公开(公告)号：US20210129990A1

公开(公告)日：2021-05-06

申请号：US17146944

申请日：2021-01-12

Applicant: Panasonic Intellectual Property Management Co., Ltd.

Inventor： Kazuo INOUE ,  Kazunobu KONISHI ,  Stephen JOHN ,  Katsuhiko ASAI ,  Shunsuke KUHARA

IPC: B64C39/02 ,  G08G5/00

Abstract: An unmanned aircraft includes: at least two generators generating forces to fly the unmanned aircraft, each including a rotor blade generating an airflow; a sensor detecting a tilt of the unmanned aircraft; and a processor controlling the generators to control flight of the unmanned aircraft. The processor: obtains an output force adjustment trigger for the generators; obtaining the trigger, causes each generator to individually operate at least until the tilt of the unmanned aircraft detected by the sensor satisfies a predetermined condition; determines a reference value related to an output force of each generator from a value related to the output force of each generator when the tilt of the unmanned aircraft satisfies the predetermined condition and a positional relationship between the generators; and controls the flight of the unmanned aircraft, using the reference values determined.