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Quad-thopter: Tailless flapping wing robot with four pairs of wings
Author(s) -
Christophe De Wagter,
Matěj Karásek,
Guido C. H. E. de Croon
Publication year - 2018
Publication title -
international journal of micro air vehicles
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.324
H-Index - 21
eISSN - 1756-8307
pISSN - 1756-8293
DOI - 10.1177/1756829318794972
Subject(s) - flapping , micro air vehicle , wing , aerospace engineering , aerodynamics , thrust , engineering , wing twist , simulation , automotive engineering , computer science , angle of attack
We present a novel design of a tailless flapping wing micro air vehicle, which uses four independently driven pairs of flapping wings in order to fly and perform agile maneuvers. The wing pairs are arranged such that differential thrust generates the desired roll and pitch moments, similar to a quadrotor. Moreover, two pairs of wings are tilted clockwise and two pairs of wings anti-clockwise. This allows the micro air vehicle to generate a yaw moment. We have constructed the design and performed multiple flight tests with it, both indoors and outdoors. These tests have shown the vehicle to be capable of agile maneuvers and able to cope with wind gusts. The main advantage is that the proposed design is relatively simple to produce, and yet has the capabilities expected of tailless flapping wing micro air vehicles.

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