Title:
FLIGHT CONTROL SYSTEM, SERVER, FLIGHT CONTROL METHOD, AND FLIGHT CONTROL PROGRAM
Document Type and Number:
WIPO Patent Application WO/2024/038634
Kind Code:
A1
Abstract:
Provided is a flight method that makes it possible to prevent a collision of a drone and entanglement of a power supply cable. This flight control system relating to flight control of an electrically driven drone 3 that is connected to a power supply cable 4a provided from the ground side comprises: a first acquisition means 111 for acquiring flight distances when a plurality of drones 3 are to be flown from a parking station 800 (departure place) to respective corresponding destinations; a determination means 112 for determining flight methods for the drones 3 on the basis of the flight distances that have been acquired by the first acquisition means 111; a first control means 113 for flying the drones 3 in accordance with the flight methods that have been determined by the determination means 112; and a second control means 116 for advancing and retracting the power supply cable 4a at the speed corresponding to the flight speed of the drone 3.
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Inventors:
ABE YASUSHI (JP)
AOYAGI YASUSHI (JP)
AOYAGI YASUSHI (JP)
Application Number:
PCT/JP2023/009187
Publication Date:
February 22, 2024
Filing Date:
March 10, 2023
Export Citation:
Assignee:
IDEMITSU KOSAN CO (JP)
International Classes:
B64F3/02; B64C27/04; B64C39/02; B64D27/24; B64U10/60; G08G5/00; G08G5/04
Foreign References:
| JP2020154762A | 2020-09-24 | |||
| JP2017217942A | 2017-12-14 | |||
| JP2017013653A | 2017-01-19 |
Attorney, Agent or Firm:
HEIWA INTERNATIONAL PATENT OFFICE (JP)
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