Title:
FLIGHT CONTROL DEVICE, AND CONTROL DEVICE FOR VERTICAL TAKEOFF/LANDING AIRCRAFT
Document Type and Number:
WIPO Patent Application WO/2023/079964
Kind Code:
A1
Abstract:
This flight control device performs flight control processing for causing an eVTOL to fly. The flight control device sets an operating mode to one of a plurality of failsafe modes in accordance with which of a plurality of normal modes the operating mode is when an abnormality occurs in the eVTOL. If the operating mode at the time of abnormality occurrence is a vertical landing mode, the flight control device changes the operating mode to a continue landing mode in step S105. If the operating mode at the time of abnormality occurrence is a vertical takeoff mode, the flight control device sets the operating mode to an emergency landing mode in step S107. If the operating mode at the time of abnormality occurrence is a cruise mode or a hovering mode, the flight control device sets the operating mode to a reset mode in step S108.
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Inventors:
TAKEMURA YUICHI (JP)
NAKATA SHINGO (JP)
NAKATA SHINGO (JP)
Application Number:
PCT/JP2022/039013
Publication Date:
May 11, 2023
Filing Date:
October 20, 2022
Export Citation:
Assignee:
DENSO CORP (JP)
International Classes:
B64D45/00; B64C29/00; B64C39/02; B64D27/24
Foreign References:
| CN111213106A | 2020-05-29 | |||
| JP2020167485A | 2020-10-08 | |||
| JP2018030568A | 2018-03-01 | |||
| JP2020196440A | 2020-12-10 | |||
| JP2020196440A | 2020-12-10 |
Attorney, Agent or Firm:
YAHAGI Kazuyuki et al. (JP)
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