Deformation Control of Highly Flexible Aircraft in Trimmed Flight and Gust Encounter
Author:
Affiliation:
1. Technion—Israel Institute of Technology, 3200003 Haifa, Israel
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C034353
Reference20 articles.
1. NollT. E.BrownJ. M.Perez-DavisM. E.IshmaelS. D.TiffanyG. C.GaierM. “Investigation of the Helios Prototype Aircraft Mishap,” Vol. I, NASA Mishap Report, Jan. 2004, http://www.nasa.gov/pdf/64317main_helios.pdf [retrieved Sept. 2014].
2. Flight Dynamics of Highly Flexible Flying Wings
3. Dynamic Response of Highly Flexible Flying Wings
4. Nonlinear Modal Aeroservoelastic Analysis Framework for Flexible Aircraft
5. An active flexible wing multi-disciplinary design optimization method
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