A multicopter 1 comprises: a support 10; rotors 20 supported by the support 10; an internal combustion engine 32 supported by the support 10; a generator 47 supported by the support 10 and driven by the internal combustion engine 32 to generate power; electric motors 48 supported by the support 10, supplied with electric power from the generators 47, and configured to drive the rotors 20; and a controller configured to control a flight of an aircraft by individually adjusting a rotational speed of each of the rotors 20. The multicopter 1 also comprises at least one of a plurality of the internal combustion engines 32 or a plurality of the generators 47.
MULTICOPTER
MULTIKOPTER
MULTICOPTÈRE
2024-01-17
Patent
Electronic Resource
English
MULTICOPTER CONTROL METHOD, MULTICOPTER CONTROLLER, AND MULTICOPTER TOY
European Patent Office | 2017
|European Patent Office | 2019
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