Aeroelastic Response of Flapped-Wing Systems Using Robust Estimation Control Methodology-Reference-Cited by-同舟云学术

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Aeroelastic Response of Flapped-Wing Systems Using Robust Estimation Control Methodology

Published:2006-01 Issue:1 Volume:29 Page:199-202
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Na Sungsoo¹,Librescu Liviu²,Kim Myung-Hyun³,Jeong In-Joo¹,Marzocca Pier⁴

Affiliation:

1. Korea University, Seoul 136-701, Republic of Korea

2. Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24061

3. Pusan National University, Pusan 609-735, Republic of Korea

4. Clarkson University, Potsdam, New York 13699-5725

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.15015

Reference15 articles.

1. Aeroelastic response of 2-D lifting surfaces to gust and arbitrary explosive loading signatures

2. Active aeroelastic control of 2-D wing-flap systems operating in an incompressible flowfield and impacted by a blast pulse

3. Flutter suppression control law design and testing for the active flexible wing

4. Historical Perspective on Analysis and Control of Aeroelastic Responses

5. Feedback control of flexible systems

Cited by 10 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. Discussion of “Robust Aeroelastic Control of a Thin-Walled Wing Structure with Model Uncertainty” by Jeonghwan Choo, Gwonchan Yoon, Ji-Seok Song, Taeyun Kwon, Sungsoo Na, and Zhanming Qin;Journal of Aerospace Engineering;2014-01

2. Discussion on “Active aeroelastic control of 2-D wing-flap systems operating in an incompressible flowfield and impacted by a blast pulse” by Librescu et al., Journal of Sound and Vibration 283 (3–5) (2005) 685–706;Journal of Sound and Vibration;2013-06

3. Robust aeroelastic instability suppression of an advanced wing with model uncertainty in subsonic compressible flow field;Aerospace Science and Technology;2013-03

4. Robust Aeroelastic Control of a Thin-Walled Wing Structure with Model Uncertainty;Journal of Aerospace Engineering;2012-04

5. Dynamic aeroelastic response and active control of composite thin-walled beam structures in compressible flow;Journal of Sound and Vibration;2011-10

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