[go: up one dir, main page]

WO2019230885A1 - Serveur et système de gestion de vol pour véhicule aérien sans pilote - Google Patents

Serveur et système de gestion de vol pour véhicule aérien sans pilote Download PDF

Info

Publication number
WO2019230885A1
WO2019230885A1 PCT/JP2019/021528 JP2019021528W WO2019230885A1 WO 2019230885 A1 WO2019230885 A1 WO 2019230885A1 JP 2019021528 W JP2019021528 W JP 2019021528W WO 2019230885 A1 WO2019230885 A1 WO 2019230885A1
Authority
WO
WIPO (PCT)
Prior art keywords
flight
management server
unmanned air
air vehicle
mission
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Ceased
Application number
PCT/JP2019/021528
Other languages
English (en)
Japanese (ja)
Inventor
太郎 吉井
高橋　和也
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Sensyn Robotics Inc
Original Assignee
Sensyn Robotics Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Sensyn Robotics Inc filed Critical Sensyn Robotics Inc
Priority to JP2019563630A priority Critical patent/JP6713156B2/ja
Publication of WO2019230885A1 publication Critical patent/WO2019230885A1/fr
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Images

Classifications

    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/60—Intended control result
    • G05D1/656—Interaction with payloads or external entities
    • G05D1/689—Pointing payloads towards fixed or moving targets
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/02—Initiating means
    • B64C13/16—Initiating means actuated automatically, e.g. responsive to gust detectors
    • B64C13/20—Initiating means actuated automatically, e.g. responsive to gust detectors using radiated signals
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C21/00—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
    • G01C21/20—Instruments for performing navigational calculations
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/20—Control system inputs
    • G05D1/22—Command input arrangements
    • G05D1/221—Remote-control arrangements
    • G05D1/222—Remote-control arrangements operated by humans
    • G05D1/224—Output arrangements on the remote controller, e.g. displays, haptics or speakers
    • G05D1/2244—Optic
    • G05D1/2245—Optic providing the operator with a purely computer-generated representation of the environment of the vehicle, e.g. virtual reality
    • G05D1/2246—Optic providing the operator with a purely computer-generated representation of the environment of the vehicle, e.g. virtual reality displaying a map of the environment
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/20—Control system inputs
    • G05D1/22—Command input arrangements
    • G05D1/221—Remote-control arrangements
    • G05D1/225—Remote-control arrangements operated by off-board computers
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/60—Intended control result
    • G05D1/646—Following a predefined trajectory, e.g. a line marked on the floor or a flight path
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/60—Intended control result
    • G05D1/648—Performing a task within a working area or space, e.g. cleaning
    • G05D1/6482—Performing a task within a working area or space, e.g. cleaning by dividing the whole area or space in sectors to be processed separately
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/60—Intended control result
    • G05D1/69—Coordinated control of the position or course of two or more vehicles
    • G05D1/698—Control allocation
    • G05D1/6987—Control allocation by centralised control off-board any of the vehicles
    • G—PHYSICS
    • G06—COMPUTING OR CALCULATING; COUNTING
    • G06Q—INFORMATION AND COMMUNICATION TECHNOLOGY [ICT] SPECIALLY ADAPTED FOR ADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL OR SUPERVISORY PURPOSES; SYSTEMS OR METHODS SPECIALLY ADAPTED FOR ADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL OR SUPERVISORY PURPOSES, NOT OTHERWISE PROVIDED FOR
    • G06Q50/00—Information and communication technology [ICT] specially adapted for implementation of business processes of specific business sectors, e.g. utilities or tourism
    • G06Q50/10—Services
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2201/00—UAVs characterised by their flight controls
    • B64U2201/10—UAVs characterised by their flight controls autonomous, i.e. by navigating independently from ground or air stations, e.g. by using inertial navigation systems [INS]
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D2105/00—Specific applications of the controlled vehicles
    • G05D2105/80—Specific applications of the controlled vehicles for information gathering, e.g. for academic research
    • G05D2105/89—Specific applications of the controlled vehicles for information gathering, e.g. for academic research for inspecting structures, e.g. wind mills, bridges, buildings or vehicles
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D2107/00—Specific environments of the controlled vehicles
    • G05D2107/70—Industrial sites, e.g. warehouses or factories
    • G05D2107/75—Electric power generation plants
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D2109/00—Types of controlled vehicles
    • G05D2109/20—Aircraft, e.g. drones
    • G05D2109/25—Rotorcrafts
    • G05D2109/254—Flying platforms, e.g. multicopters
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D2111/00—Details of signals used for control of position, course, altitude or attitude of land, water, air or space vehicles
    • G05D2111/10—Optical signals

