4D metrology of flapping-wing micro air vehicle based on fringe projection

Qican Zhang*, Lei Huang, Yao Wei Chin, Gih Keong Lau, Anand Asundi

*Corresponding author for this work

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

5 Scopus citations

Abstract

Inspired by dominant flight of the natural flyers and driven by civilian and military purposes, micro air vehicle (MAV) has been developed so far by passive wing control but still pales in aerodynamic performance. Better understanding of flapping wing flight mechanism is eager to improve MAV's flight performance. In this paper, a simple and effective 4D metrology technique to measure full-field deformation of flapping membrane wing is presented. Based on fringe projection and 3D Fourier analysis, the fast and complex dynamic deformation, including wing rotation and wing stroke, of a flapping wing during its flight can be accurately reconstructed from the deformed fringe patterns recorded by a highspeed camera. An experiment was carried on a flapping-wing MAV with 5-cm span membrane wing beating at 30 Hz, and the results show that this method is effective and will be useful to the aerodynamicist or micro aircraft designer for visualizing high-speed complex wing deformation and consequently aid the design of flapping wing mechanism to enhanced aerodynamic performance.

Original languageEnglish
Title of host publicationInternational Conference on Optics in Precision Engineering and Nanotechnology, icOPEN 2013
DOIs
StatePublished - 2013
EventInternational Conference on Optics in Precision Engineering and Nanotechnology, icOPEN 2013 - Singapore, Singapore
Duration: 9 Apr 201311 Apr 2013

Publication series

NameProceedings of SPIE - The International Society for Optical Engineering
Volume8769
ISSN (Print)0277-786X
ISSN (Electronic)1996-756X

Conference

ConferenceInternational Conference on Optics in Precision Engineering and Nanotechnology, icOPEN 2013
Country/TerritorySingapore
CitySingapore
Period9/04/1311/04/13

Keywords

  • 4D metrology
  • Deformation measurement
  • Flapping wing
  • Fourier analysis
  • Fringe projection
  • Micro air vehicle

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