Design and Aerodynamic Analysis of Dragonfly-like Flapping Wing Micro Air Vehicle

2022 ◽  
Author(s):  
Yanjuan Hu ◽  
Weiwei Ru ◽  
Qiang Liu ◽  
Zhanli Wang
Keyword(s):  
Flapping Wing ◽  
Micro Air Vehicle ◽  
Aerodynamic Analysis ◽  
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

Modeling and Trajectory Generation of Bird-like Flapping-wing Micro Air Vehicle

2020 ◽  
Author(s):  
Xinxing Mu ◽  
Xiuyu He ◽  
Liang Zhang ◽  
Qiang Fu ◽  
Wei He
Keyword(s):  
Trajectory Generation ◽  
Flapping Wing ◽  
Micro Air Vehicle ◽  
Air Vehicle

A Multi-Agent System for Autonomous Adaptive Control of a Flapping-Wing Micro Air Vehicle

2015 ◽  
Author(s):  
Garrison Greenwood ◽  
Michal Podhradsky ◽  
John Gallagher ◽  
Eric Matson
Keyword(s):  
Adaptive Control ◽  
Flapping Wing ◽  
Micro Air Vehicle ◽  
Multi Agent System ◽  
Agent System ◽  
Air Vehicle ◽  
Multi Agent

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

Flapping Wing Micro Air Vehicle Bench Test Set-up

2009 ◽  
Author(s):  
Craig Svanberg ◽  
Mark Reeder ◽  
David Curtis ◽  
Richard Cobb
Keyword(s):  
Flapping Wing ◽  
Micro Air Vehicle ◽  
Bench Test ◽  
Test Set ◽  
Air Vehicle ◽  
Set Up
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