Localizations and force reconstruction of low-velocity impact in a composite panel using optical fiber sensors

Author:

Park Chan Yik1,Kim Jong Heon1,Jun Seung-Moon1,Kim Chun-Gon2

Affiliation:

1. a Agency for Defense Development , Daejeon , Korea

2. b Department of Aerospace Engineering , Korea Advanced Institute of Science and Technology , Daejeon , Korea

Publisher

Informa UK Limited

Subject

Mechanical Engineering,Mechanics of Materials,Ceramics and Composites

Reference15 articles.

1. Zaloga SJ, Rockwell D, Finnegan P. World unmanned aerial vehicle systems, market profile and forecast. 2011 ed. Fairfax (VA): Teal Group Co; 2011.

2. DeGarmo M, Nelson GM. Prospective unmanned aerial vehicle operations in the future national airspace system. In: Proceedings of the AIAA 4th Aviation Technology, Integration and Operations Forum – AIAA 2004-6243; 2004; Chicago, IL.

3. Neubauer M, Gunteher G, Fullhas K. Structural design aspects and criteria for military UAV. In: Proceedings of the UAV Design Processes and Criteria – RTO-MP-AVT 145; 2007; Florence, Italy.

4. Kosmatka JB, Oliver J. Development of an in-flight structural health monitoring system for composite unmanned aircraft. In: Proceedings of the 47th AISS/ASME/ASCE/AHS/ASV Structures, Structural Dynamics and Materials Conference – AIAA 2006-1881; 2006; Newport, Rhode Island.

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