Performance Enhancement of Gust Load Alleviation Systems for Flexible Aircraft using H∞Optimal Control with Preview-Reference-Cited by-同舟云学术

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Performance Enhancement of Gust Load Alleviation Systems for Flexible Aircraft using H∞Optimal Control with Preview

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

Khalil Ahmed¹,Fezans Nicolas¹

Affiliation:

1. German Aerospace Center (DLR)

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2019-0822

Reference38 articles.

1. Hargrove, W. J. “The C-5A active lift distribution control system,” Tech. Rep. 76N31148, NASA, August 1976.

2. 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, DFRC-E-DAA-TN4736, NASA, April 2012.

3. Hoffmann, G. “Stabilisierung, Böenkompensation und Schwingungsdämpfung am elastischen beweglichen Flugzeugmodell im Windkanal,” Tech. Rep. DLR-FB 76-44, DFVLR (now part of DLR), 1976.

Cited by 3 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. On the Aeroelasticity of a Cantilever Wing Equipped with the Spanwise Morphing Trailing Edge Concept;Aerospace;2023-09-15

2. A multi-channel $$\varvec{H}_\infty $$ preview control approach to load alleviation design for flexible aircraft;CEAS Aeronautical Journal;2021-04

3. Gust load alleviation for a long-range aircraft with and without anticipation;CEAS Aeronautical Journal;2019-01-29

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