Title:
FLIGHT DEVICE
Document Type and Number:
WIPO Patent Application WO/2018/037795
Kind Code:
A1
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:
BABA HIROYASU (JP)
MATSUE TAKENORI (JP)
KAWASAKI KOJI (JP)
KATO NAOYA (JP)
MATSUE TAKENORI (JP)
KAWASAKI KOJI (JP)
KATO NAOYA (JP)
Application Number:
PCT/JP2017/026503
Publication Date:
March 01, 2018
Filing Date:
July 21, 2017
Export Citation:
Assignee:
SOKEN INC (JP)
DENSO CORP (JP)
DENSO CORP (JP)
International Classes:
B64C27/08; B64C11/06
Foreign References:
| JP2005289127A | 2005-10-20 | |||
| JP2016049900A | 2016-04-11 |
Attorney, Agent or Firm:
SATO INTERNATIONAL PATENT FIRM (JP)
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