WO2018018982A1 - Yaw angle value calibration method and system for unmanned aerial vehicle - Google Patents

Yaw angle value calibration method and system for unmanned aerial vehicle Download PDF

Info

Publication number
WO2018018982A1
WO2018018982A1 PCT/CN2017/082975 CN2017082975W WO2018018982A1 WO 2018018982 A1 WO2018018982 A1 WO 2018018982A1 CN 2017082975 W CN2017082975 W CN 2017082975W WO 2018018982 A1 WO2018018982 A1 WO 2018018982A1
Authority
WO
WIPO (PCT)
Prior art keywords
angle value
drone
mobile terminal
yaw angle
magnetic
Prior art date
Application number
PCT/CN2017/082975
Other languages
French (fr)
Chinese (zh)
Inventor
缪志豪
Original Assignee
广州亿航智能技术有限公司
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 广州亿航智能技术有限公司 filed Critical 广州亿航智能技术有限公司
Publication of WO2018018982A1 publication Critical patent/WO2018018982A1/en

Links

Classifications

    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C21/00Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
    • G01C21/04Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by terrestrial means
    • G01C21/06Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by terrestrial means involving measuring of drift angle; involving correction for drift
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C21/00Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
    • G01C21/04Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by terrestrial means
    • G01C21/08Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by terrestrial means involving use of the magnetic field of the earth

Definitions

  • the present invention relates to the field of drone technology, and in particular, to a method and system for calibrating a yaw angle value of a drone.
  • the accuracy of the yaw angle of the UAV is generally ensured by the magnetic field sensor calibration of the UAV and the mobile terminal, respectively, and is used in various mobile terminals.
  • the accuracy of the sensor is uneven. Even after the calibration of the magnetic field sensor of many mobile terminals is completed, there is still a large deviation from the normal value.
  • the mobile terminal controls the head of the drone. There will be an angle, which makes it impossible to use the magnetic field sensor of the mobile terminal to accurately control the head orientation of the drone, which may lead to inaccurate drone control, even to the bomber.
  • a method for calibrating a yaw angle value of a drone includes the following steps:
  • the method further includes the following steps:
  • the method before the step of acquiring the first magnetic offset angle value, the method further includes the following steps:
  • the step of acquiring the first magnetic bias angle value comprises the following steps:
  • the step of acquiring the second magnetic bias angle value comprises the following steps:
  • a calibration system for a UAV yaw angle value comprising the following units:
  • a first acquiring unit configured to acquire a first magnetic bias angle value when the mobile terminal is in a preset position aligned with the drone, where the first magnetic bias angle value is a magnetic bias angle of the magnetic field sensor of the mobile terminal Value
  • a second obtaining unit configured to acquire a second magnetic bias angle value, where the second magnetic bias angle value is a magnetic bias angle value of the magnetic field sensor of the drone;
  • a compensation unit configured to calculate a difference between the first magnetic bias angle value and the second magnetic bias angle value, and add or subtract the difference value from the yaw angle value generated by the mobile terminal to obtain the compensated bias Navigation angle value;
  • a sending unit configured to send the compensated yaw angle value to the drone, wherein the drone adjusts the head orientation according to the compensated yaw angle value.
  • the system further includes an identification unit and a first determining unit;
  • the identification unit is configured to scan the drone by a photographing device of the mobile terminal, and scan the drawing Identifying the outline of the drone in the face;
  • the first determining unit is configured to determine whether the contour matches a preset contour
  • the system further includes an identification unit and a second determining unit;
  • the identification unit is configured to scan the drone by a photographing device of the mobile terminal, and identify an outline of the drone in a scan screen;
  • the second determining unit is configured to determine whether the deviation of the contour from the preset contour is within a preset range
  • the first acquiring unit is configured to initialize a magnetic field sensor of the mobile terminal, monitor sensing data of a magnetic field sensor of the mobile terminal, and acquire the first magnetic field according to the sensing data. Offset angle value.
  • the second acquiring unit acquires the second magnetic eccentricity angle value by performing wireless communication with the drone.
  • the magnetic bias angle values of the magnetic field sensors of the mobile terminal and the drone are respectively acquired, and the difference between the two is used to generate the mobile terminal
  • the yaw angle value of the operating drone is compensated, and the compensated yaw angle value is sent to the drone, and the drone adjusts the head orientation according to the compensated yaw angle value, due to the yaw angle value
  • the compensation is carried out, and the mobile terminal controls the head of the drone to face the ⁇ without the angle, which effectively improves the precision of the drone control and ensures the flight safety of the drone.
  • FIG. 1 is a schematic flow chart of a method for calibrating a yaw angle value of a drone according to an embodiment
  • FIG. 2 is a schematic view showing a practical application of a calibration method of a yaw angle value of a drone according to an embodiment
  • FIG. 3 is a schematic structural view of a calibration system of a UAV yaw angle value of one embodiment
  • FIG. 4 is a schematic structural view of a calibration system of a UAV yaw angle value of one embodiment
  • FIG. 5 is a schematic structural diagram of a calibration system of a UAV yaw angle value of one embodiment.
  • FIG. 1 a flow chart of a method for calibrating a yaw angle value of a drone according to an embodiment of the present invention is shown.
  • the method for calibrating the yaw angle value of the drone in this embodiment includes the following steps:
  • Step S101 When the mobile terminal is in a preset position aligned with the drone, the first magnetic offset angle value is obtained.
