Aeroelastic Modeling and Control of an Experimental Flexible Wing-Reference-Cited by-同舟云学术

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Aeroelastic Modeling and Control of an Experimental Flexible Wing

Published:2019-01-06 Issue: Volume: Page:
ISSN:
Container-title:AIAA Scitech 2019 Forum
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Author:

Pusch Manuel¹,Ossmann Daniel¹,Dillinger Johannes¹,Kier Thiemo M.¹,Tang Martin¹,Lübker Jannis¹

Affiliation:

1. German Aerospace Center (DLR)

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2019-0131

Reference15 articles.

1. Regan, C. D., and Jutte, C. V. “Survey of Applications of Active Control Technology for Gust Alleviation and New Challenges for Lighter-weight Aircraft,” Tech. Rep. NASA/TM-2012-216008, NASA, 2012.

2. Wildschek, A. “An adaptive feed-forward controller for active wing bending vibration alleviation on large transport aircraft,” Ph.D. thesis,Technische Universität München, 2009.

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2. Aircraft feedback gust load control design and experimental wing bench validation;AIAA SCITECH 2022 Forum;2022-01-03

3. Identification and assessment of a nonlinear dynamic actuator model for controlling an experimental flexible wing;CEAS Aeronautical Journal;2021-04

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5. Partial Pole Placement using Static Output Feedback;IFAC-PapersOnLine;2020

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