Aeroelastic Identification of Flying UAVs by Output-Only Data with Applications on Vibrations Passive Control-Reference-Cited by-同舟云学术

Aeroelastic Identification of Flying UAVs by Output-Only Data with Applications on Vibrations Passive Control

Published:2010-04-12 Issue: Volume: Page:
ISSN:
Container-title:51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference<BR> 18th AIAA/ASME/AHS Adaptive Structures Conference<BR> 12th
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Author:

Mastroddi Franco,Coppotelli Giuliano

Publisher

American Institute of Aeronautics and Astronautics

Reference34 articles.

1. 1Coppotelli, G., Mastroddi, F. “Output-Only Analysis on Aeroelastic Systems,” proceedings XVIII Congresso Nazionale AIDAA, Volterra, 19-22 Settembre, 2005.

2. 2Coppotelli, G., Di Vincenzo, F.G., Mastroddi, F. “Aeroelastic System Identification of a Flying UAV in Operative Conditions," International Forum on Aeroelasticity and Structural Dynamics, Seattle, WA, 21-25June, 2009.

3. 3Kim, T. “New System Identification for Coupled Fluid-Structure Systems: "Aerodynamics is Aeroelasticity Minus Structure"” International Forum on Aeroelasticity and Structural Dynamics, Seattle, WA, 21-25June, 2009.

4. Aerothermoelastic Stability of Composite Aerovehicle Wings Subjected to Heat Inputs

5. 5Thuruthimattam, B. J., Friedmann, P. P., McNamara, J. J., and Powell, K. “Modeling Approaches to Hypersonic Aerothermoelasticity with Applications to Reusable Launch Vehicles,” 44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference, April 7th - 10th 2003. 2003, AIAA-2003-1967.

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