  • the first magnetic bias angle value is a magnetic bias angle value of the magnetic field sensor of the mobile terminal
  • Step S102 Acquire a second magnetic bias angle value, where the second magnetic bias angle value is a magnetic bias angle value of the magnetic field sensor of the drone;
  • Step S103 calculating a difference between the first magnetic bias angle value and the second magnetic bias angle value
  • Step S104 adding or subtracting a difference value from a yaw angle value generated by the mobile terminal to obtain a compensated yaw angle value;
  • Step S105 Send the compensated yaw angle value to the drone, wherein the drone adjusts the head orientation according to the compensated yaw angle value.
  • the magnetic bias angle values of the magnetic field sensors of the mobile terminal and the drone are respectively obtained, and the difference between the two is used to compensate the yaw angle value of the operating drone generated by the mobile terminal, and then The compensated yaw angle value is sent to the drone, and the drone adjusts the head orientation according to the compensated yaw angle value. Because the yaw angle value is compensated, the mobile terminal and the drone head are between There is no angle, which effectively improves the accuracy of drone control and ensures the flight safety of the drone.
  • the mobile terminal After obtaining the magnetic bias angle value of the magnetic field sensor of the mobile terminal and the drone, the mobile terminal is in a preset position aligned with the drone to avoid affecting the magnetic bias angle value due to the difference in position.
  • the mobile terminal includes a smart phone, a tablet, a laptop, and a personal digital assistant.
  • the calibration method of the yaw angle value of the drone is implemented by a mobile terminal provided with an APP (application), and includes the following steps: [0053] When the mobile terminal is in a preset position aligned with the drone, the APP inside the mobile terminal acquires a first magnetic bias angle value A, and the first magnetic bias angle value A is a magnetic bias of the magnetic field sensor of the mobile terminal. Angle value
  • the APP in the mobile terminal acquires a second magnetic bias angle value B, and the second magnetic bias angle value B is a magnetic bias angle value of the magnetic field sensor of the drone;
  • the APP in the mobile terminal calculates a difference D between the first magnetic deviation angle value A and the second magnetic deviation angle value B, and the difference D may be the second magnetic deviation angle value B minus the first magnetic deviation angle
  • the value of the value A may also be the value of the first magnetic bias angle value A minus the second magnetic bias angle value B;
  • the mobile terminal When the drone performs the mission in the air, the mobile terminal will generate a yaw angle C value to control the nose direction of the drone, and the APP in the mobile terminal adds the yaw angle C value to the difference D to obtain a
  • the compensated yaw angle value C is sent to the drone, wherein the drone adjusts the head orientation according to the compensated yaw angle value C'.
  • the method before the step of acquiring the first magnetic bias angle value, the method further includes the following steps: [0060] scanning the drone by the photographing device of the mobile terminal, and identifying the drone in the scan screen Outline
  • the UAV is mainly scanned by the camera of the mobile terminal, and the UAV compares the contour and the preset contour of the UAV in the scanned image in the scanned image. Whether it matches, if it matches, it means that the mobile terminal is currently in the preset position aligned with the drone.
  • the above process is essentially a dynamic identification of the drone image scanned by the camera, which ensures that the mobile terminal is in a preset position aligned with the drone quickly and conveniently.
  • the process of determining that the mobile terminal is currently in a preset position aligned with the drone may be performed in a mobile terminal side, and the preset contour may be displayed on the screen of the mobile terminal, such as displaying a no in the center of the screen.
  • the outline of the human-machine, the area in the outline of the drone is the area scanned by the camera (camera) of the mobile terminal, and after the camera scans the drone, as long as it is scanned
  • the drone is identical to the outline of the drone displayed in the center of the screen, that is, the outline of the drone in the scanned image matches the preset contour, and it can be determined that the mobile terminal is currently aligned with the drone.
  • the default location is identical to the outline of the drone displayed in the center of the screen, that is, the outline of the drone in the scanned image matches the preset contour, and it can be determined that the mobile terminal is currently aligned with the drone. The default location.
  • the step of acquiring the first magnetic bias angle value further includes the following steps: [0065] scanning the drone by the photographing device of the mobile terminal, and identifying the drone in the scan screen Outline
  • the UAV is mainly scanned by the camera of the mobile terminal, and the UAV determines the contour and the preset contour of the UAV in the scanned image in the scanned image. Whether the deviation is within a preset range, and if so, indicates that the mobile terminal is currently in a preset position aligned with the drone.
  • the above process is essentially a dynamic identification of the image of the drone scanned by the camera, which ensures that the mobile terminal is in a preset position aligned with the drone quickly and conveniently.
  • a deviation range associated with the preset contour is set in advance, and as long as the range is properly set, the calculation of the difference between the magnetic offset angle values of the mobile terminal and the drone does not cause a large error. Moreover, since the deviation range is set, it is possible to more flexibly determine that the mobile terminal is in a preset position aligned with the drone.
  • the step of obtaining the first magnetic bias angle value comprises the steps of:
  • acquiring the magnetic bias angle value of the magnetic field sensor of the mobile terminal firstly needs to initialize the magnetic field sensor of the mobile terminal, and then calculating the magnetic field of the mobile terminal according to the sensing data of the magnetic field sensor of the mobile terminal.
  • the value of the magnetic bias angle of the sensor Since the magnetic bias angle value of the magnetic field sensor may change during use due to various factors, after determining that the mobile terminal is in a preset position aligned with the drone, the magnetic field sensor that initializes the mobile terminal can acquire the latest one.
  • the magnetic bias angle value of the magnetic field sensor eliminates the influence of various factors during the use of the magnetic field sensor.
  • the step of obtaining the second magnetic bias angle value comprises the steps of:
  • the drone has a wireless communication function, and can perform the magnetic declination of its own magnetic field sensor.
  • the degree value is sent out by wireless communication, and the external device can obtain the magnetic bias angle value of the magnetic field sensor of the drone by wirelessly communicating with the drone, and does not need to be wired to the drone, which can be very Quickly and easily obtain the magnetic bias angle value of the magnetic field sensor of the drone.
