Table of Contents
ISRN Aerospace Engineering
Volume 2014, Article ID 163870, 13 pages
http://dx.doi.org/10.1155/2014/163870
Research Article

Attitude and Vibration Control of Flexible Spacecraft Using Singular Perturbation Approach

Space Research Institute, Tehran 15875-1774, Iran

Received 4 December 2013; Accepted 16 January 2014; Published 29 May 2014

Academic Editors: Z. Qin, I. Taymaz, and J. Yao

Copyright © 2014 Morteza Shahravi and Milad Azimi. 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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