WO2018227372A1 - Procédé et système de commande de véhicule aérien sans pilote à localisation de terminal - Google Patents

Procédé et système de commande de véhicule aérien sans pilote à localisation de terminal Download PDF

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Publication number
WO2018227372A1
WO2018227372A1 PCT/CN2017/088057 CN2017088057W WO2018227372A1 WO 2018227372 A1 WO2018227372 A1 WO 2018227372A1 CN 2017088057 W CN2017088057 W CN 2017088057W WO 2018227372 A1 WO2018227372 A1 WO 2018227372A1
Authority
WO
WIPO (PCT)
Prior art keywords
position coordinate
difference
terminal
drone
user
Prior art date
Application number
PCT/CN2017/088057
Other languages
English (en)
Chinese (zh)
Inventor
李炜
Original Assignee
深圳市伊特利网络科技有限公司
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 深圳市伊特利网络科技有限公司 filed Critical 深圳市伊特利网络科技有限公司
Priority to PCT/CN2017/088057 priority Critical patent/WO2018227372A1/fr
Publication of WO2018227372A1 publication Critical patent/WO2018227372A1/fr

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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
    • G05D1/10—Simultaneous control of position or course in three dimensions
    • 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
    • G05D1/0011—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots associated with a remote control arrangement

Definitions

  • the present invention relates to the field of communications, and in particular, to a method and system for controlling a drone of a terminal.
  • a smart phone belongs to a common device used by people every day.
  • the terminal controls the drone to automatically convert the control command according to the positional relationship, and the user experience is low.
  • a drone control method for terminal positioning is provided, which solves the shortcoming of low user experience in the prior art.
  • a drone control method for terminal positioning comprising the following steps:
  • the difference is a negative value, the user's left turn command is received, and the left turn command is replaced with a right turn command.
  • the method further includes:
  • the method further includes:
  • Calculating a height difference between the first position coordinate and the second position coordinate for example, the height difference is greater than a set threshold, prompting the user to land the drone.
  • a drone control system for terminal positioning comprising:
  • a positioning unit configured to acquire a first position coordinate of the terminal and a second position coordinate of the drone
  • a calculating unit configured to calculate a difference between an X value of the first position coordinate and a second position coordinate X value
  • the control unit is configured to receive a left turn command of the user if the difference is a negative value, and replace the left turn command with a right turn command.
  • system further includes:
  • the control unit is configured to not convert the user's control command if the difference is a positive value.
  • system further includes:
  • the control unit is configured to calculate a height difference between the first position coordinate and the second position coordinate, and if the height difference is greater than a set threshold, prompting the user to land the drone.
  • a computer readable storage medium having stored thereon a computer program, the program being executed by a processor to implement the above-described terminal positioning method.
  • a terminal comprising one or more processors, a memory, a transceiver, and one or more programs, the one or more programs being stored in the memory and configured by the Executed by one or more processors, the program including instructions for performing the steps in the drone control method of the terminal positioning described above.
  • the technical solution provided by the specific embodiment of the present invention acquires the first position coordinate of the terminal and the second position coordinate of the drone, and calculates a difference between the X value of the first position coordinate and the X value of the second position coordinate, if the difference is Negative value, receiving the user's left turn command, replacing the left turn command with the right turn command, so it has automatic conversion of the control command according to the difference of X, which is convenient for the user to control the drone, and is convenient for the user.
  • FIG. 1 is a flowchart of a method for controlling a drone of a terminal positioning according to the present invention.
  • FIG. 2 is a structural diagram of a drone control system for terminal positioning according to the present invention.
  • FIG. 3 is a schematic structural diagram of hardware of a terminal provided by the present invention.
  • FIG. 1 is a flowchart of a method for controlling a UAV of a terminal according to a first preferred embodiment of the present invention.
  • the method is implemented by a terminal.
  • the method is as shown in FIG. 1 and includes the following steps:
  • Step S101 Acquire a first position coordinate of the terminal and a second position coordinate of the drone;
  • Step S102 Calculate a difference between the X value of the first position coordinate and the X value of the second position coordinate;
  • Step S103 If the difference is a negative value, receive a left turn command of the user, and replace the left turn command with a right turn command.
  • the technical solution provided by the specific embodiment of the present invention acquires the first position coordinate of the terminal and the second position coordinate of the drone, and calculates a difference between the X value of the first position coordinate and the X value of the second position coordinate, if the difference is Negative value, receiving the user's left turn command, replacing the left turn command with the right turn command, so it has automatic conversion of the control command according to the difference of X, which is convenient for the user to control the drone, and is convenient for the user.
  • the method may further include:
  • the method may further include:
  • Calculating a height difference between the first position coordinate and the second position coordinate for example, the height difference is greater than a set threshold, prompting the user to land the drone.
  • FIG. 2 is a schematic diagram of a UAV control system for terminal positioning according to a second preferred embodiment of the present invention. As shown in FIG. 2, the system includes:
  • the positioning unit 201 is configured to acquire first coordinate coordinates of the terminal and second position coordinates of the drone;
  • the calculating unit 202 is configured to calculate a difference between the X value of the first position coordinate and the second position coordinate X value;
  • the control unit 203 is configured to receive a left turn command of the user if the difference is a negative value, and replace the left turn command with a right turn command.
  • the technical solution provided by the specific embodiment of the present invention acquires the first position coordinate of the terminal and the second position coordinate of the drone, and calculates a difference between the X value of the first position coordinate and the X value of the second position coordinate, if the difference is Negative value, receiving the user's left turn command, replacing the left turn command with the right turn command, so it has automatic conversion of the control command according to the difference of X, which is convenient for the user to control the drone, and is convenient for the user.
  • the above system may further include:
  • the control unit 203 is configured to not convert the user's control command if the difference is a positive value.
  • the above system may further include:
  • the control unit 203 is configured to calculate a height difference between the first position coordinate and the second position coordinate. If the height difference is greater than the set threshold, the user is prompted to land the drone.
  • a specific embodiment of the present invention further provides a computer readable storage medium having stored thereon a computer program, the program being executed by the processor to implement the terminal positioning control method.
  • a specific embodiment of the present invention further provides a terminal, as shown in FIG. 3, including one or more processors 302, a memory 301, a transceiver 303, and one or more programs, the one or more programs being stored in The memory is configured and executed by the one or more processors, the program including instructions for performing the steps in the drone control method of the terminal positioning described above.
  • 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)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)

