Adaptive tracking algorithm for a rigid spacecraft with input saturation

Wang, Y; Yu, F; Bishop, A; Yu, C

Adaptive tracking algorithm for a rigid spacecraft with input saturation

Wang, Y Yu, F Bishop, A

Yu, C

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Publication Type:: Conference Proceeding
Citation:: Proceedings of the 28th Chinese Control and Decision Conference, CCDC 2016, 2016, pp. 1605 - 1610
Issue Date:: 2016-08-03

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Field	Value	Language
dc.contributor.author	Wang, Y	en_US
dc.contributor.author	Yu, F	en_US
dc.contributor.author	Bishop, A https://orcid.org/0000-0001-8581-8562	en_US
dc.contributor.author	Yu, C	en_US
dc.date.issued	2016-08-03	en_US
dc.identifier.citation	Proceedings of the 28th Chinese Control and Decision Conference, CCDC 2016, 2016, pp. 1605 - 1610	en_US
dc.identifier.isbn	9781467397148	en_US
dc.identifier.uri	http://hdl.handle.net/10453/120130
dc.description.abstract	© 2016 IEEE. In this paper, the tracking problem for a rigid spacecraft with input saturation is investigated. Due to the complexity of the dynamic of a rigid spacecraft, a hierarchical control scheme, dividing the model of a rigid spacecraft into translational level and attitude level, is designed. The controllers for translational dynamic and attitude dynamic of the six-freedom-degrees spacecraft are successively proposed respectively. The input saturation is also considered in designing the two controllers. For translational level, a kind of special saturation function is employed to get the controller whose amplitude is constrained. For the attitude dynamic, a new adaptive quaternion-based control scheme is proposed to withstand the effect of bounded uncertain items and input saturation. Finally, simulation results are provided to show the effectiveness of the proposed scheme.	en_US
dc.relation.ispartof	Proceedings of the 28th Chinese Control and Decision Conference, CCDC 2016	en_US
dc.relation.isbasedon	10.1109/CCDC.2016.7531240	en_US
dc.rights	info:eu-repo/semantics/closedAccess
dc.title	Adaptive tracking algorithm for a rigid spacecraft with input saturation	en_US
dc.type	Conference Proceeding
utslib.for	0906 Electrical and Electronic Engineering	en_US
pubs.embargo.period	Not known	en_US
pubs.organisational-group	/University of Technology Sydney
pubs.organisational-group	/University of Technology Sydney/Faculty of Engineering and Information Technology
pubs.organisational-group	/University of Technology Sydney/Faculty of Engineering and Information Technology/School of Biomedical Engineering
pubs.organisational-group	/University of Technology Sydney/Strength - CHT - Health Technologies
utslib.copyright.status	closed_access	*
pubs.publication-status	Published	en_US

Abstract:

© 2016 IEEE. In this paper, the tracking problem for a rigid spacecraft with input saturation is investigated. Due to the complexity of the dynamic of a rigid spacecraft, a hierarchical control scheme, dividing the model of a rigid spacecraft into translational level and attitude level, is designed. The controllers for translational dynamic and attitude dynamic of the six-freedom-degrees spacecraft are successively proposed respectively. The input saturation is also considered in designing the two controllers. For translational level, a kind of special saturation function is employed to get the controller whose amplitude is constrained. For the attitude dynamic, a new adaptive quaternion-based control scheme is proposed to withstand the effect of bounded uncertain items and input saturation. Finally, simulation results are provided to show the effectiveness of the proposed scheme.

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http://hdl.handle.net/10453/120130