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Mathematical Problems in Engineering
Volume 2015 (2015), Article ID 187924, 9 pages
http://dx.doi.org/10.1155/2015/187924
Research Article

Terminal Sliding Mode Control for Attitude Tracking of Spacecraft Based on Rotation Matrix

Center for Control Theory and Guidance Technology, Harbin Institute of Technology, Harbin 150001, China

Received 6 June 2014; Revised 14 August 2014; Accepted 1 September 2014

Academic Editor: Sabri Arik

Copyright © 2015 Yong Guo et al. 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.

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