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Patent Searching and Data


Title:
FLIGHT VEHICLE CONTROL SYSTEM
Document Type and Number:
WIPO Patent Application WO/2022/264665
Kind Code:
A1
Abstract:
Provided is a flight vehicle control system that performs proper control on flight vehicles capable of vertical takeoffs and landings and that enables the flight vehicles to perform takeoffs and landings safely in a dense state in accordance with the conditions and environments of the flight vehicles. A flight vehicle control system 30 comprises a flight vehicle control device 20 and a ground monitoring device 10. The flight vehicle control device 20 comprises: a condition monitoring unit 22 which monitors the surrounding environment of a flight vehicle 1 and/or the operating condition of the flight vehicle 1; a flight control unit 21 which controls the flight of the flight vehicle 1; a closed space setting unit 23 which sets a closed space 2 for the flight vehicle 1; and a communication unit 24 for communicating with the ground monitoring device 10. The ground monitoring device 10 comprises: a flight position monitoring unit 11 which monitors the flight positions of a plurality of the flight vehicles 1; a closed space management unit 12 which manages the closed spaces 2 of the plurality of the flight vehicles 1; and a communication unit 13 which communicates with a plurality of the flight vehicle control devices 20. The closed space setting unit 23 performs control on the closed space 2 for the corresponding flight vehicle 1 on the basis of monitoring results obtained by the corresponding condition monitoring unit 22.

Inventors:
IMAMOTO KENJI (JP)
ITO TAKAHIRO (JP)
BANDO MIKIO (JP)
Application Number:
PCT/JP2022/017407
Publication Date:
December 22, 2022
Filing Date:
April 08, 2022
Export Citation:
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Assignee:
HITACHI LTD (JP)
International Classes:
B64C27/08; B64C39/02; G08G5/04
Foreign References:
JP2020057312A2020-04-09
JP2009184675A2009-08-20
JP2019172166A2019-10-10
JP2020087145A2020-06-04
Attorney, Agent or Firm:
KAICHI IP (JP)
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