  • the calibration method of the yaw angle value of the drone can be applied to the mobile phone application software.
  • the mobile terminal can be a magnetic field sensor of the mobile phone, the mobile terminal, and the drone. Both can be magnetic compasses, and users can control the application software of the drone in the mobile phone.
  • the application software has the UAV yaw angle value calibration function, and the magnetic compass assists the calibration interface.
  • the magnetic compass assists the calibration interface to display the outline of a drone. The user places the mobile phone above the drone, and the front end of the mobile phone body is aligned with the head of the drone, and the drone is flat.
  • the camera of the mobile phone is aimed at the drone, and the UAV is scanned in real time.
  • the UAV shape and the magnetic compass assisted calibration interface in the screen scanned by the mobile phone The outline of the displayed drone matches, and the handset is in alignment with the drone.
  • the application software initializes the magnetic compass of the mobile phone, monitors the data related to the magnetic compass, and calculates the magnetic declination of the magnetic compass, and then wirelessly communicates with the drone.
  • the front end of the mobile phone represents the head direction of the drone. The specific operation is as follows. Initially, if the user holds the mobile phone, the screen level Upward, the front end of the mobile phone is facing the front of the user (assuming the north direction), and the head direction of the corresponding aircraft is also facing the front of the user (north direction).
  • the corresponding aircraft's nose will also rotate in its horizontal plane until it points in the west direction.
  • the nose of the corresponding aircraft will also rotate in the plane in which it is located until pointing The northwest is 45 degrees.
  • the scheme compensates for the yaw angle.
  • the mobile phone controls the head of the drone to face the ⁇ , there is no angle, which effectively improves the accuracy of the drone control and ensures the flight safety of the drone.
  • the present invention also provides a calibration system for the yaw angle value of the unmanned aerial vehicle, and the following is an implementation of the calibration system for the yaw angle value of the unmanned aerial vehicle of the present invention.
  • FIG. 3 it is a schematic structural view of a calibration system for a yaw angle value of an unmanned aerial vehicle according to an embodiment of the present invention.
  • the calibration system for the yaw angle value of the drone in this embodiment includes the following units:
  • the first obtaining unit 210 is configured to acquire a first magnetic bias angle value when the mobile terminal is in a preset position aligned with the drone, and the first magnetic bias angle value is a magnetic bias of the magnetic field sensor of the mobile terminal. Angle value
  • the second obtaining unit 220 is configured to obtain a second magnetic bias angle value, where the second magnetic bias angle value is a magnetic bias angle value of the magnetic field sensor of the drone;
  • the compensation unit 230 is configured to calculate a difference between the first magnetic bias angle value and the second magnetic bias angle value, and add or subtract the difference value from the yaw angle value generated by the mobile terminal to obtain the compensated Yaw angle value;
  • the sending unit 240 is configured to send the compensated yaw angle value to the drone, wherein the drone adjusts the head orientation according to the compensated yaw angle value.
  • the calibration system of the yaw angle value of the drone further includes an identification unit 250 and a first determining unit 260;
  • the identification unit 250 is configured to scan the drone by the photographing device of the mobile terminal, and identify the outline of the drone in the scan screen;
  • the first determining unit 260 is configured to determine whether the contour matches the preset contour, and if so, determine that the mobile terminal is currently in a preset position aligned with the drone.
  • the calibration system of the UAV yaw angle value further includes an identification unit 250 and a second determination unit 270;
  • the identification unit 250 is configured to scan the drone by the photographing device of the mobile terminal, and identify the outline of the drone in the scan screen;
  • the second determining unit 270 is configured to determine whether the deviation of the contour from the preset contour is within a preset range, and if yes, determine that the mobile terminal is currently in a preset position aligned with the drone.
  • the first obtaining unit 210 is configured to initialize a magnetic field sensor of the mobile terminal, monitor sensing data of the magnetic field sensor of the mobile terminal, and acquire a first magnetic bias angle value according to the sensing data.
  • the second acquisition unit 220 acquires the second magnetic bias angle value by wirelessly communicating with the drone.
  • the calibration system for the yaw angle value of the UAV of the present invention and the calibrator of the yaw angle value of the UAV of the present invention are all applicable to the embodiment of the UAV yaw angle value calibration system.
  • the method and system for calibrating the yaw angle value of the unmanned aerial vehicle according to the present invention which are respectively obtaining the magnetic eccentricity angle values of the magnetic field sensors of the mobile terminal and the drone, and generating the mobile terminal by using the difference between the two
  • the yaw angle value of the operating drone is compensated, and the compensated yaw angle value is sent to the drone, and the drone adjusts the head orientation according to the compensated yaw angle value, due to the yaw angle value
  • the compensation is carried out, and the mobile terminal controls the head of the drone to face the ⁇ without the angle, which effectively improves the precision of the drone control and ensures the flight safety of the drone.

Abstract

A yaw angle value calibration method and system for an unmanned aerial vehicle. The method comprises acquiring the magnetic declination value of both a mobile terminal and an unmanned aerial vehicle, using the difference between the two magnetic declination values to compensate a yaw angle value generated by the mobile terminal for operating the unmanned aerial vehicle, then sending the compensated yaw angle value to the unmanned aerial vehicle, the unmanned aerial vehicle adjusting the orientation of the nose according to the compensated yaw angle value. As the yaw angle value is compensated for, an included angle does not exist when the mobile terminal controls the orientation of the unmanned aerial vehicle nose, effectively improving the control accuracy of the unmanned aerial vehicle and ensuring the safe flight thereof.

