DocumentCode
2595343
Title
A flapping-wing micro air vehicle with interchangeable parts for system integration studies
Author
Sahai, Ranjana ; Galloway, Kevin C. ; Karpelson, Michael ; Wood, Robert J.
Author_Institution
Harvard Microrobotics Lab., Harvard Univ., Cambridge, MA, USA
fYear
2012
fDate
7-12 Oct. 2012
Firstpage
501
Lastpage
506
Abstract
This paper describes the development of a unique flapping-wing micro air vehicle (FWMAV) whose major components, i.e. the motor, transmission mechanisms, and wings, are rapidly interchangeable. When coupled with a test stand that includes a 6-axis force sensor, encoder, power-recording capabilities, and high speed video, the result is a highly versatile experimental platform on which system integration studies can be conducted. This paper provides a detailed description of the design and fabrication of this FWMAV whose interchangeability of parts is mostly accomplished through a novel system of tabs, slots, and retaining rods. Results of a study on energy saving elements in the transmission mechanism as well as an exploration of this effect for different wing sizes are also presented. Finally, the implications of interchangeable parts on the creation of customizable flyers are discussed.
Keywords
actuators; aerospace components; aircraft; force sensors; video signal processing; 6-axis force sensor; FWMAV; customizable flyers; encoder; energy saving elements; high speed video; interchangeable parts; motor; power-recording capabilities; retaining rod system; system integration studies; transmission mechanisms; unique flapping-wing micro air vehicle; versatile experimental platform; Actuators; Couplers; Fabrication; Gears; Joints; Rubber; Shafts;
fLanguage
English
Publisher
ieee
Conference_Titel
Intelligent Robots and Systems (IROS), 2012 IEEE/RSJ International Conference on
Conference_Location
Vilamoura
ISSN
2153-0858
Print_ISBN
978-1-4673-1737-5
Type
conf
DOI
10.1109/IROS.2012.6386058
Filename
6386058
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