Application of Decaying Boundary Layer and Switching Function Method Thorough Error Feedback for Sliding Mode Control on Spacecraft’s Attitude

Hassrizal, H.B. and Rossiter, J.A. orcid.org/0000-0002-1336-0633 (2017) Application of Decaying Boundary Layer and Switching Function Method Thorough Error Feedback for Sliding Mode Control on Spacecraft’s Attitude. In: 2017 25th Mediterranean Conference on Control and Automation (MED). 25th Mediterranean Conference on Control and Automation 2017, 03/07/2017-06/07/2017, Valletta, Malta. Institute of Electrical and Electronics Engineers , pp. 1250-1256. ISBN 978-1-5090-4533-4

Abstract

Metadata

Authors/Creators:
Copyright, Publisher and Additional Information: © 2017 IEEE. This is an author produced version of a paper subsequently published in 2017 25th Mediterranean Conference on Control and Automation (MED). Uploaded in accordance with the publisher's self-archiving policy.
Dates:
  • Accepted: 1 March 2017
  • Published (online): 20 July 2017
  • Published: 20 July 2017
Institution: The University of Sheffield
Academic Units: The University of Sheffield > Faculty of Engineering (Sheffield) > Department of Automatic Control and Systems Engineering (Sheffield)
Depositing User: Symplectic Sheffield
Date Deposited: 10 May 2017 10:28
Last Modified: 11 Sep 2017 11:52
Published Version: https://doi.org/10.1109/MED.2017.7984289
Status: Published
Publisher: Institute of Electrical and Electronics Engineers
Refereed: Yes
Identification Number: https://doi.org/10.1109/MED.2017.7984289

Share / Export

Statistics