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Mathematical Problems in Engineering
Volume 2014, Article ID 312494, 11 pages
http://dx.doi.org/10.1155/2014/312494
Research Article

Adaptive-Gain Second-Order Sliding Mode Control of Attitude Tracking of Flexible Spacecraft

Nonlinear Dynamic Analysis Research Center, Department of Mathematics, Faculty of Applied Science, King Mongkut’s University of Technology North Bangkok, Bangkok 10800, Thailand

Received 15 March 2014; Accepted 11 April 2014; Published 21 May 2014

Academic Editor: Her-Terng Yau

Copyright © 2014 Chutiphon Pukdeboon. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.

How to Cite this Article

Chutiphon Pukdeboon, “Adaptive-Gain Second-Order Sliding Mode Control of Attitude Tracking of Flexible Spacecraft,” Mathematical Problems in Engineering, vol. 2014, Article ID 312494, 11 pages, 2014. https://doi.org/10.1155/2014/312494.