MULTICOPTER

Provided is a multicopter providing a high level of freedom in compact design, and consuming a relatively small amount of energy. The multicopter () includes a machine body (), an N number of first lift generators () arranged on a first concentric circle (C) centered substantially around a gravitational center (G) of the machine body () and in a front part and a rear part of the machine body in a bilateral symmetry, and an M number of second lift generators () arranged on a second concentric circle (C) centered substantially around the gravitational center (G) of the machine body () and having a larger diameter than the first concentric circle (C), and in a front part and a rear part of the machine body () on a central axial line (X) extending in a fore and aft direction of the machine body (), N being greater than M.