Definitions

  • the present invention relates to a flight management server and a flight management system for an unmanned air vehicle.
  • Patent Document 1 discloses a system that creates a flight route of an unmanned aircraft that acquires data for inspection from a windmill by reflecting the control state of the windmill.
  • drones have various needs such as security, collection of information at the time of disaster, surveying, etc. as well as the above-mentioned inspections, and the targets are diverse, such as solar power generation facilities, bridges, roads, etc.
  • An object of the present invention is to provide a technique capable of automatically setting an optimal flight route by simply selecting various work targets.
  • An unmanned air vehicle flight management server connected to a user terminal and an unmanned air vehicle via a network, A storage unit that stores flight route information including flight parameters, and a plurality of flight applications by purpose; A reception unit that accepts a flight request including at least a flight location and a flight purpose; A generating unit that generates a flight mission including a flight route generated by referring to the flight route information based on the flight request and a flight application selected from the purpose-specific flight application; A communication unit for transmitting the generated flight mission to the unmanned air vehicle; An unmanned air vehicle flight management server.
  • a flight management server and a flight management system have the following configuration.
  • An unmanned air vehicle flight management server connected to a user terminal and an unmanned air vehicle via a network, A storage unit that stores flight route information including flight parameters, and a plurality of flight applications by purpose; A reception unit that accepts a flight request including at least a flight location and a flight purpose; A generating unit that generates a flight mission including a flight route generated by referring to the flight route information based on the flight request and a flight application selected from the purpose-specific flight application; A communication unit for transmitting the generated flight mission to the unmanned air vehicle; An unmanned air vehicle flight management server.
  • a flight management system for an unmanned air vehicle including a user terminal, an unmanned air vehicle, and a flight management server connected via a network
  • the flight management server is: A storage unit for storing flight route information including flight parameters and a plurality of purpose-specific flight applications; Accepting a flight request including at least a flight location and a flight purpose from the user terminal; Generating a flight mission including a flight route generated by referring to the flight route information and a flight application selected from the purpose-specific flight application based on the flight request; Sending the generated flight mission to the unmanned air vehicle;
  • the unmanned air vehicle performs the flight mission and transmits a flight log to the flight management server.
  • Flight management system for unmanned air vehicles is: A storage unit for storing flight route information including flight parameters and a plurality of purpose-specific flight applications; Accepting a flight request including at least a flight location and a flight purpose from the user terminal; Generating a flight mission including a flight route generated by referring to the flight route information and a flight application selected from
  • the present system a flight management system
  • the present system a flight management system for an unmanned air vehicle according to an embodiment of the present invention.
  • the same or similar elements are denoted by the same or similar reference numerals and names, and redundant description of the same or similar elements may be omitted in the description of each embodiment.
  • the features shown in each embodiment can be applied to other embodiments as long as they do not contradict each other.
  • the present system includes a management server 1, a plurality of user terminals 2 and 3, and one or more flying bodies 4.
  • the management server 1, the user terminals 2 and 3, and the flying object 4 are connected to be communicable with each other via a network.
  • FIG. 2 is a diagram illustrating a hardware configuration of the management server 1.
  • the structure shown in figure is an example and may have a structure other than this.
  • the management server 1 is connected to a plurality of user terminals 2 and 3 and the flying vehicle 4 to constitute a part of the present system.
  • the management server 1 may be a general-purpose computer such as a workstation or a personal computer, or may be logically realized by cloud computing.
  • the management server 1 includes at least a processor 10, a memory 11, a storage 12, a transmission / reception unit 13, an input / output unit 14, and the like, which are electrically connected to each other through a bus 15.
  • the processor 10 is an arithmetic device that controls the overall operation of the management server 1 and performs data transmission / reception control between elements and information processing necessary for application execution and authentication processing.
  • the processor 10 is a CPU (Central Processing Unit) and executes each information process by executing a program for the system stored in the storage 12 and expanded in the memory 11.
  • CPU Central Processing Unit
  • the memory 11 includes a main memory composed of a volatile storage device such as a DRAM (Dynamic Random Access Memory) and an auxiliary memory composed of a nonvolatile storage device such as a flash memory or an HDD (Hard Disc Drive). .
