Health structure monitoring for the design of an innovative UAS fixed wing through inverse finite element method (iFEM)-Reference-Cited by-同舟云学术

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Health structure monitoring for the design of an innovative UAS fixed wing through inverse finite element method (iFEM)

Published:2017-10 Issue: Volume:69 Page:439-448
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Papa Umberto^ORCID,Russo Salvatore,Lamboglia Angelo,Del Core Giuseppe,Iannuzzo Generoso

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference17 articles.

1. Structural shape identification from experimental strains using a modal transformation technique;Bogert,2003

2. CEA-06-250UW-350 Micro-Measurements. Datasheet, spec. general-purpose strain gauge, Document No.: 11312, Revision: 25 Aug 2015.

3. A mini unmanned aerial vehicle (UAV): system overview and image acquisition;Eisenbess,2004

4. An inverse finite element method for beam shape sensing: theoretical frame work and experimental validation;Gherlone;Smart Mater. Struct.,2014

5. Advanced Engineering Mathematics;Kreyszig,1993

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