DocumentCode
164129
Title
Development of multi-tentacle micro air vehicle
Author
Joe Woong Yeol ; Chun-Han Lin
Author_Institution
Dept. of Aerosp. & Mech. Eng., Embry-Riddle Aeronaut. Univ., Prescott, AZ, USA
fYear
2014
fDate
27-30 May 2014
Firstpage
815
Lastpage
820
Abstract
We introduce a developmental stage of multi-tentacle MAV (micro air vehicle) platform. It is based on a four rotary wing aerial platform such as a quadrotor system and three of 4 DOF (degree of freedom) tentacles attached at the bottom of it. Unlikely mobile manipulating research which focuses more on the stability and control of manipulators and floating platform, a multi-tentacle system presented in this paper is intended to suggest a new paradigm of small scaled aerial robotics research and to show the proof of concept of them by experiment. Newly integrated and developed multi-tentacle aerial vehicle can have extended locomotions compared currently existing flying-only vehicles such as vertically and upside down perching capability, inclined or rough surface landing capability, and object pickup and release. Furthermore, control of a particular motion of tentacles adds propulsive force for taking off as birds or flying animals do.
Keywords
autonomous aerial vehicles; biomimetics; helicopters; microrobots; mobile robots; telerobotics; 4 DOF tentacles; flying-only vehicles; four rotary wing aerial platform; inclined surface landing capability; multitentacle microair vehicle; object pickup capability; object release capability; propulsive force; quadrotor system; rough surface landing capability; small scaled aerial robotics; upside down perching capability; vertical perching capability; Birds; Educational institutions; Manipulators; Mobile communication; Vehicles; aerial robot; micro air vehicles; multi-tentacles;
fLanguage
English
Publisher
ieee
Conference_Titel
Unmanned Aircraft Systems (ICUAS), 2014 International Conference on
Conference_Location
Orlando, FL
Type
conf
DOI
10.1109/ICUAS.2014.6842327
Filename
6842327
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