  • the memory 11 is used as a work area of the processor 10 and stores BIOS (Basic Input / Output System) executed when the management server 1 is started up, various setting information, and the like.
  • BIOS Basic Input / Output System
  • the storage 12 stores various programs such as application programs.
  • a database storing data used for each process may be constructed in the storage 12.
  • the transmission / reception unit 13 connects the management server 1 to a network and a block chain network.
  • the transmission / reception unit 13 may include a Bluetooth (registered trademark) and a BLE (Bluetooth Low Energy) short-range communication interface.
  • the input / output unit 14 is an information input device such as a keyboard / mouse and an output device such as a display.
  • the bus 15 is commonly connected to each of the above elements, and transmits, for example, an address signal, a data signal, and various control signals.
  • the user terminals 2 and 3 shown in FIG. 3 also include a processor 20, a memory 21, a storage 22, a transmission / reception unit 23, an input / output unit 24, and the like, which are electrically connected to each other through a bus 25. Since the function of each element can be configured in the same manner as the management server 1 described above, detailed description of each element is omitted.
  • FIG. 4 is a block diagram showing a hardware configuration of the flying object 4.
  • the flight controller 41 may have one or more processors such as a programmable processor (eg, a central processing unit (CPU)).
  • a programmable processor eg, a central processing unit (CPU)
  • the flight controller 41 has a memory 411 and can access the memory.
  • Memory 411 stores logic, code, and / or program instructions that can be executed by the flight controller to perform one or more steps.
  • the flight controller 41 may include sensors 412 such as an inertial sensor (acceleration sensor, gyro sensor), a GPS sensor, and a proximity sensor (for example, a rider).
  • the memory 411 may include a separable medium such as an SD card or a random access memory (RAM) or an external storage device. Data obtained from the camera / sensors 42 may be transmitted directly to the memory and stored. For example, still image / moving image data shot by a camera or the like is recorded in a built-in memory or an external memory.
  • the camera 42 is installed on the flying object via the gimbal 43.
  • the flight controller 41 includes a control module (not shown) configured to control the state of the flying object.
  • the control module may adjust the spatial arrangement, velocity, and / or acceleration of an aircraft that has six degrees of freedom (translational motion x, y, and z, and rotational motion ⁇ x , ⁇ y, and ⁇ z ).
  • the propulsion mechanism (motor 45 and the like) of the flying object is controlled via an ESC 44 (Electric Speed Controller).
  • the propeller 46 is rotated by the motor 45 fed from the battery 48 to generate lift of the flying object.
  • the control module can control one or more of the states of the mounting unit and sensors.
  • the flight controller 41 is configured to send and / or receive data from one or more external devices (eg, a transceiver 49, a terminal, a display device, or other remote controller).
  • a transceiver 49 e.g., a transceiver 49, a terminal, a display device, or other remote controller.
  • the communication with the unit 47 is possible.
  • the transceiver 49 can use any appropriate communication means such as wired communication or wireless communication.
  • the transmission / reception unit 47 uses one or more of local area network (LAN), wide area network (WAN), infrared, wireless, WiFi, point-to-point (P2P) network, telecommunication network, cloud communication, and the like. can do.
  • LAN local area network
  • WAN wide area network
  • infrared wireless
  • WiFi point-to-point
  • P2P point-to-point
  • telecommunication network cloud communication, and the like. can do.
  • the transmission / reception unit 47 transmits and / or receives one or more of data acquired by the sensors 42, a processing result generated by the flight controller 41, predetermined control data, a user command from a terminal or a remote controller, and the like. be able to.
  • the sensors 42 may include an inertial sensor (acceleration sensor, gyro sensor), a GPS sensor, a proximity sensor (eg, a rider), or a vision / image sensor (eg, a camera).
  • an inertial sensor acceleration sensor, gyro sensor
  • GPS sensor GPS sensor
  • proximity sensor eg, a rider
  • vision / image sensor eg, a camera
  • FIG. 5 is a block diagram illustrating functions implemented in the management server 1.
  • the management server 1 includes a communication unit 110, a flight mission generation unit 130, a report generation unit 150, an application unit 170, and a storage unit 190.
  • the flight mission generation unit 130 includes a route generation unit 132, an application selection unit 134, an evaluation unit 136, and a correction unit 138.
  • the storage unit 190 includes various databases of flight route information 192, purpose-specific flight applications 194, flight logs 196, and interface information 198.
  • the communication unit 110 communicates with the user terminal 2 and the flying object 4.
  • the communication unit 110 also functions as a reception unit that receives a flight request including at least a flight location and a flight purpose from the user terminal 2.
  • the flight mission generation unit 130 generates a flight mission.
  • the flight mission is an application selected from the flight route and purpose-specific flight application 194.
