Gust response modeling and alleviation scheme design for an elastic aircraft

Author:

Wu ZhiGang,Chen Lei,Yang Chao,Tang ChangHong

Publisher

Springer Science and Business Media LLC

Subject

General Engineering,General Materials Science

Reference18 articles.

1. Wen C Y. Modern Flight Control. Beijing: BUAA University Press, 2004. 181–192

2. Karpel M, Moulin B, Chen P C. Dynamic response of aeroservoelastic systems to gust excitation. J Aircraft, 2005, 42: 1264–1272

3. Wu Z G, Yang C. Investigation on active flutter suppression and gust alleviation for an active aeroelastic wing. J Mech Strength, 2003, 25: 32–35

4. Chen L, Wu Z G, Yang C, et al. Active control and wind tunnel verification of multi-control surfaces wing for gust alleviation (in Chinese). Acta Aeronautica et Astronautica Sinica, 2009, 30: 2250–2256

5. ZAERO. Software package. ZONA Technology Inc., Scottsdale, 2008

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