Multiple pairs of flapping wings for attitude control

Research output: Patent

Abstract

The present invention is in the field of flapping wing micro air vehicles, combining a multicopter and a flapping micro air vehicle in one device. Micro air vehicle is defined as a powered aerial vehicle that does not carry a human operator and uses
aerodynamic forces to provide vehicle lift.
Original languageEnglish
Patent numberNL2016130B1
IPCB64C 33/02 B64C 39/00
Priority date21/01/16
Publication statusPublished - 2017

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