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.
aerodynamic forces to provide vehicle lift.
| Original language | English |
|---|---|
| Patent number | NL2016130B1 |
| IPC | B64C 33/02 B64C 39/00 |
| Priority date | 21/01/16 |
| Publication status | Published - 2017 |