By Topic

The design and implementation of micro flapping wing air vehicle

Sign In

Cookies must be enabled to login.After enabling cookies , please use refresh or reload or ctrl+f5 on the browser for the login options.

Formats Non-Member Member
$33 $13
Learn how you can qualify for the best price for this item!
Become an IEEE Member or Subscribe to
IEEE Xplore for exclusive pricing!
close button

puzzle piece

IEEE membership options for an individual and IEEE Xplore subscriptions for an organization offer the most affordable access to essential journal articles, conference papers, standards, eBooks, and eLearning courses.

Learn more about:

IEEE membership

IEEE Xplore subscriptions

2 Author(s)
Jiang Zhe ; The Key Laboratory of System and Control, Chinese Academy of Sciences, Beijing 100190, P.R. China ; Su Gang

This paper studies the system design of micro flapping wing air vehicle, and describes the mechanical design and controller design of micro flapping wing air vehicle. X-airfoil is selected to design the wing of air vehicle. The combination of cork and carbon fiber is used to design air vehicle body. The system for the aerodynamic testing of micro flapping wings air vehicle is designed to verify the thrust and lift obtained from the system applied for the micro flapping wings air vehicle. The indicators of flight are given by flight test.

Published in:

Control Conference (CCC), 2012 31st Chinese

Date of Conference:

25-27 July 2012