Fuzzy dynamic characteristic model based attitude control of hypersonic vehicle in gliding phase-Reference-Cited by-同舟云学术

Fuzzy dynamic characteristic model based attitude control of hypersonic vehicle in gliding phase

Published:2011-03 Issue:3 Volume:54 Page:448-459
ISSN:1674-733X
Container-title:Science China Information Sciences
language:en
Short-container-title:Sci. China Inf. Sci.

Author:

Luo Xiong,Li Jiang

Publisher

Springer Science and Business Media LLC

Subject

General Computer Science

Link

http://link.springer.com/content/pdf/10.1007/s11432-011-4193-z.pdf

Reference11 articles.

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2. Liu Y B. Research on modeling and advanced flight control theories for hypersonic vehicle (in Chinese). Ph.D. thesis, Nanjing: Nanjing University of Aeronautics and Astronautics, 2007

3. Lu P, Hanson J M. Entry guidance for the X-33 vehicle. J Spacecraft Rockets, 1998, 35: 342–349

4. Wu H X, Liu Y W, Liu Z H, et al. Characteristic modeling and the control of flexible structure. Sci China Ser F-Inf Sci, 2001, 44: 278–291

5. Yang J C, Hu J, Ni M L. Adaptive guidance law design based on characteristic model for reentry vehicles. Sci China Ser F-Inf Sci, 2008, 51: 2005–2021

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