Title:
AIRCRAFT AUTOMATIC CONTROL SYSTEM, METHOD FOR EVALUATING EFFECTIVENESS THEREOF, AND MEASURING DEVICE FOR SAID AUTOMATIC CONTROL SYSTEM
Document Type and Number:
WIPO Patent Application WO/2024/048101
Kind Code:
A1
Abstract:
An aircraft automatic control system according to an embodiment of the present invention comprises: a measuring unit which measures, as forecast information, a difference between a wind speed actually being experienced by the aircraft, and a wind speed to be encountered in the future, and which appends information for identifying an estimation error of the resulting measured value, or a validity/invalidity thereof, to measurement information and outputs the same; a rudder for controlling a lifting force, a drag force, or an attitude of the aircraft, or a device for controlling a thrust force; and a control arithmetic unit for calculating an angle of the rudder or the thrust force on the basis of a wind speed value in a planned flight direction of the aircraft, measured by the measuring unit, so as to reduce the effect the wind speed has on a fuselage.
Inventors:
INOKUCHI HAMAKI (JP)
HAMADA YOSHIRO (JP)
HAMADA YOSHIRO (JP)
Application Number:
PCT/JP2023/026239
Publication Date:
March 07, 2024
Filing Date:
July 18, 2023
Export Citation:
Assignee:
JAPAN AEROSPACE EXPLORATION (JP)
International Classes:
B64C13/16; B64D47/00
Foreign References:
| JP6583677B2 | 2019-10-02 | |||
| JP2021079731A | 2021-05-27 | |||
| JP7097052B2 | 2022-07-07 | |||
| JP7051081B2 | 2022-04-11 | |||
| US20140236397A1 | 2014-08-21 | |||
| JP2008500525A | 2008-01-10 |
Attorney, Agent or Firm:
MINAMI AOYAMA PATENT AND TRADEMARK ATTORNEYS (JP)
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