Optimal sliding mode controllers for attitude tracking of spacecraft

Pukdeboon, C. and Zinober, A.S.I. (2009) Optimal sliding mode controllers for attitude tracking of spacecraft. In: Proceedings of the IEEE Multi-Conference on Systems and Control. IEEE Multi-Conference on Systems and Control, July 8-10, 2009, Saint Petersburg, Russia. Institute of Electrical and Electronics Engineers , pp. 1708-1713. ISBN 978-1-4244-4601-8

Abstract

Metadata

Authors/Creators:
  • Pukdeboon, C.
  • Zinober, A.S.I. (A.Zinober@sheffield.ac.uk)
Copyright, Publisher and Additional Information: © Copyright 2009 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: Lyapunov methods; Riccati equations; aircraft control; attitude control; matrix algebra; optimal control; tracking; variable structure systems
Dates:
  • Published: 2009
Institution: The University of Sheffield
Academic Units: The University of Sheffield > Faculty of Science (Sheffield) > School of Mathematics and Statistics (Sheffield)
Depositing User: Mrs Megan Hobbs
Date Deposited: 12 Apr 2010 09:08
Last Modified: 17 Nov 2015 04:08
Published Version: http://dx.doi.org/10.1109/CCA.2009.5281130
Status: Published
Publisher: Institute of Electrical and Electronics Engineers
Identification Number: https://doi.org/10.1109/CCA.2009.5281130

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