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International Journal of Aerospace Engineering
Volume 2018, Article ID 1427487, 12 pages
https://doi.org/10.1155/2018/1427487
Research Article

Robust Adaptive Output Feedback Control for a Guided Spinning Rocket

1Beijing Institute of Technology, Beijing 100081, China
2Key Laboratory of Dynamics and Control of Flight Vehicle, Ministry of Education, Beijing 100081, China

Correspondence should be addressed to Liangyu Zhao; nc.ude.tib@yloahz

Received 25 October 2017; Revised 5 April 2018; Accepted 18 April 2018; Published 14 May 2018

Academic Editor: Kenneth M. Sobel

Copyright © 2018 Zhongjiao Shi 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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