  • the flight route is generated by the route generation unit 132 with reference to the flight route information 192.
  • the flight application is selected by the application selection unit 134 with reference to the purpose-specific flight application 194.
  • an evaluation unit 136 that evaluates whether the generated flight mission is appropriate may be provided.
  • the evaluation unit 136 may evaluate the suitability based on a score or the like by, for example, a user operation on a flight mission or machine learning based on a flight mission accumulated in the past. If the score is not within the predetermined range, the flight mission is corrected by the correction unit 138.
  • information (still images, moving images, audio and other information) acquired by the flying object 4 is accumulated in the flight log 196.
  • the report generation unit 150 generates report information to be transmitted to the user terminal 2 based on the flight log. Examples of the report according to the present embodiment include the inspection result of the inspection target facility and the security result of the security target facility, but may be various reports according to needs.
  • the interface information 198 stores various control information to be displayed on the display unit (display or the like) of the user terminal 2 together with the application unit 170 (see FIG. 10 for a screen example).
  • FIG. 6 is a functional block diagram implemented in the user terminal 2.
  • the user terminal 2 includes a communication unit 210, a storage unit 220, an input unit 240, an output unit 250, and an application unit 270, and interacts with each other.
  • the purpose-specific flight application 194 is prepared for each work purpose (use) of the flying object 4 working with the present system.
  • an application 1941 for security / monitoring, an application 1942 for equipment inspection, an application 1943 for surveying, and an application 1944 for disaster countermeasures are included, but are not limited thereto.
  • information on flight control (altitude, speed, range, etc.) suitable for the purpose, acquisition conditions (camera resolution, shooting angle, overlap rate, presence of filters, estimated flight time, battery required)
  • the user transmits a flight request from the user terminal 2 (SQ101).
  • the flight request includes at least information regarding the flight location and the flight purpose.
  • the management server 1 refers to the storage unit 190 (see FIG. 5) (SQ102) and generates a flight mission (SQ104).
  • the generated flight mission is transmitted to the flying object 4 directly (or indirectly via a terminal or a transmitter) (SQ106).
  • the flying object 4 transmits (reports) the information acquired during the flight mission to the management server 1 in real time (or after the fact) (SQ108).
  • the management server 1 generates a report based on information (flight log) acquired from the flying object (SQ110).
  • FIG. 9 is an example of generating a flight mission (flight route) of a photovoltaic power generation facility.
  • a route based on the inspection by a plurality of flying objects may be generated in consideration of the power supply (battery) of the flying object, the inspection time, and the like.
  • flight routes R1 and R2 by the flying bodies 4a and 4b are generated for the flight areas A1 and A2.
  • Information acquired by the flying objects 4a and 4b is merged based on position information and time information associated with the acquired information on the management server 1 side, and used for report generation.
  • a flight request may be transmitted for each flying body to generate a flying route, or a flight request of one flying body 4a as shown in FIG.
  • flight routes R4 and R5 for each aircraft may be assigned based on the flight route R3 generated for the aircraft.
  • a series of flight routes R ⁇ b> 6 by one flying body 4 may be generated for a plurality of flight routes in the flight areas A ⁇ b> 1 and A ⁇ b> 2 that are originally performed by two (a plurality).
  • the replacement battery 5 is replaced in the middle of the flight route R6.
  • a flight route R7 may be set.
  • FIG. 13 is a display example displayed on the display DP of the user terminal 2 when receiving an input (operation) of a flight request from the user.
  • the user selects the purpose of checking the solar facility (not shown), and designates a specific range S on the map, whereby the flight route R8 is automatically generated.
  • the flight mission including the automatically generated flight route can be customized by receiving additional detailed adjustments from the user.
  • FIG. 14 is a display example in which a report generated based on still image information acquired by the flying object is displayed on the display DP of the user terminal 2.
  • the still image information P1 acquired by the flying object is plotted on the map image M acquired in advance (for example, an ortho image based on separately acquired information or a map image acquired through the Internet) ( By superimposing), the latest information is superimposed and displayed so that it can be easily confirmed.
  • the information displayed on the display DP of the user terminal 2 as a report is not limited to the plotted still image information, and information useful for inspection (for example, date and time, information on the flying object, the number of abnormal parts, etc.) is displayed. Also good.
  • the flying object of the present invention can be used in airplane related industries such as a multicopter drone. Furthermore, the present invention can be suitably used as an aerial photography flying object equipped with a camera or the like. It can also be used in various industries such as security, agriculture, and infrastructure monitoring.

