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WO2018032422A1 - Procédé et système de commande du courant d'entrée de multiples moteurs d'un véhicule aérien sans pilote - Google Patents

Procédé et système de commande du courant d'entrée de multiples moteurs d'un véhicule aérien sans pilote Download PDF

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Publication number
WO2018032422A1
WO2018032422A1 PCT/CN2016/095716 CN2016095716W WO2018032422A1 WO 2018032422 A1 WO2018032422 A1 WO 2018032422A1 CN 2016095716 W CN2016095716 W CN 2016095716W WO 2018032422 A1 WO2018032422 A1 WO 2018032422A1
Authority
WO
WIPO (PCT)
Prior art keywords
drone
current
wind power
power value
current range
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/CN2016/095716
Other languages
English (en)
Chinese (zh)
Inventor
张琬彬
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to PCT/CN2016/095716 priority Critical patent/WO2018032422A1/fr
Publication of WO2018032422A1 publication Critical patent/WO2018032422A1/fr
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U40/00—On-board mechanical arrangements for adjusting control surfaces or rotors; On-board mechanical arrangements for in-flight adjustment of the base configuration
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D31/00—Power plant control systems; Arrangement of power plant control systems in aircraft
    • B64D31/02—Initiating means
    • B64D31/06—Initiating means actuated automatically

Definitions

  • the invention relates to the field of drones, in particular to a method and a system for controlling input current of a multi-motor of a drone.
  • the drone that is, the unmanned aircraft, can be made small in size because it does not require a cockpit.
  • the existing drones are generally powered by batteries, and the existing drones cannot conduct current according to the battery power. Adjustment, resulting in a large loss of power, affecting the user's experience.
  • a control method for multi-motor input current of a drone is provided, which solves the shortcoming of low user experience in the prior art.
  • a method for controlling a multi-motor input current of a drone comprising the steps of:
  • the drone current is controlled within a current range corresponding to the wind power value.
  • the method further includes:
  • the method further includes:
  • the user is fed back to the current range and the current range is adjusted based on the feedback.
  • a control system for a multi-motor input current of a drone comprising:
  • a detecting unit for detecting a wind power value of the drone
  • a determining unit configured to determine whether the wind power value is higher than a set threshold
  • a control unit is configured to control the drone current within a current range corresponding to the wind power value.
  • system further includes:
  • a sending unit for transmitting the current range to the user.
  • system further includes:
  • the adjusting unit is configured to receive feedback from the user on the current range, and adjust the current range according to the feedback.
  • the technical solution provided by the specific embodiment of the present invention detects the wind power value of the drone.
  • the drone current is controlled within the current range corresponding to the wind power value, so the utility model has the advantages of improving the user experience. .
  • FIG. 1 is a flow chart of a method for controlling input current of a multi-motor of a drone according to the present invention
  • FIG. 2 is a structural diagram of a control system for a multi-motor input current of a drone according to the present invention.
  • FIG. 1 is a flowchart of a method for controlling input current of a multi-motor of a UAV according to a first preferred embodiment of the present invention.
  • the method is implemented by a robot, and the method is as shown in FIG. step:
  • Step S101 detecting a wind power value of the drone
  • Step S102 determining whether the wind power value is higher than a set threshold
  • Step S103 When the wind power value is higher than the set threshold, the drone current is controlled within a current range corresponding to the wind power value.
  • the technical solution provided by the specific embodiment of the present invention detects the wind power value of the drone.
  • the drone current is controlled within the current range corresponding to the wind power value, so the utility model has the advantages of improving the user experience. .
  • the foregoing method may further include:
  • the foregoing method may further include:
  • the user is fed back to the current range and the current range is adjusted based on the feedback.
  • FIG. 2 is a schematic diagram of a multi-motor input current control system for a drone according to a second preferred embodiment of the present invention.
  • the system includes:
  • a detecting unit 201 configured to detect a wind power value of the drone
  • the determining unit 202 is configured to determine whether the wind power value is higher than a set threshold
  • the control unit 203 is configured to control the drone current within a current range corresponding to the wind power value.
  • the technical solution provided by the specific embodiment of the present invention detects the wind power value of the drone.
  • the drone current is controlled within the current range corresponding to the wind power value, so the utility model has the advantages of improving the user experience. .
  • the above system may further include:
  • the sending unit 204 is configured to send the current range to the user.
  • the above system may further include:
  • the adjusting unit 205 is configured to receive feedback from the user on the current range, and adjust the current range according to the feedback.
  • Computer readable media includes both computer storage media and communication media including any medium that facilitates transfer of a computer program from one location to another.
  • a storage medium may be any available media that can be accessed by a computer.
  • the computer readable medium may include random access memory (Random) Access Memory, RAM), Read-Only Memory (ROM), Electrically Erasable Programmable Read Only Memory (Electrically Erasable Programmable Read-Only Memory, EEPROM), Compact Disc Read-Only Memory, CD-ROM, or other optical disc storage, magnetic storage medium or other magnetic storage device, or any other medium that can be used to carry or store desired program code in the form of instructions or data structures and that can be accessed by a computer. Also. Any connection may suitably be a computer readable medium.
  • a disk and a disc include a compact disc (CD), a laser disc, a compact disc, a digital versatile disc (DVD), a floppy disk, and a Blu-ray disc, wherein the disc is usually magnetically copied, and the disc is The laser is used to optically replicate the data. Combinations of the above should also be included within the scope of the computer readable media.

