Wing Shape Sensing from Measured Strain
Author:
Affiliation:
1. NASA Armstrong Flight Research Center, Edwards, California 93523-0273
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J053986
Reference14 articles.
1. NollT. E.BrownJ. M.Perez-DavisM. E.IshamaelS. D.TiffanyG. C.GaierM. “Investigation of the Helios Prototype Aircraft Mishap, Volume I Mishap Report,” NASA, Washington, D.C., 2004, https://www.nasa.gov/pdf/64317main_helios.pdf.
2. LizotteA. M.LokosW. A. “Deflection-Based Structural Loads Estimation from the Active Aeroelastic Wing F/A-18 Aircraft,” NASA TM-2005-212871, 2005.
3. Dynamic strain measurements by fibre Bragg grating sensor
4. KoW. L.RichardsW. L.TranV. T. “Displacement Theories for In-Flight Deformed Shape Predictions of Aerospace Structures,” NASA TP-2007-214612, 2007.
5. Estimation of dynamic structural displacements using fiber Bragg grating strain sensors
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