AUTOMATIC TAKEOFF/LANDING SYSTEM FOR VERTICAL TAKEOFF/LANDING AIRCRAFT, VERTICAL TAKEOFF/LANDING AIRCRAFT, AND CONTROL METHOD FOR TAKEOFF/LANDING OF VERTICAL TAKEOFF/LANDING AIRCRAFT

WIPO Patent Application WO/2023/127289

A1

This automatic takeoff/landing system for a vertical takeoff/landing aircraft comprises: a relative wind information acquisition unit that acquires the direction of relative wind at a moving object; and a control unit that executes takeoff/landing control to cause the vertical take/off landing aircraft to takeoff/land at a takeoff/landing target point provided on the moving object. The control unit, at the time of takeoff/landing of the vertical takeoff/landing aircraft, executes the takeoff/landing control on the basis of the direction of the relative wind acquired by the relative wind information acquisition unit, in a state in which the heading direction of the vertical takeoff/landing aircraft is caused to face the direction of the relative wind.

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KOJIMA TORU (JP)

PCT/JP2022/040661

July 06, 2023

October 31, 2022

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MITSUBISHI HEAVY IND LTD (JP)

B64C13/18; G08G5/02

JP2020149640A	2020-09-17
JP2021062719A	2021-04-22
JPH06247394A	1994-09-06

SAKAI INTERNATIONAL PATENT OFFICE (JP)

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