Abstract

La présente invention concerne un procédé et un système de commande de véhicule aérien sans pilote à localisation de terminal, le procédé comprenant les étapes suivantes consistant : à acquérir des premières coordonnées de position d'un terminal et des secondes coordonnées de position d'un véhicule aérien sans pilote ; à calculer une différence entre une valeur X des premières coordonnées de position et une valeur X des secondes coordonnées de position ; si la différence est négative, à recevoir une instruction de virage à gauche d'utilisateur et à remplacer l'instruction de virage à gauche par une instruction de virage à droite. Les solutions techniques de la présente invention présentent l'avantage d'une bonne expérience utilisateur.
PCT/CN2017/088057 2017-06-13 2017-06-13 Procédé et système de commande de véhicule aérien sans pilote à localisation de terminal WO2018227372A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PCT/CN2017/088057 WO2018227372A1 (fr) 2017-06-13 2017-06-13 Procédé et système de commande de véhicule aérien sans pilote à localisation de terminal

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/CN2017/088057 WO2018227372A1 (fr) 2017-06-13 2017-06-13 Procédé et système de commande de véhicule aérien sans pilote à localisation de terminal

Publications (1)

Publication Number Publication Date
WO2018227372A1 true WO2018227372A1 (fr) 2018-12-20

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/CN2017/088057 WO2018227372A1 (fr) 2017-06-13 2017-06-13 Procédé et système de commande de véhicule aérien sans pilote à localisation de terminal

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WO (1) WO2018227372A1 (fr)

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105468024A (zh) * 2016-01-29 2016-04-06 北京臻迪机器人有限公司 一种无人机控制方法和装置
CN105676860A (zh) * 2016-03-17 2016-06-15 歌尔声学股份有限公司 一种可穿戴设备、无人机控制装置和控制实现方法
CN106292799A (zh) * 2016-08-25 2017-01-04 北京奇虎科技有限公司 无人机、遥控装置及其控制方法
CN106598057A (zh) * 2015-10-19 2017-04-26 鹦鹉无人机股份有限公司 适于保持驾驶命令的无人机驾驶设备以及相关控制方法

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106598057A (zh) * 2015-10-19 2017-04-26 鹦鹉无人机股份有限公司 适于保持驾驶命令的无人机驾驶设备以及相关控制方法
CN105468024A (zh) * 2016-01-29 2016-04-06 北京臻迪机器人有限公司 一种无人机控制方法和装置
CN105676860A (zh) * 2016-03-17 2016-06-15 歌尔声学股份有限公司 一种可穿戴设备、无人机控制装置和控制实现方法
CN106292799A (zh) * 2016-08-25 2017-01-04 北京奇虎科技有限公司 无人机、遥控装置及其控制方法

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