Description

无人机偏航角度值的校准方法和系统 技术领域  Calibration method and system for yaw angle value of drone
[0001] 本发明涉及无人机技术领域, 特别是涉及一种无人机偏航角度值的校准方法和 系统。  [0001] The present invention relates to the field of drone technology, and in particular, to a method and system for calibrating a yaw angle value of a drone.
背景技术  Background technique
[0002] 在无人机技术领域中, 目前一般通过分别对无人机和移动终端进行磁场传感器 校准来保证移动终端控制无人机吋偏航角的精准性, 而各种移动终端中使用的 传感器精度参差不齐, 甚至于很多移动终端的磁场传感器校准完成后和正常值 还是有较大偏差, 当移动终端和无人机的磁场传感器精度不一致吋, 移动终端 控制无人机机头朝向吋会存在一个夹角, 从而导致无法利用移动终端的磁场传 感器精准地控制无人机的机头朝向, 由此会引发无人机控制不精准, 甚至于炸 机。  [0002] In the field of UAV technology, the accuracy of the yaw angle of the UAV is generally ensured by the magnetic field sensor calibration of the UAV and the mobile terminal, respectively, and is used in various mobile terminals. The accuracy of the sensor is uneven. Even after the calibration of the magnetic field sensor of many mobile terminals is completed, there is still a large deviation from the normal value. When the accuracy of the magnetic field sensor of the mobile terminal and the drone is inconsistent, the mobile terminal controls the head of the drone. There will be an angle, which makes it impossible to use the magnetic field sensor of the mobile terminal to accurately control the head orientation of the drone, which may lead to inaccurate drone control, even to the bomber.
技术问题  technical problem
[0003] 基于此, 有必要针对传统的利用移动终端的磁场传感器无法精准地控制无人机 的机头朝向的问题, 提供一种无人机偏航角度值的校准方法和系统。  [0003] Based on this, it is necessary to provide a calibration method and system for the yaw angle value of the UAV, in view of the fact that the conventional magnetic field sensor using the mobile terminal cannot accurately control the head orientation of the UAV.
问题的解决方案  Problem solution
技术解决方案  Technical solution
[0004] 根据本发明的一个方面, 提供的一种无人机偏航角度值的校准方法, 包括以下 步骤:  [0004] According to an aspect of the invention, a method for calibrating a yaw angle value of a drone includes the following steps:
[0005] 当移动终端处于与无人机对准的预设位置吋, 获取第一磁偏角度值, 第一磁偏 角度值是移动终端的磁场传感器的磁偏角度值;  [0005] when the mobile terminal is in a preset position aligned with the drone, obtaining a first magnetic offset angle value, where the first magnetic offset angle value is a magnetic bias angle value of the magnetic field sensor of the mobile terminal;
[0006] 获取第二磁偏角度值, 第二磁偏角度值是无人机的磁场传感器的磁偏角度值; [0007] 计算第一磁偏角度值与第二磁偏角度值之间的差值; [0006] acquiring a second magnetic bias angle value, where the second magnetic bias angle value is a magnetic bias angle value of the magnetic field sensor of the drone; [0007] calculating between the first magnetic bias angle value and the second magnetic bias angle value Difference
[0008] 将移动终端生成的偏航角度值加上或者减去差值, 获得补偿后的偏航角度值; [0009] 将补偿后的偏航角度值发送至无人机, 其中, 无人机根据补偿后的偏航角度值 调整机头朝向。 [0010] 优选的, 在所述获取第一磁偏角度值的步骤之前还包括以下步骤: [0008] adding or subtracting the difference value of the yaw angle value generated by the mobile terminal to obtain the compensated yaw angle value; [0009] transmitting the compensated yaw angle value to the drone, wherein, The machine adjusts the head orientation according to the compensated yaw angle value. [0010] Preferably, before the step of acquiring the first magnetic offset angle value, the method further includes the following steps:
[0011] 通过移动终端的拍摄装置对所述无人机进行扫描, 在扫描画面中识别所述无人 机的轮廓;  [0011] scanning the drone by a photographing device of the mobile terminal, and identifying an outline of the drone in a scan screen;
[0012] 判断所述轮廓是否与预设轮廓相匹配, 若是, 则确定所述移动终端当前处于与 无人机对准的预设位置。  [0012] determining whether the contour matches a preset contour, and if so, determining that the mobile terminal is currently in a preset position aligned with the drone.
[0013] 优选的, 在所述获取第一磁偏角度值的步骤之前还包括以下步骤:  [0013] Preferably, before the step of acquiring the first magnetic offset angle value, the method further includes the following steps:
[0014] 通过移动终端的拍摄装置对所述无人机进行扫描, 在扫描画面中识别所述无人 机的轮廓; [0014] scanning the drone by a photographing device of the mobile terminal, and identifying an outline of the drone in a scan screen;
[0015] 判断所述轮廓是否与预设轮廓的偏差是否在预设范围内, 若是, 则确定所述移 动终端处于与无人机对准的预设位置。  [0015] determining whether the deviation of the contour from the preset contour is within a preset range, and if yes, determining that the mobile terminal is in a preset position aligned with the drone.
[0016] 优选的, 所述获取第一磁偏角度值的步骤包括以下步骤: [0016] Preferably, the step of acquiring the first magnetic bias angle value comprises the following steps:
[0017] 初始化所述移动终端的磁场传感器, 监听所述移动终端的磁场传感器的传感数 据, 根据所述传感数据获取所述第一磁偏角度值。  And [0017] initializing a magnetic field sensor of the mobile terminal, monitoring sensing data of the magnetic field sensor of the mobile terminal, and acquiring the first magnetic bias angle value according to the sensing data.