Landscapes

  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Business, Economics & Management (AREA)
  • Tourism & Hospitality (AREA)
  • Economics (AREA)
  • Health & Medical Sciences (AREA)
  • General Health & Medical Sciences (AREA)
  • Human Resources & Organizations (AREA)
  • Marketing (AREA)
  • Primary Health Care (AREA)
  • Strategic Management (AREA)
  • General Business, Economics & Management (AREA)
  • Theoretical Computer Science (AREA)
  • Navigation (AREA)
  • Traffic Control Systems (AREA)
  • Management, Administration, Business Operations System, And Electronic Commerce (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)

Abstract

Le problème à résoudre dans le cadre de la présente invention consiste à paramétrer automatiquement un itinéraire de vol optimal en sélectionnant uniquement divers thèmes de travail. Par conséquent, un serveur de gestion de vol (1) d'après la présente invention est connecté à un terminal utilisateur (2) et à un véhicule aérien sans pilote (4) par l'intermédiaire d'un réseau. Le serveur de gestion de vol (1) comprend : une unité de stockage (190) destinée à stocker une pluralité d'applications de vol en fonction de différents objectifs et des informations sur un itinéraire de vol contenant des paramètres de vol ; une unité de réception (110) destinée à recevoir une demande de vol contenant au moins un endroit de vol et un objectif de vol ; une unité de génération (130) conçue pour utiliser la demande de vol de façon à générer une mission de vol contenant un trajet de vol généré à l'aide des informations sur un itinéraire de vol faisant office de référence et une application de vol sélectionnée parmi les applications de vol en fonction de différents objectifs ; et une unité de communication (110) conçue pour transmettre la mission de vol générée au véhicule aérien sans pilote (4).
PCT/JP2019/021528 2018-05-30 2019-05-30 Serveur et système de gestion de vol pour véhicule aérien sans pilote Ceased WO2019230885A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2019563630A JP6713156B2 (ja) 2018-05-30 2019-05-30 無人飛行体のフライト管理サーバ及びフライト管理システム

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
JP2018-103334 2018-05-30
JP2018103334 2018-05-30

Publications (1)

Publication Number Publication Date
WO2019230885A1 true WO2019230885A1 (fr) 2019-12-05

Family

ID=68697604

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/JP2019/021528 Ceased WO2019230885A1 (fr) 2018-05-30 2019-05-30 Serveur et système de gestion de vol pour véhicule aérien sans pilote

Country Status (2)

Country Link
JP (3) JP6713156B2 (fr)
WO (1) WO2019230885A1 (fr)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP6765738B1 (ja) * 2019-06-21 2020-10-07 株式会社センシンロボティクス 無人飛行体のフライト管理サーバ及びフライト管理システム
JP2021139874A (ja) * 2020-03-04 2021-09-16 株式会社センシンロボティクス 飛行体の管理サーバ及び管理システム
JP2021139876A (ja) * 2020-03-04 2021-09-16 株式会社センシンロボティクス 飛行体の管理サーバ及び管理システム
WO2025169632A1 (fr) * 2024-02-05 2025-08-14 ソニーグループ株式会社 Dispositif de traitement d'informations et procédé de traitement d'informations

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2022080325A (ja) * 2020-11-18 2022-05-30 日本電気株式会社 行動提案装置、行動提案方法およびコンピュータプログラム
DE112022004505T5 (de) 2021-11-19 2024-08-08 Fujifilm Corporation Bewegliches objekt, bildgebungssystem mit beweglichem objekt und bildgebungsverfahren mit beweglichem objekt
CN118383037A (zh) 2021-11-19 2024-07-23 富士胶片株式会社 信息处理装置、信息处理方法及程序

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2018034033A1 (fr) * 2016-08-16 2018-02-22 本郷飛行機株式会社 Dispositif de commande de communication
WO2018078863A1 (fr) * 2016-10-31 2018-05-03 株式会社オプティム Système, procédé et programme de commande de drone

