CONTROL DEVICE OF VERTICAL TAKEOFF/LANDING AIRCRAFT

Title:

CONTROL DEVICE OF VERTICAL TAKEOFF/LANDING AIRCRAFT

Document Type and Number:

Japanese Patent JP2023104324

Kind Code:

A

Abstract:

To provide a control device of a vertical takeoff/landing aircraft that is capable of enhancing safety when abnormality of a driving device has occurred.SOLUTION: A flight control device conducts flight control processing for making an eVTOL fly. If EPU abnormality occurs during vertical takeoff, the flight control device 40 conducts during-takeoff processing in flight control processing. The flight control device 40 conducts abnormality stop processing in step S402 of the during-takeoff processing. In the abnormality stop processing, processing is carried out to stop the drive of an abnormal EPU. The flight control device 40 conducts correction augmentation processing in step S403. In the correction augmentation processing, output of at least one normal EPU is augmented. In the correction augmentation processing, for example, output of an adjacent EPU among a plurality of normal EPUs is augmented. The adjacent EPU is a normal EPU adjacent to the abnormal EPU in a circumferential direction of a yawing axis.SELECTED DRAWING: Figure 6

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Inventors:

FUKUSHI MASATO
SUGITA SHUN

Application Number:

JP2022005243A

Publication Date:

July 28, 2023

Filing Date:

January 17, 2022

Export Citation:

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Assignee:

DENSO CORP

International Classes:

B64D25/00; B64C27/26; B64D27/24

Attorney, Agent or Firm:

Kazuyuki Yahagi
Taihei Nonobe
Takanori Kubo

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