Boundary control of flexible aircraft wings for vibration suppression-Reference-Cited by-同舟云学术

Boundary control of flexible aircraft wings for vibration suppression

Published:2018-03-22 Issue:11 Volume:92 Page:2499-2508
ISSN:0020-7179
Container-title:International Journal of Control
language:en
Short-container-title:International Journal of Control

Author:

He Xiuyu¹,He Wei¹^ORCID,Chen Yunan¹,Mu XinXing¹,Yu Yao¹,Sun Changyin²

Affiliation:

1. School of Automation and Electrical Engineering and Key Laboratory of Knowledge Automation for Industrial Processes, Ministry of Education, University of Science and Technology Beijing, Beijing, China

2. School of Automation, Southeast University , Nanjing, China

Funder

National Key Research and Development Program of China

National Natural Science Foundation of China

Newton Advanced Fellowship from The Royal Society, UK

Beijing Natural Science Foundation

Fundamental Research Funds for the China Central Universities USTB

Publisher

Informa UK Limited

Subject

Computer Science Applications,Control and Systems Engineering

Link

https://www.tandfonline.com/doi/pdf/10.1080/00207179.2018.1442025

Reference26 articles.

1. Aerodynamic Coefficients and Deformation Measurements on Flexible Micro Air Vehicle Wings

2. Adaptive attitude and position control of an insect-like flapping wing air vehicle

3. Adaptive boundary control of store induced oscillations in a flexible aircraft wing

4. Optimal boundary control with critical penalization for a PDE model of fluid–solid interactions

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