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8060270B2 (en) * 2008-02-29 2011-11-15 The Boeing Company System and method for inspection of structures and objects by swarm of remote unmanned vehicles
CN109002052A (zh) * 2014-07-31 2018-12-14 深圳市大疆创新科技有限公司 使用无人飞行器实现的虚拟观光系统及方法
US11034444B2 (en) * 2015-10-07 2021-06-15 Blue Innovation Co., Ltd. Flight management system for flying objects
JP6739972B2 (ja) * 2016-04-11 2020-08-12 株式会社東芝 マルチエージェントシステム、タスク割当装置、タスク割当方法及びプログラム

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2018034033A1 (fr) * 2016-08-16 2018-02-22 本郷飛行機株式会社 Dispositif de commande de communication
WO2018078863A1 (fr) * 2016-10-31 2018-05-03 株式会社オプティム Système, procédé et programme de commande de drone

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP6765738B1 (ja) * 2019-06-21 2020-10-07 株式会社センシンロボティクス 無人飛行体のフライト管理サーバ及びフライト管理システム
JP2021139874A (ja) * 2020-03-04 2021-09-16 株式会社センシンロボティクス 飛行体の管理サーバ及び管理システム
JP2021139876A (ja) * 2020-03-04 2021-09-16 株式会社センシンロボティクス 飛行体の管理サーバ及び管理システム
WO2025169632A1 (fr) * 2024-02-05 2025-08-14 ソニーグループ株式会社 Dispositif de traitement d'informations et procédé de traitement d'informations

Also Published As

Publication number Publication date
JP2020140726A (ja) 2020-09-03
JPWO2019230885A1 (ja) 2020-06-11
JP2024096828A (ja) 2024-07-17
JP6713156B2 (ja) 2020-06-24

Similar Documents

Publication Publication Date Title
JP6713156B2 (ja) 無人飛行体のフライト管理サーバ及びフライト管理システム
US20170023939A1 (en) System and Method for Controlling an Unmanned Aerial Vehicle over a Cellular Network
CN103675609A (zh) 电力巡线设备及系统
JP2025016555A (ja) 位置算出方法及び情報処理システム
JP2025111687A (ja) 無人飛行体のフライト管理サーバ及びフライト管理システム
JP7679097B2 (ja) 作業計画生成システム
JP6966810B2 (ja) 管理サーバ及び管理システム、表示情報生成方法、プログラム
KR102526202B1 (ko) 실내 자율 비행 드론 제어 시스템 및 그 방법
JP7149569B2 (ja) 建造物の測定方法
JP6807093B1 (ja) 点検システム及び管理サーバ、プログラム、ヒビ割れ情報提供方法
JP2020201849A (ja) 飛行体の制御方法
JP6730764B1 (ja) 飛行体の飛行経路表示方法及び情報処理装置
JP6765738B1 (ja) 無人飛行体のフライト管理サーバ及びフライト管理システム
JP2019123337A (ja) 動作体
JP7333129B2 (ja) 撮影方法
JP2026016667A (ja) 無人飛行体のフライト管理サーバ及びフライト管理システム
WO2021124579A1 (fr) Procédé de capture d'image de véhicule volant et dispositif de traitement d'informations
JP6960643B1 (ja) 点検システム及び管理サーバ、プログラム、ヒビ割れ情報提供方法
WO2021038667A1 (fr) Dispositif de commande de véhicule aérien sans pilote, système de commande de véhicule aérien sans pilote et procédé de commande de véhicule aérien sans pilote
JP6715541B1 (ja) 飛行体の管理サーバ及び管理システム
JP6786138B1 (ja) 飛行体の管理サーバ及び管理システム
JP6771253B1 (ja) 飛行体の管理サーバ及び管理システム
JPWO2021064982A1 (ja) 情報処理装置および情報処理方法
KR102840590B1 (ko) 치수 표시 시스템 및 치수 표시 방법
JP7370045B2 (ja) 寸法表示システムおよび寸法表示方法

Legal Events

Date Code Title Description
ENP Entry into the national phase

Ref document number: 2019563630

Country of ref document: JP

Kind code of ref document: A

121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 19811494

Country of ref document: EP

Kind code of ref document: A1

NENP Non-entry into the national phase

Ref country code: DE

122 Ep: pct application non-entry in european phase

Ref document number: 19811494

Country of ref document: EP

Kind code of ref document: A1