Print Email Facebook Twitter Quad-thopter: Tailless Flapping Wing Robot with 4 Pairs of Wings Title Quad-thopter: Tailless Flapping Wing Robot with 4 Pairs of Wings Author de Wagter, C. (TU Delft Control & Simulation) Karasek, M. (TU Delft Control & Simulation) de Croon, G.C.H.E. (TU Delft Control & Simulation) Contributor J.-M. Moschetta G. Hattenberger, H. de Plinval (editor) Date 2017-09-01 Abstract We present a novel design of a tailless flapping wing Micro Air Vehicle (MAV), 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 MAV 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 MAVs. To reference this document use: http://resolver.tudelft.nl/uuid:b4fc2b39-b8b1-4791-b071-98557a7254f0 Source International Micro Air Vehicle Conference and Flight Competition 2017 Event 9th international micro air vehicles, 2017-09-18 → 2017-09-21, Toulouse, France Part of collection Institutional Repository Document type conference paper Rights © 2017 C. de Wagter, M. Karasek, G.C.H.E. de Croon Files PDF 263_imav2017_proceedings.pdf 3.07 MB Close viewer /islandora/object/uuid:b4fc2b39-b8b1-4791-b071-98557a7254f0/datastream/OBJ/view