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)

Abstract

L'invention concerne un procédé et un système de commande du courant d'entrée de multiples moteurs d'un véhicule aérien sans pilote, le procédé comprenant les étapes suivantes : détecter une valeur de force du vent d'un véhicule aérien sans pilote (S101) ; déterminer si la valeur de force du vent est supérieure à une valeur seuil prédéfinie (S102) ; lorsque la valeur de force du vent est supérieure à la valeur seuil prédéfinie, commander un courant du véhicule aérien sans pilote de sorte que ce courant se situe dans une plage actuelle correspondant à la valeur de force du vent (S103). Le procédé et le système offrent l'avantage de conférer une bonne expérience d'utilisateur.
PCT/CN2016/095716 2016-08-17 2016-08-17 Procédé et système de commande du courant d'entrée de multiples moteurs d'un véhicule aérien sans pilote Ceased WO2018032422A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PCT/CN2016/095716 WO2018032422A1 (fr) 2016-08-17 2016-08-17 Procédé et système de commande du courant d'entrée de multiples moteurs d'un véhicule aérien sans pilote

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/CN2016/095716 WO2018032422A1 (fr) 2016-08-17 2016-08-17 Procédé et système de commande du courant d'entrée de multiples moteurs d'un véhicule aérien sans pilote

Publications (1)

Publication Number Publication Date
WO2018032422A1 true WO2018032422A1 (fr) 2018-02-22

Family

ID=61195977

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/CN2016/095716 Ceased WO2018032422A1 (fr) 2016-08-17 2016-08-17 Procédé et système de commande du courant d'entrée de multiples moteurs d'un véhicule aérien sans pilote

Country Status (1)

Country Link
WO (1) WO2018032422A1 (fr)

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2011246105A (ja) * 2010-05-27 2011-12-08 Honeywell Internatl Inc 無人飛行機のための風況推定
CN104977935A (zh) * 2014-04-04 2015-10-14 北京中科火冠科技有限公司 一种旋翼无人机风场静电喷药装置及方法
CN105157488A (zh) * 2015-09-21 2015-12-16 中国航天空气动力技术研究院 基于无人机的导弹攻击航路规划方法
CN105197243A (zh) * 2015-09-22 2015-12-30 北京农业信息技术研究中心 一种农用无人机机载变量施药系统及方法
CN105292480A (zh) * 2015-11-13 2016-02-03 南京衡创天伟无人机技术有限公司 一种多旋翼无人机喷洒系统和喷洒控制方法
CN105676866A (zh) * 2016-04-20 2016-06-15 北京博瑞爱飞科技发展有限公司 无人机的飞行控制方法和装置
CN205403847U (zh) * 2016-03-02 2016-07-27 成都翼比特自动化设备有限公司 一种用于无人机的预警装置
CN106275462A (zh) * 2016-08-12 2017-01-04 张琬彬 无人机多电机的电压分配方法及系统

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2011246105A (ja) * 2010-05-27 2011-12-08 Honeywell Internatl Inc 無人飛行機のための風況推定
CN104977935A (zh) * 2014-04-04 2015-10-14 北京中科火冠科技有限公司 一种旋翼无人机风场静电喷药装置及方法
CN105157488A (zh) * 2015-09-21 2015-12-16 中国航天空气动力技术研究院 基于无人机的导弹攻击航路规划方法
CN105197243A (zh) * 2015-09-22 2015-12-30 北京农业信息技术研究中心 一种农用无人机机载变量施药系统及方法
CN105292480A (zh) * 2015-11-13 2016-02-03 南京衡创天伟无人机技术有限公司 一种多旋翼无人机喷洒系统和喷洒控制方法
CN205403847U (zh) * 2016-03-02 2016-07-27 成都翼比特自动化设备有限公司 一种用于无人机的预警装置
CN105676866A (zh) * 2016-04-20 2016-06-15 北京博瑞爱飞科技发展有限公司 无人机的飞行控制方法和装置
CN106275462A (zh) * 2016-08-12 2017-01-04 张琬彬 无人机多电机的电压分配方法及系统

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