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Abstract and Applied Analysis
Volume 2014 (2014), Article ID 302982, 15 pages
http://dx.doi.org/10.1155/2014/302982
Research Article

Finite-Time Control for Attitude Tracking Maneuver of Rigid Satellite

1Department of Control Science and Engineering, Harbin Institute of Technology, Harbin 150001, China
2College of Engineering, Bohai University, Jinzhou 121000, China
3Department of Engineering, Faculty of Engineering and Science, The University of Agder, 4898 Grimstad, Norway

Received 7 November 2013; Accepted 8 January 2014; Published 26 February 2014

Academic Editor: Junmin Wang

Copyright © 2014 Mingyi Huo 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.

How to Cite this Article

Mingyi Huo, Xing Huo, Hamid Reza Karimi, and Jianfei Ni, “Finite-Time Control for Attitude Tracking Maneuver of Rigid Satellite,” Abstract and Applied Analysis, vol. 2014, Article ID 302982, 15 pages, 2014. doi:10.1155/2014/302982