Title:
飛行装置
Document Type and Number:
Japanese Patent JP6603186
Kind Code:
B2
Abstract:
When this flight device 10 changes the flight attitude and flight altitude, a control unit 40 changes the flight attitude and flight altitude using mainly the outputs of motors 131, 141, 151, 161 of each thruster 13-16, and finely adjusts the flight attitude and flight altitude using the pitch angles of propellers 23. When the altitude of the flight device 10 is maintained, i.e. when there are no significant changes to the flight attitude and the flight altitude such as during hovering, the control unit 40 controls the flight attitude and flight altitude by changing the pitch angles of the propellers 23, while reducing changes to the outputs of the motors 131, 141, 151, 161.
Inventors:
Hiroyasu Baba
Takenori Matsue
Koji Kawasaki
Naoya Kato
Takenori Matsue
Koji Kawasaki
Naoya Kato
Application Number:
JP2016161947A
Publication Date:
November 06, 2019
Filing Date:
August 22, 2016
Export Citation:
Assignee:
株式会社SOKEN
株式会社デンソー
株式会社デンソー
International Classes:
B64C27/08; B64C11/06
Domestic Patent References:
| JP2005349871A | ||||
| JP2005289127A | ||||
| JP2016049900A |
Foreign References:
| KR1020160092732A |
Attorney, Agent or Firm:
Patent Business Corporation Sato International Patent Office