering and Applied Sciences - Uncategorised Boyan Jiang 1 Qinglei Hu 2 Michael Friswell 3 0031364-06122016145019.pdf jiang2016.pdf 2016-12-06T14:50:19.9170000 Output 998434 application/pdf Accepted Manuscript true 2016-12-06T00:00:00.0000000 true
title Fixed-time rendezvous control of spacecraft with a tumbling target under loss of actuator effectiveness
spellingShingle Fixed-time rendezvous control of spacecraft with a tumbling target under loss of actuator effectiveness
Michael Friswell
title_short Fixed-time rendezvous control of spacecraft with a tumbling target under loss of actuator effectiveness
title_full Fixed-time rendezvous control of spacecraft with a tumbling target under loss of actuator effectiveness
title_fullStr Fixed-time rendezvous control of spacecraft with a tumbling target under loss of actuator effectiveness
title_full_unstemmed Fixed-time rendezvous control of spacecraft with a tumbling target under loss of actuator effectiveness
title_sort Fixed-time rendezvous control of spacecraft with a tumbling target under loss of actuator effectiveness
author_id_str_mv 5894777b8f9c6e64bde3568d68078d40
author_id_fullname_str_mv 5894777b8f9c6e64bde3568d68078d40_***_Michael Friswell
author Michael Friswell
author2 Boyan Jiang
Qinglei Hu
Michael Friswell
format Journal article
container_title IEEE Transactions on Aerospace and Electronic Systems
container_volume 52
container_issue 4
container_start_page 1576
publishDate 2016
institution Swansea University
issn 0018-9251
doi_str_mv 10.1109/TAES.2016.140406
college_str Faculty of Science and Engineering
hierarchytype
hierarchy_top_id facultyofscienceandengineering
hierarchy_top_title Faculty of Science and Engineering
hierarchy_parent_id facultyofscienceandengineering
hierarchy_parent_title Faculty of Science and Engineering
department_str School of Engineering and Applied Sciences - Uncategorised{{{_:::_}}}Faculty of Science and Engineering{{{_:::_}}}School of Engineering and Applied Sciences - Uncategorised
document_store_str 1
active_str 0
description This paper investigates the fixed-time fault-tolerant control problem of spacecraft rendezvous and docking with a freely tumbling target in the presence of external disturbance and thruster faults. More specifically, based on the attitude of the target spacecraft, a line-of-sight coordinate frame is defined first, and the dynamical equations relative to the tumbling target are derived to describe the relative position (not six degrees of freedom). Then two fixed-time position controllers are proposed to guarantee that the closed-loop system is stable in finite time in the sense of a fixed-time concept, even in the presence of simultaneous external disturbance and thruster faults. Numerical simulations illustrate that the chaser spacecraft can successfully perform the rendezvous using the proposed controllers.
published_date 2016-08-31T03:38:19Z
_version_ 1763751702741123072
score 11.012678

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