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Quasi-continuous higher-order sliding-mode controllers for spacecraft-attitude-tracking manoeuvres

Pukdeboon, C., Zinober, A.S.I. and Thein, M.W. (2010) Quasi-continuous higher-order sliding-mode controllers for spacecraft-attitude-tracking manoeuvres. IEEE Transactions on Industrial Electronics, 57 (4). pp. 1436-1444. ISSN 0278-0046

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Abstract

This paper studies higher order sliding-modecontrol laws to deal with some spacecraft-attitude-tracking problems. Quasi-continuous second- and third-order sliding controllers and differentiators are applied to quaternion-based spacecraftattitude- tracking maneuvers. A class of linear sliding manifolds is selected as a function of angular velocities and quaternion errors. The second method of Lyapunov is used to show that tracking is achieved globally. An example of multiaxial attitude-tracking maneuvers is presented, and simulation results are included to verify and compare the practical usefulness of the various controllers.

Item Type: Article
Copyright, Publisher and Additional Information: © Copyright 2010 IEEE. Personal use of this material is permitted. However, permission to reprint/republish this material for advertising or promotional purposes or for creating new collective works for resale or redistribution to servers or lists, or to reuse any copyrighted component of this work in other works must be obtained from the IEEE.
Keywords: Higher order sliding-mode control (HOSMC), sliding-mode differentiators, spacecraft control
Academic Units: The University of Sheffield > Faculty of Science (Sheffield) > School of Mathematics and Statistics (Sheffield)
Depositing User: Mrs Megan Hobbs
Date Deposited: 29 Mar 2010 11:04
Last Modified: 08 Feb 2013 17:00
Published Version: http://dx.doi.org/10.1109/TIE.2009.2030215
Status: Published
Publisher: Institute of Electrical and Electronics Engineers
Identification Number: 10.1109/TIE.2009.2030215
URI: http://eprints.whiterose.ac.uk/id/eprint/10727

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