Flapping Wing Micro Air Vehicle Aerodynamic Modeling Including Flapping and Rigid Body Velocity

2012 ◽  
Author(s):  
David Sigthorsson ◽  
Michael Oppenheimer ◽  
David Doman
Keyword(s):  
Rigid Body ◽  
Flapping Wing ◽  
Micro Air Vehicle ◽  
Aerodynamic Modeling ◽  
Air Vehicle ◽  
Body Velocity

scholarly journals Rigid-Body Kinematics Versus Flapping Kinematics of a Flapping Wing Micro Air Vehicle

2015 ◽  
Vol 38 (12) ◽  
pp. 2257-2269 ◽  
Author(s):  
J. V. Caetano ◽  
M. B. Weehuizen ◽  
C. C. de Visser ◽  
G. C. H. E. de Croon ◽  
M. Mulder
Keyword(s):  
Rigid Body ◽  
Flapping Wing ◽  
Micro Air Vehicle ◽  
Air Vehicle

Design and Fabrication of an SU-8 Biomimetic Flapping-wing Micro Air Vehicle by MEMS Technology

ROBOT ◽  
2011 ◽  
Vol 33 (3) ◽  
pp. 366-370 ◽  
Author(s):  
Pengcheng CHI ◽  
Weiping ZHANG ◽  
Wenyuan CHEN ◽  
Hongyi LI ◽  
Kun MENG ◽  
...  
Keyword(s):  
Flapping Wing ◽  
Micro Air Vehicle ◽  
Air Vehicle ◽  
Mems Technology

scholarly journals Dove: A biomimetic flapping-wing micro air vehicle

2017 ◽  
Vol 10 (1) ◽  
pp. 70-84 ◽  
Author(s):  
Wenqing Yang ◽  
Liguang Wang ◽  
Bifeng Song
Keyword(s):  
Mechanism Design ◽  
Flapping Wing ◽  
Micro Air Vehicle ◽  
Flexible Wing ◽  
The Past ◽  
Ground Station ◽  
Air Vehicle ◽  
Research Goal ◽  
Color Video ◽  
Flapping Mechanism

This paper describes the design and development of the Dove, a flapping-wing micro air vehicle (FWMAV), which was developed in Northwestern Polytechnical University. FWMAVs have attracted international attentions since the past two decades. Since some achievements have been obtained, such as the capability of supporting an air vehicle to fly, our research goal was to design an FWMAV that has the ability to accomplish a task. Main investigations were presented in this paper, including the flexible wing design, the flapping mechanism design, and the on-board avionics development. The current Dove has a mass of 220 g, a wingspan of 50 cm, and the ability of operating fully autonomously, flying lasts half an hour, and transmitting live stabilized color video to a ground station over 4 km away.

Controlled Flight Maneuvers of a Flapping Wing Micro Air Vehicle: a Step Towards the Delfly II Identification

2013 ◽  
Author(s):  
Joao V. Caetano ◽  
Coen C. de Visser ◽  
Bart D. Remes ◽  
Christophe De Wagter ◽  
Erik-Jan Van Kampen ◽  
...  
Keyword(s):  
Flapping Wing ◽  
Micro Air Vehicle ◽  
Air Vehicle
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