[0018] 优选的, 所述获取第二磁偏角度值的步骤包括以下步骤: [0018] Preferably, the step of acquiring the second magnetic bias angle value comprises the following steps:
[0019] 通过与所述无人机进行无线通信来获取所述第二磁偏角度值。 [0019] acquiring the second magnetic bias angle value by wirelessly communicating with the drone.
[0020] [0020]
[0021] 根据本发明的另一个方面, 提供的一种无人机偏航角度值的校准系统, 包括以 下单元:  [0021] According to another aspect of the present invention, a calibration system for a UAV yaw angle value is provided, comprising the following units:
[0022] 第一获取单元, 用于当移动终端处于与无人机对准的预设位置吋, 获取第一磁 偏角度值, 第一磁偏角度值是移动终端的磁场传感器的磁偏角度值;  [0022] a first acquiring unit, configured to acquire a first magnetic bias angle value when the mobile terminal is in a preset position aligned with the drone, where the first magnetic bias angle value is a magnetic bias angle of the magnetic field sensor of the mobile terminal Value
[0023] 第二获取单元, 用于获取第二磁偏角度值, 第二磁偏角度值是无人机的磁场传 感器的磁偏角度值;  [0023] a second obtaining unit, configured to acquire a second magnetic bias angle value, where the second magnetic bias angle value is a magnetic bias angle value of the magnetic field sensor of the drone;
[0024] 补偿单元, 用于计算第一磁偏角度值与第二磁偏角度值之间的差值, 将移动终 端生成的偏航角度值加上或者减去差值, 获得补偿后的偏航角度值;  [0024] a compensation unit, configured to calculate a difference between the first magnetic bias angle value and the second magnetic bias angle value, and add or subtract the difference value from the yaw angle value generated by the mobile terminal to obtain the compensated bias Navigation angle value;
[0025] 发送单元, 用于将补偿后的偏航角度值发送至无人机, 其中, 无人机根据补偿 后的偏航角度值调整机头朝向。  [0025] a sending unit, configured to send the compensated yaw angle value to the drone, wherein the drone adjusts the head orientation according to the compensated yaw angle value.
[0026] 优选的, 所述系统还包括识别单元和第一判断单元;  [0026] Preferably, the system further includes an identification unit and a first determining unit;
[0027] 所述识别单元用于通过移动终端的拍摄装置对所述无人机进行扫描, 在扫描画 面中识别所述无人机的轮廓; [0027] the identification unit is configured to scan the drone by a photographing device of the mobile terminal, and scan the drawing Identifying the outline of the drone in the face;
[0028] 所述第一判断单元用于判断所述轮廓是否与预设轮廓相匹配,  [0028] the first determining unit is configured to determine whether the contour matches a preset contour,
[0029] 若是, 则确定所述移动终端当前处于与无人机对准的预设位置。 [0029] If yes, it is determined that the mobile terminal is currently in a preset position aligned with the drone.
[0030] 优选的, 所述系统还包括识别单元和第二判断单元; [0030] Preferably, the system further includes an identification unit and a second determining unit;
[0031] 所述识别单元用于通过移动终端的拍摄装置对所述无人机进行扫描, 在扫描画 面中识别所述无人机的轮廓; [0031] the identification unit is configured to scan the drone by a photographing device of the mobile terminal, and identify an outline of the drone in a scan screen;
[0032] 所述第二判断单元用于判断所述轮廓是否与预设轮廓的偏差是否在预设范围内 [0032] the second determining unit is configured to determine whether the deviation of the contour from the preset contour is within a preset range
, 若是, 则确定所述移动终端当前处于与无人机对准的预设位置。 And if so, determining that the mobile terminal is currently in a preset position aligned with the drone.
[0033] 优选的, 其中, 所述第一获取单元用于初始化所述移动终端的磁场传感器, 监 听所述移动终端的磁场传感器的传感数据, 根据所述传感数据获取所述第一磁 偏角度值。  [0033] Preferably, the first acquiring unit is configured to initialize a magnetic field sensor of the mobile terminal, monitor sensing data of a magnetic field sensor of the mobile terminal, and acquire the first magnetic field according to the sensing data. Offset angle value.
[0034] 优选的, 所述第二获取单元通过与所述无人机进行无线通信来获取所述第二磁 偏角度值。  [0034] Preferably, the second acquiring unit acquires the second magnetic eccentricity angle value by performing wireless communication with the drone.
发明的有益效果  Advantageous effects of the invention
有益效果  Beneficial effect
[0035] 根据上述本发明的无人机偏航角度值的校准方法和系统, 其是分别获取移动终 端和无人机的磁场传感器的磁偏角度值, 利用两者的差值对移动终端生成的操 作无人机的偏航角度值进行补偿, 再将补偿后的偏航角度值发送至无人机, 无 人机根据补偿后的偏航角度值调整机头朝向, 由于对偏航角度值进行了补偿, 移动终端控制无人机机头朝向吋就不存在夹角, 有效提高了无人机控制的精准 度, 保证无人机的飞行安全。  [0035] According to the above-described method and system for calibrating the yaw angle value of the unmanned aerial vehicle, the magnetic bias angle values of the magnetic field sensors of the mobile terminal and the drone are respectively acquired, and the difference between the two is used to generate the mobile terminal The yaw angle value of the operating drone is compensated, and the compensated yaw angle value is sent to the drone, and the drone adjusts the head orientation according to the compensated yaw angle value, due to the yaw angle value The compensation is carried out, and the mobile terminal controls the head of the drone to face the 吋 without the angle, which effectively improves the precision of the drone control and ensures the flight safety of the drone.
