Title:
航空機の制御システム、航空機の制御方法及び航空機
Document Type and Number:
Japanese Patent JP6706235
Kind Code:
B2
Abstract:
An aircraft control system includes a flow control device and a control circuit. The flow control device is configured to control a flow of air around an aircraft. The control circuit is configured to control the flow control device so that a pressure distribution loaded on a surface of a structure that constitutes the aircraft is equal to a control value of a pressure distribution calculated based on a physical quantity detected by a sensor provided in the aircraft. The physical quantity relates to the air.
Inventors:
Takashi Miyawaki
Abe Masakatsu
Hiroki Kato
Abe Masakatsu
Hiroki Kato
Application Number:
JP2017213275A
Publication Date:
June 03, 2020
Filing Date:
November 02, 2017
Export Citation:
Assignee:
Subaru corporation
International Classes:
B64C21/10; B64C21/08; B64D45/00; H05H1/24
Domestic Patent References:
| JP6336199A | ||||
| JP2008505004A |
Foreign References:
| US5740991 | ||||
| US9541106 |
Attorney, Agent or Firm:
Takehiko Yamada