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International Journal of Aerospace Engineering
Volume 2016 (2016), Article ID 1395952, 14 pages
http://dx.doi.org/10.1155/2016/1395952
Research Article

Inverse Optimal Attitude Stabilization of Flexible Spacecraft with Actuator Saturation

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

Received 28 December 2015; Accepted 28 March 2016

Academic Editor: Kenneth M. Sobel

Copyright © 2016 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.

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