Title:
AIRCRAFT POSITION CONTROL SYSTEM, AIRCRAFT, AND AIRCRAFT POSITION CONTROL METHOD
Document Type and Number:
WIPO Patent Application WO/2022/101895
Kind Code:
A1
Abstract:
An aircraft position control system that causes the position of an aircraft to adapt to the movement of a target landing point caused by swaying, said system comprising: a sway amount estimation processing unit that estimates the amount of swaying of the target landing point on the basis of an attitude weighted acceleration for correcting the attitude of the aircraft and on the basis of relative positions between the aircraft and the target landing point; and a target information generation unit that, on the basis of the estimated amount of swaying, outputs a target relative position serving as a target between the aircraft and the target landing point and a target relative velocity serving as a target between the aircraft and the target landing point.
Inventors:
KOJIMA TORU (JP)
MORI SATOSHI (JP)
TAKAGI KATSUMI (JP)
MORI SATOSHI (JP)
TAKAGI KATSUMI (JP)
Application Number:
PCT/IB2022/050233
Publication Date:
May 19, 2022
Filing Date:
January 13, 2022
Export Citation:
Assignee:
MITSUBISHI HEAVY IND LTD (JP)
International Classes:
B64C13/18; B64D45/04; B64D47/08; B64F1/00; G05B11/36; G06T7/20; G06T7/70
Foreign References:
| JP2005059656A | 2005-03-10 | |||
| JPH07304500A | 1995-11-21 | |||
| US20170267374A1 | 2017-09-21 | |||
| CN105059558A | 2015-11-18 | |||
| JP2021062720A | 2021-04-22 | |||
| JPH0471998A | 1992-03-06 | |||
| JP2021062720A | 2021-04-22 |
Other References:
See also references of EP 4227216A4
Attorney, Agent or Firm:
SAKAI INTERNATIONAL PATENT OFFICE (JP)
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