A reduced-order-model-based multiple-in multiple-out gust alleviation control law design method in transonic flow-Reference-Cited by-同舟云学术

A reduced-order-model-based multiple-in multiple-out gust alleviation control law design method in transonic flow

Published:2013-12-07 Issue:2 Volume:57 Page:368-378
ISSN:1674-7321
Container-title:Science China Technological Sciences
language:en
Short-container-title:Sci. China Technol. Sci.

Author:

Chen Gang,Wang Xian,Li YueMing

Publisher

Springer Science and Business Media LLC

Subject

General Engineering,General Materials Science

Link

http://link.springer.com/content/pdf/10.1007/s11431-013-5416-x.pdf

Reference43 articles.

1. Code of Federal Regulations, Aeronautics and Space, Part 25.341. Gust and turbulence loads. Maryland: Office of Federal Register, National Archives and Records Administration, January 2003

2. Robert C, Michael J A, Ryan P D, et al. Fight test of the f/a-18 active aeroelastic wing airplane. NASA/TM-2005-213664, 2005.

3. Simpson J, Suleman A, Cooper J. Review of European research project active aeroelastic aircraft structures. In: IFASD Conference, Munich, 2005

4. Gur O, Bhatia M, Schetz J, et al. Design optimization of a truss-braced-wing transonic transport aircraft. J Aircraft, 2010, 47(6): 1907–1917

5. Moulin B, Karpel M. Gust loads alleviation using special control surfaces. J Aircraft, 2007, 44(1): 17–24

Cited by 13 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. A data-driven online prediction method for surface-deformed liquid level in vessels under ocean conditions;Nuclear Engineering and Design;2023-12

2. Recent advances in precision measurement & pointing control of spacecraft;Chinese Journal of Aeronautics;2021-10

3. Gust loads on aircraft;The Aeronautical Journal;2019-06-25

4. Ground Flutter Simulation Test Based on Reduced Order Modeling of Aerodynamics by CFD/CSD Coupling Method;International Journal of Applied Mechanics;2019-01

5. Unsteady Aerodynamic Modeling Based on POD-ARX;International Journal of Aerospace Engineering;2018-09-20