Paper Title:
Structural Design and Testing of Small Ultralight Solar-Powered Unmanned Aerial Vehicle
  Abstract

Lightweight design was carried out in order to meeting the requirement of long endurance. Structure form was designed based on loading characteristics. Rationality of structure form was verified by finite element method and static tests, which proved deformation of wing measuring up mechanical properties of cell panel. Finite element modal analysis was performed. Then mode test was carried to correcting analysis results. Low order modes by testing are coincided with that computed in finite element method (FEM).

  Info
Periodical
Advanced Materials Research (Volumes 317-319)
Chapter
Materials and Its Applications
Edited by
Xin Chen
Pages
227-230
DOI
10.4028/www.scientific.net/AMR.317-319.227
Citation
W. Zhang, L. J. Yao, X. Y. Tong, "Structural Design and Testing of Small Ultralight Solar-Powered Unmanned Aerial Vehicle", Advanced Materials Research, Vols. 317-319, pp. 227-230, 2011
Online since
August 2011
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Price
$32.00
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