对附图的简要说明  Brief description of the drawing
附图说明  DRAWINGS
[0036] 图 1为其中-一个实施例的无人机偏航角度值的校准方法的流程示意图;  1 is a schematic flow chart of a method for calibrating a yaw angle value of a drone according to an embodiment;
[0037] 图 2为其中-一个实施例的无人机偏航角度值的校准方法的实际应用示意图; 2 is a schematic view showing a practical application of a calibration method of a yaw angle value of a drone according to an embodiment;
[0038] 图 3为其中-一个实施例的无人机偏航角度值的校准系统的结构示意图; 3 is a schematic structural view of a calibration system of a UAV yaw angle value of one embodiment;
[0039] 图 4为其中-一个实施例的无人机偏航角度值的校准系统的结构示意图;  4 is a schematic structural view of a calibration system of a UAV yaw angle value of one embodiment; [0039] FIG.
[0040] 图 5为其中-一个实施例的无人机偏航角度值的校准系统的结构示意图。 本发明的实施方式 [0040] FIG. 5 is a schematic structural diagram of a calibration system of a UAV yaw angle value of one embodiment. Embodiments of the invention
[0041] 为使本发明的目的、 技术方案及优点更加清楚明白, 以下结合附图及实施例, 对本发明进行进一步的详细说明。 应当理解, 此处所描述的具体实施方式仅仅 用以解释本发明, 并不限定本发明的保护范围。  The present invention will be further described in detail below with reference to the accompanying drawings and embodiments. It is understood that the specific embodiments described herein are merely illustrative of the invention and are not intended to limit the scope of the invention.
[0042] 参见图 1所示, 为本发明一个实施例中无人机偏航角度值的校准方法的流程示 意图。 该实施例中的无人机偏航角度值的校准方法包括以下步骤:  [0042] Referring to FIG. 1, a flow chart of a method for calibrating a yaw angle value of a drone according to an embodiment of the present invention is shown. The method for calibrating the yaw angle value of the drone in this embodiment includes the following steps:
[0043] 步骤 S101 : 当移动终端处于与无人机对准的预设位置吋, 获取第一磁偏角度值 [0043] Step S101: When the mobile terminal is in a preset position aligned with the drone, the first magnetic offset angle value is obtained.
, 第一磁偏角度值是移动终端的磁场传感器的磁偏角度值; The first magnetic bias angle value is a magnetic bias angle value of the magnetic field sensor of the mobile terminal;
[0044] 步骤 S102: 获取第二磁偏角度值, 第二磁偏角度值是无人机的磁场传感器的磁 偏角度值;  [0044] Step S102: Acquire a second magnetic bias angle value, where the second magnetic bias angle value is a magnetic bias angle value of the magnetic field sensor of the drone;
[0045] 步骤 S103: 计算第一磁偏角度值与第二磁偏角度值之间的差值;  [0045] Step S103: calculating a difference between the first magnetic bias angle value and the second magnetic bias angle value;
[0046] 步骤 S104: 将移动终端生成的偏航角度值加上或者减去差值, 获得补偿后的偏 航角度值; [0046] Step S104: adding or subtracting a difference value from a yaw angle value generated by the mobile terminal to obtain a compensated yaw angle value;
[0047] 步骤 S105: 将补偿后的偏航角度值发送至无人机, 其中, 无人机根据补偿后的 偏航角度值调整机头朝向。  [0047] Step S105: Send the compensated yaw angle value to the drone, wherein the drone adjusts the head orientation according to the compensated yaw angle value.
[0048] 上述步骤 S101至 S104均是在移动终端中执行。  [0048] The above steps S101 to S104 are all performed in the mobile terminal.
[0049] 在本实施例中, 分别获取移动终端和无人机的磁场传感器的磁偏角度值, 利用 两者的差值对移动终端生成的操作无人机的偏航角度值进行补偿, 再将补偿后 的偏航角度值发送至无人机, 无人机根据补偿后的偏航角度值调整机头朝向, 由于对偏航角度值进行了补偿, 移动终端与无人机机头之间就不存在夹角, 有 效提高了无人机控制的精准度, 保证无人机的飞行安全。 [0049] In this embodiment, the magnetic bias angle values of the magnetic field sensors of the mobile terminal and the drone are respectively obtained, and the difference between the two is used to compensate the yaw angle value of the operating drone generated by the mobile terminal, and then The compensated yaw angle value is sent to the drone, and the drone adjusts the head orientation according to the compensated yaw angle value. Because the yaw angle value is compensated, the mobile terminal and the drone head are between There is no angle, which effectively improves the accuracy of drone control and ensures the flight safety of the drone.
[0050] 在获取移动终端与无人机的磁场传感器的磁偏角度值吋, 移动终端处于与无人 机对准的预设位置可以避免因位置的不同对磁偏角度值产生影响。  [0050] After obtaining the magnetic bias angle value of the magnetic field sensor of the mobile terminal and the drone, the mobile terminal is in a preset position aligned with the drone to avoid affecting the magnetic bias angle value due to the difference in position.
[0051] 移动终端包括智能手机 (Smart Phone) 、 平板电脑、 笔记本电脑、 个人数字助  [0051] The mobile terminal includes a smart phone, a tablet, a laptop, and a personal digital assistant.
