Second-order terminal sliding mode control for hypersonic vehicle in cruising flight with sliding mode disturbance observer-Reference-Cited by-同舟云学术

Second-order terminal sliding mode control for hypersonic vehicle in cruising flight with sliding mode disturbance observer

Published:2013-05 Issue:2 Volume:11 Page:299-305
ISSN:1672-6340
Container-title:Journal of Control Theory and Applications
language:en
Short-container-title:J. Control Theory Appl.

Author:

Zhang Ruimin,Sun Changyin,Zhang Jingmei,Zhou Yingjiang

Publisher

Springer Science and Business Media LLC

Subject

Computer Science Applications,Hardware and Architecture,Control and Systems Engineering

Link

http://link.springer.com/content/pdf/10.1007/s11768-013-1164-5.pdf

Reference17 articles.

1. D. Gao, Z. Sun, X. Luo, et al. Fuzzy adaptive control for hypersonic vehicle via backstepping method. Control Theory & Application, 2008, 25(5): 805–810 (in Chinese).

2. J. Chen, C. Pan. Dynamic surface backstepping control design for one hypersonic vehicle. Proceedings of International Conference on Mechatronics and Automation. Changchun: IEEE, 2009: 4770–4774.

3. H. Xu, M. Mirmirani, P. A. Ioannou. Robust neural adaptive control of a hypersonic aircraft. AIAA Guidance, Navigation and Control Conference and Exhibit. Austin, Texas: AIAA, 2003: 1–8.

4. B. Xu, D. Gao, S. Wang. Adaptive neural control based on HGO for hypersonic flight vehicles. Science China Information Sciences, 2011, 54(3): 511–520.

5. B. Durmaz, M. K. Ozgoren, M. U. Salamcik. Sliding mode control for nonlinear systems with adaptive sliding surface. Transactions of the Institute of Measurement and Control, 2012, 34(1): 1–35.

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