WO2018032419A1 - Procédé et système de commande de la tension de moteur interne d'un véhicule aérien sans pilote - Google Patents
Procédé et système de commande de la tension de moteur interne d'un véhicule aérien sans pilote Download PDFInfo
- Publication number
- WO2018032419A1 WO2018032419A1 PCT/CN2016/095712 CN2016095712W WO2018032419A1 WO 2018032419 A1 WO2018032419 A1 WO 2018032419A1 CN 2016095712 W CN2016095712 W CN 2016095712W WO 2018032419 A1 WO2018032419 A1 WO 2018032419A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- remaining power
- drone
- current range
- motor voltage
- current
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D31/00—Power plant control; Arrangement thereof
Definitions
- the invention relates to the field of drones, in particular to a method and a system for controlling the voltage of a motor in 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 a motor voltage in a drone is provided, which solves the disadvantage of low user experience in the prior art.
- a method of controlling a motor voltage in a drone comprising the steps of:
- the drone current is controlled within the current range corresponding to the remaining power.
- 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 motor voltage in a drone comprising:
- a detecting unit for detecting the remaining power of the drone
- a determining unit configured to determine whether the remaining power is lower than a set threshold
- the control unit is configured to control the drone current in a current range corresponding to the remaining power.
- 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 remaining power of the drone.
- the drone current is controlled within the current range corresponding to the remaining power, so that the utility model has the advantages of improving the user experience. .
- FIG. 1 is a flow chart of a method for controlling a motor voltage in a drone according to the present invention
- FIG. 2 is a structural diagram of a control system for a motor voltage in a drone according to the present invention.
- FIG. 1 is a flowchart of a method for controlling a motor voltage in a UAV according to a first preferred embodiment of the present invention.
- the method is implemented by a robot.
- the method is as shown in FIG. 1 and includes the following steps. :
- Step S101 detecting remaining power of the drone
- Step S102 determining whether the remaining power is lower than a set threshold
- Step S103 When the remaining power is lower than the set threshold, the drone current is controlled to be within a current range corresponding to the remaining power.
- the technical solution provided by the specific embodiment of the present invention detects the remaining power of the drone.
- the drone current is controlled within the current range corresponding to the remaining power, so that 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 control system of a motor voltage in a UAV according to a second preferred embodiment of the present invention.
- the system includes:
- the detecting unit 201 is configured to detect a remaining power of the drone
- the determining unit 202 is configured to determine whether the remaining power is lower than a set threshold
- the control unit 203 is configured to control the drone current within a current range corresponding to the remaining power.
- the technical solution provided by the specific embodiment of the present invention detects the remaining power of the drone.
- the drone current is controlled within the current range corresponding to the remaining power, so that 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.
Abstract
La présente invention concerne un procédé et un système de commande de la tension de moteur interne d'un véhicule aérien sans pilote, le procédé comprenant les étapes suivantes consistant : à détecter le niveau de puissance restant d'un véhicule aérien sans pilote (S101); à déterminer si le niveau de puissance restant est inférieur à une valeur seuil prédéfinie (S102); lorsque le niveau de puissance restant est inférieur à la valeur seuil prédéfinie, à commander un courant du véhicule aérien sans pilote pour qu'il soit dans une plage de courant correspondant au niveau de puissance restant (S103). La solution technique offre l'avantage d'une grande expérience utilisateur.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PCT/CN2016/095712 WO2018032419A1 (fr) | 2016-08-17 | 2016-08-17 | Procédé et système de commande de la tension de moteur interne d'un véhicule aérien sans pilote |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PCT/CN2016/095712 WO2018032419A1 (fr) | 2016-08-17 | 2016-08-17 | Procédé et système de commande de la tension de moteur interne d'un véhicule aérien sans pilote |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2018032419A1 true WO2018032419A1 (fr) | 2018-02-22 |
Family
ID=61196353
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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PCT/CN2016/095712 WO2018032419A1 (fr) | 2016-08-17 | 2016-08-17 | Procédé et système de commande de la tension de moteur interne d'un véhicule aérien sans pilote |
Country Status (1)
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WO (1) | WO2018032419A1 (fr) |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
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CN102107702A (zh) * | 2010-12-27 | 2011-06-29 | 上海鹄展大丰电动自行车制造有限公司 | 电动车行车电脑装置 |
CN202106921U (zh) * | 2011-04-02 | 2012-01-11 | 刘鸿滨 | 一种适用于电动车辆的行车电脑控制装置 |
US20130124000A1 (en) * | 2010-07-23 | 2013-05-16 | Sharp Kabushiki Kaisha | Power control network system, power control method, and power controller |
CN103701163A (zh) * | 2013-12-06 | 2014-04-02 | 深圳市大疆创新科技有限公司 | 电池、具有该电池的飞行器及电池控制方法 |
CN106081131A (zh) * | 2016-08-17 | 2016-11-09 | 张琬彬 | 无人机内电机电压的控制方法及系统 |
CN106208905A (zh) * | 2016-08-17 | 2016-12-07 | 张琬彬 | 电量控制无人机电机电流的方法及系统 |
-
2016
- 2016-08-17 WO PCT/CN2016/095712 patent/WO2018032419A1/fr active Application Filing
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20130124000A1 (en) * | 2010-07-23 | 2013-05-16 | Sharp Kabushiki Kaisha | Power control network system, power control method, and power controller |
CN102107702A (zh) * | 2010-12-27 | 2011-06-29 | 上海鹄展大丰电动自行车制造有限公司 | 电动车行车电脑装置 |
CN202106921U (zh) * | 2011-04-02 | 2012-01-11 | 刘鸿滨 | 一种适用于电动车辆的行车电脑控制装置 |
CN103701163A (zh) * | 2013-12-06 | 2014-04-02 | 深圳市大疆创新科技有限公司 | 电池、具有该电池的飞行器及电池控制方法 |
CN106081131A (zh) * | 2016-08-17 | 2016-11-09 | 张琬彬 | 无人机内电机电压的控制方法及系统 |
CN106208905A (zh) * | 2016-08-17 | 2016-12-07 | 张琬彬 | 电量控制无人机电机电流的方法及系统 |
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