[0052] 具体的, 无人机偏航角度值的校准方法是通过设有一 APP (应用程序) 的移动 终端来实施的, 包括以下步骤: [0053] 当移动终端处于与无人机对准的预设位置吋, 移动终端的里面的 APP获取第一 磁偏角度值 A, 第一磁偏角度值 A是移动终端的磁场传感器的磁偏角度值;[0052] Specifically, the calibration method of the yaw angle value of the drone is implemented by a mobile terminal provided with an APP (application), and includes the following steps: [0053] When the mobile terminal is in a preset position aligned with the drone, the APP inside the mobile terminal acquires a first magnetic bias angle value A, and the first magnetic bias angle value A is a magnetic bias of the magnetic field sensor of the mobile terminal. Angle value
[0054] 移动终端里的 APP获取第二磁偏角度值 B, 第二磁偏角度值 B是无人机的磁场传 感器的磁偏角度值; [0054] The APP in the mobile terminal acquires a second magnetic bias angle value B, and the second magnetic bias angle value B is a magnetic bias angle value of the magnetic field sensor of the drone;
[0055] 移动终端里的 APP计算第一磁偏角度值 A与第二磁偏角度值 B之间的差值 D, 差 值 D可以是第二磁偏角度值 B减去第一磁偏角度值 A的值, 也可以是第一磁偏角 度值 A减去第二磁偏角度值 B的值;  [0055] The APP in the mobile terminal calculates a difference D between the first magnetic deviation angle value A and the second magnetic deviation angle value B, and the difference D may be the second magnetic deviation angle value B minus the first magnetic deviation angle The value of the value A may also be the value of the first magnetic bias angle value A minus the second magnetic bias angle value B;
[0056] 当无人机在空中飞行执行任务吋移动终端将生成偏航角度 C值来控制无人机的 机头方向, 移动终端里的 APP将偏航角度 C值加上差值 D得到一个新的偏航角度 值 C', 即为以下公式: B-A=D, C+D=C ; 或者 A-B=D, C-D=C ; 此步骤为对偏 航角度值 C的补偿;  [0056] When the drone performs the mission in the air, the mobile terminal will generate a yaw angle C value to control the nose direction of the drone, and the APP in the mobile terminal adds the yaw angle C value to the difference D to obtain a The new yaw angle value C' is the following formula: BA=D, C+D=C; or AB=D, CD=C; This step is to compensate the yaw angle value C;
[0057] 将补偿后的偏航角度值 C发送至无人机, 其中, 无人机根据补偿后的偏航角度 值 C'调整机头朝向。  [0057] The compensated yaw angle value C is sent to the drone, wherein the drone adjusts the head orientation according to the compensated yaw angle value C'.
[0058] 上述过程均是在移动终端的 APP中执行。 [0058] The above processes are all performed in the APP of the mobile terminal.
[0059] 在其中一个实施例中, 在获取第一磁偏角度值的步骤之前还包括以下步骤: [0060] 通过移动终端的拍摄装置对无人机进行扫描, 在扫描画面中识别无人机的轮廓  [0059] In one embodiment, before the step of acquiring the first magnetic bias angle value, the method further includes the following steps: [0060] scanning the drone by the photographing device of the mobile terminal, and identifying the drone in the scan screen Outline
[0061] 判断轮廓是否与预设轮廓相匹配, 若是, 则确定移动终端当前处于与无人机对 准的预设位置。 [0061] determining whether the contour matches the preset contour, and if so, determining that the mobile terminal is currently in a preset position aligned with the drone.
[0062] 在本实施例中, 主要是通过移动终端的拍摄装置对无人机进行扫描, 无人机在 扫描得到的画面中, 比较无人机在扫描得到的画面中的轮廓与预设轮廓是否匹 配, 若匹配, 则表示移动终端当前处于与无人机对准的预设位置。 上述过程实 质上是对拍摄装置扫描的无人机图像进行动态识别, 可以保证快速又便捷地确 定移动终端处于与无人机对准的预设位置。  [0062] In this embodiment, the UAV is mainly scanned by the camera of the mobile terminal, and the UAV compares the contour and the preset contour of the UAV in the scanned image in the scanned image. Whether it matches, if it matches, it means that the mobile terminal is currently in the preset position aligned with the drone. The above process is essentially a dynamic identification of the drone image scanned by the camera, which ensures that the mobile terminal is in a preset position aligned with the drone quickly and conveniently.
[0063] 优选的, 确定移动终端当前处于与无人机对准的预设位置的过程可以在移动终 端一方中进行, 预设轮廓可以显示在移动终端的屏幕上, 如在屏幕中央显示一 个无人机的外形轮廓, 无人机的外形轮廓中的区域为移动终端的拍摄装置 (摄 像头) 扫描的区域, 在拍摄装置对无人机进行扫描吋, 只要扫描到的画面中的 无人机与屏幕中央显示的无人机的外形轮廓一致, 即扫描到的画面中的无人机 的轮廓与预设轮廓相匹配, 就可以确定此吋移动终端当前处于与无人机对准的 预设位置。 [0063] Preferably, the process of determining that the mobile terminal is currently in a preset position aligned with the drone may be performed in a mobile terminal side, and the preset contour may be displayed on the screen of the mobile terminal, such as displaying a no in the center of the screen. The outline of the human-machine, the area in the outline of the drone is the area scanned by the camera (camera) of the mobile terminal, and after the camera scans the drone, as long as it is scanned The drone is identical to the outline of the drone displayed in the center of the screen, that is, the outline of the drone in the scanned image matches the preset contour, and it can be determined that the mobile terminal is currently aligned with the drone. The default location.
[0064] 在其中一个实施例中, 在获取第一磁偏角度值的步骤之前还包括以下步骤: [0065] 通过移动终端的拍摄装置对无人机进行扫描, 在扫描画面中识别无人机的轮廓  [0064] In one embodiment, the step of acquiring the first magnetic bias angle value further includes the following steps: [0065] scanning the drone by the photographing device of the mobile terminal, and identifying the drone in the scan screen Outline
[0066] 判断轮廓是否与预设轮廓的偏差是否在预设范围内, 若是, 则确定移动终端处 于与无人机对准的预设位置。 [0066] determining whether the deviation of the contour from the preset contour is within a preset range, and if so, determining that the mobile terminal is in a preset position aligned with the drone.
