MY187782A - Aerial vehicle guidance method, guidance device, and guidance system - Google Patents

Aerial vehicle guidance method, guidance device, and guidance system

Info

Publication number
MY187782A
MY187782A MYPI2021001406A MYPI2021001406A MY187782A MY 187782 A MY187782 A MY 187782A MY PI2021001406 A MYPI2021001406 A MY PI2021001406A MY PI2021001406 A MYPI2021001406 A MY PI2021001406A MY 187782 A MY187782 A MY 187782A
Authority
MY
Malaysia
Prior art keywords
aerial vehicle
guidance
cable
route
pole node
Prior art date
Application number
MYPI2021001406A
Inventor
Shuhei Komatsu
Original Assignee
A L I Tech 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 A L I Tech Inc filed Critical A L I Tech Inc
Publication of MY187782A publication Critical patent/MY187782A/en

Links

Classifications

    • 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
    • B64C13/18—Initiating means actuated automatically, e.g. responsive to gust detectors using automatic pilot
    • 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
    • G05D1/10—Simultaneous control of position or course in three dimensions
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/04—Anti-collision systems
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00—Type of UAV
    • B64U10/10—Rotorcrafts
    • B64U10/13—Flying platforms
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/10—Propulsion
    • B64U50/19—Propulsion using electrically powered motors

Landscapes

  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Traffic Control Systems (AREA)
  • Navigation (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)

Abstract

To provide new technology for guidance of an aerial vehicle (1). An aerial vehicle guidance method according to the present invention includes: a guidance device that performs a step of accepting a route request, a step of reading out pole node information corresponding to positions of poles (20), a step of identifying at least a start-point pole node and an end-point pole node based on the route request and the pole node information and generating a route, and a step of transmitting the generated route to an aerial vehicle (1); and a step of the aerial vehicle (1) flying according to the route; wherein: in the flying step, the aerial vehicle (1): measures that at least a strength of an electric field or a magnetic field of a cable (30) is a predetermined condition, and calculates the distance to the cable (30) based on the result of the measurement; receives information relating to at least a value of a voltage or a current flowing through the cable (30), and corrects the result of the calculation based on the information; and flies while maintaining a predetermined distance from the cable (30) based on the result of the corrected calculation.
MYPI2021001406A 2018-09-17 2019-09-17 Aerial vehicle guidance method, guidance device, and guidance system MY187782A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2018173169A JP6601810B1 (en) 2018-09-17 2018-09-17 Aircraft guidance method, guidance device, and guidance system

Publications (1)

Publication Number Publication Date
MY187782A true MY187782A (en) 2021-10-21

Family

ID=68462297

Family Applications (1)

Application Number Title Priority Date Filing Date
MYPI2021001406A MY187782A (en) 2018-09-17 2019-09-17 Aerial vehicle guidance method, guidance device, and guidance system

Country Status (3)

Country Link
JP (1) JP6601810B1 (en)
MY (1) MY187782A (en)
WO (1) WO2020059684A1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2021079531A1 (en) * 2019-10-26 2021-04-29 株式会社Ａ．Ｌ．Ｉ． Ｔｅｃｈｎｏｌｏｇｉｅｓ Route management control server, method, and system, and first flying body and second flying body used in the same

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2017131019A (en) * 2016-01-19 2017-07-27 中国電力株式会社 Power transmission facility inspection system
JP6833452B2 (en) * 2016-10-28 2021-02-24 株式会社東芝 Patrol inspection system, information processing device, patrol inspection control program
JP2018077754A (en) * 2016-11-11 2018-05-17 株式会社リコー Autonomous mobile device, program, and control method
JP2018114807A (en) * 2017-01-17 2018-07-26 中国電力株式会社 Unmanned flight vehicle and flight system
JP6589908B2 (en) * 2017-02-28 2019-10-16 東京電力ホールディングス株式会社 Control device, flight control method, and program

Also Published As

Publication number Publication date
WO2020059684A1 (en) 2020-03-26
JP6601810B1 (en) 2019-11-06
JP2020046788A (en) 2020-03-26

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