Deformation Control of Highly Flexible Aircraft in Trimmed Flight and Gust Encounter

Author:

Yagil Leeran1,Raveh Daniella E.1,Idan Moshe1

Affiliation:

1. Technion—Israel Institute of Technology, 3200003 Haifa, Israel

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

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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