公开(公告)号：US20200150693A1

公开(公告)日：2020-05-14

申请号：US16589942

申请日：2019-10-01

Applicant: SUBARU CORPORATION

Inventor： Yukinobu TOMONAGA ,  Yu TAKAHASHI ,  Yohei MATSUGUMA

IPC: G05D1/10 ,  B64C39/02 ,  B64C27/82 ,  B64C27/52 ,  B64C37/02 ,  B60L50/60 ,  B60L53/50

Abstract: According to one implementation, a rotorcraft includes a first rotorcraft and at least one second rotorcraft. The first rotorcraft has a first main rotor and a first tail rotor. The at least one second rotorcraft has a second main rotor and a second tail rotor. The at least one second rotorcraft are attachable and detachable to and from the first rotorcraft. Further, according to one implementation, a method of controlling the above-mentioned rotorcraft includes: flying the first rotorcraft, to which the at least one second rotorcraft has been attached, to a destination; and separating the at least one second rotorcraft from the first rotorcraft at the destination.