Title:
CONTROL DEVICE FOR VERTICAL TAKE-OFF AND LANDING AIRCRAFT
Document Type and Number:
WIPO Patent Application WO/2023/136014
Kind Code:
A1
Abstract:
This flight control device carries out a flight control process for causing an eVTOL to fly. When an EPU abnormality occurs during vertical takeoff, a flight control device (40) performs a during-takeoff process in a flight control process. The flight control device (40) performs an abnormal stop process in step S402 of the during-takeoff process. In the abnormal stop process, a process for stopping the driving of the abnormal EPU is performed. The flight control device (40) performs a corrective increase process in step S403. In the corrective increase process, the output of at least one normal EPU is increased. In the corrective increase process, for example, the output of adjacent EPUs among a plurality of normal EPUs is increased. Adjacent EPUs are normal EPUs adjacent to the abnormal EPU in the circumferential direction of the yaw axis.
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Inventors:
FUKUSHI MASATO (JP)
SUGITA SHUN (JP)
SUGITA SHUN (JP)
Application Number:
PCT/JP2022/045711
Publication Date:
July 20, 2023
Filing Date:
December 12, 2022
Export Citation:
Assignee:
DENSO CORP (JP)
International Classes:
B64D25/00; B64C27/26; B64D27/24
Domestic Patent References:
| WO2018110598A1 | 2018-06-21 |
Foreign References:
| JP2014227155A | 2014-12-08 | |||
| JP2016524567A | 2016-08-18 | |||
| JP2002347698A | 2002-12-04 | |||
| JP2017100651A | 2017-06-08 | |||
| JP2020117223A | 2020-08-06 |
Attorney, Agent or Firm:
YAHAGI Kazuyuki et al. (JP)
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