Sliding mode robust control of supersonic three degrees-of-freedom airfoils-Reference-Cited by-同舟云学术

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Sliding mode robust control of supersonic three degrees-of-freedom airfoils

Published:2010-04 Issue:2 Volume:8 Page:279-288
ISSN:1598-6446
Container-title:International Journal of Control, Automation and Systems
language:en
Short-container-title:Int. J. Control Autom. Syst.

Author:

Lee Bok-Hee,Choo Jeong-hwan,Na Sungsoo,Marzocca Piergiovanni,Librescu Liviu

Publisher

Springer Science and Business Media LLC

Subject

Computer Science Applications,Control and Systems Engineering

Link

http://link.springer.com/content/pdf/10.1007/s12555-010-0214-8.pdf

Reference16 articles.

1. L. Librescu and P. Marzocca, “Advances in the linear/non-linear control of aeroelastic structural systems,” Acta Mechanica, vol. 178, no. 3–4, pp. 147–186. 2005.

2. V. Mukhopadhyay, “Flutter suppression control law design and testing for the active flexible wing,” Journal of Aircraft, vol. 32, pp. 45–51, 1995.

3. V. Mukhopadhyay, “Benchmark active control technology,” Journal of Guidance, Control, and Dynamics, part I, vol. 23, pp. 913–960, part II, vol. 23, pp. 1093–1139, part III, vol. 24, pp. 146–192, 2000–2001.

4. S. Na, L. Librescu, P. Marzocca, C. Rubillo, G. Yoon, and K. Bong, “Robust aeroelastic control of two-dimensional supersonic flapped wing systems,” Acta Mechanica, vol. 192, no. 1–4, pp. 37–47, 2007.

5. S. Na, L. Librescu, P. Marzocca, G. Yoon, and C. Rubillo, “Robust aeroelastic control of 2-d supersonic flapped lifting surfaces,” Proc. of the 47th AIAA/ASME/ASCE/ASC Structures, Structural Dynamics, and Materials Conference, AIAA-2006-1836, May 2006.

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