[0067] 在本实施例中, 主要是通过移动终端的拍摄装置对无人机进行扫描, 无人机在 扫描得到的画面中, 判断无人机在扫描得到的画面中的轮廓与预设轮廓的偏差 是否在预设范围内, 若是, 则表示移动终端当前处于与无人机对准的预设位置 。 上述过程实质上是对拍摄装置扫描的无人机图像进行动态识别, 可以保证快 速又便捷地确定移动终端处于与无人机对准的预设位置。 另外, 本实施例中, 预先设置了一个与预设轮廓关联的偏差范围, 只要这一范围设置合适, 并不会 对移动终端和无人机的磁偏角度值的差值计算产生较大误差, 而且由于设置了 偏差范围, 可以更加灵活地确定移动终端处于与无人机对准的预设位置。  [0067] In this embodiment, the UAV is mainly scanned by the camera of the mobile terminal, and the UAV determines the contour and the preset contour of the UAV in the scanned image in the scanned image. Whether the deviation is within a preset range, and if so, indicates that the mobile terminal is currently in a preset position aligned with the drone. The above process is essentially a dynamic identification of the image of the drone scanned by the camera, which ensures that the mobile terminal is in a preset position aligned with the drone quickly and conveniently. In addition, in this embodiment, a deviation range associated with the preset contour is set in advance, and as long as the range is properly set, the calculation of the difference between the magnetic offset angle values of the mobile terminal and the drone does not cause a large error. Moreover, since the deviation range is set, it is possible to more flexibly determine that the mobile terminal is in a preset position aligned with the drone.
[0068] 在其中一个实施例中, 获取第一磁偏角度值的步骤包括以下步骤:  [0068] In one of the embodiments, the step of obtaining the first magnetic bias angle value comprises the steps of:
[0069] 初始化移动终端的磁场传感器, 监听移动终端的磁场传感器的传感数据, 根据 传感数据获取第一磁偏角度值。  And [0069] initializing the magnetic field sensor of the mobile terminal, monitoring the sensing data of the magnetic field sensor of the mobile terminal, and acquiring the first magnetic deviation angle value according to the sensing data.
[0070] 在本实施例中, 获取移动终端的磁场传感器的磁偏角度值, 首先需要对移动终 端的磁场传感器进行初始化, 之后根据移动终端的磁场传感器的传感数据可以 计算获得移动终端的磁场传感器的磁偏角度值。 由于磁场传感器的磁偏角度值 可能因各种因素而在使用过程中产生变化, 因此, 在确定移动终端处于与无人 机对准的预设位置后, 初始化移动终端的磁场传感器可以获取最新的磁场传感 器的磁偏角度值, 排除之前磁场传感器使用过程中各种因素的影响。  [0070] In this embodiment, acquiring the magnetic bias angle value of the magnetic field sensor of the mobile terminal firstly needs to initialize the magnetic field sensor of the mobile terminal, and then calculating the magnetic field of the mobile terminal according to the sensing data of the magnetic field sensor of the mobile terminal. The value of the magnetic bias angle of the sensor. Since the magnetic bias angle value of the magnetic field sensor may change during use due to various factors, after determining that the mobile terminal is in a preset position aligned with the drone, the magnetic field sensor that initializes the mobile terminal can acquire the latest one. The magnetic bias angle value of the magnetic field sensor eliminates the influence of various factors during the use of the magnetic field sensor.
[0071] 在其中一个实施例中, 获取第二磁偏角度值的步骤包括以下步骤:  [0071] In one of the embodiments, the step of obtaining the second magnetic bias angle value comprises the steps of:
[0072] 通过与无人机进行无线通信来获取第二磁偏角度值。  [0072] Acquiring a second magnetic bias angle value by wirelessly communicating with the drone.
[0073] 在本实施例中, 无人机具备无线通信功能, 可以将自身的磁场传感器的磁偏角 度值以无线通信的方式发送出去, 外部设备通过与无人机进行无线通信就可以 获取无人机的磁场传感器的磁偏角度值, 无需与无人机进行有线连接, 以此种 方式可以非常方便快捷地获取无人机的磁场传感器的磁偏角度值。 [0073] In this embodiment, the drone has a wireless communication function, and can perform the magnetic declination of its own magnetic field sensor. The degree value is sent out by wireless communication, and the external device can obtain the magnetic bias angle value of the magnetic field sensor of the drone by wirelessly communicating with the drone, and does not need to be wired to the drone, which can be very Quickly and easily obtain the magnetic bias angle value of the magnetic field sensor of the drone.
[0074] 在一个具体的实施例中, 无人机偏航角度值的校准方法可以应用在手机应用软 件中, 如图 2所示, 移动终端可以为手机, 移动终端和无人机的磁场传感器均可 以为磁罗盘, 用户打幵手机中用于控制无人机的应用软件, 该应用软件具备无 人机偏航角度值校准功能, 打幵磁罗盘辅助校准界面, 此吋的手机摄像头打幵 , 此吋磁罗盘辅助校准界面中显示有一个无人机的外形轮廓, 用户将手机放至 无人机的上方, 手机机身前端的朝向与无人机机头的朝向一致, 无人机平放在 地面上, 手机的摄像头对准无人机, 对无人机进行实吋扫描, 当手机移动到某 一位置吋, 手机扫描到的画面中的无人机外形与磁罗盘辅助校准界面中显示的 无人机的外形轮廓相吻合, 此吋手机就处于与无人机对准的位置。 手机处于与 无人机对准的位置后, 应用软件对手机的磁罗盘进行初始化, 监听磁罗盘的相 关数据, 从而计算获得磁罗盘的磁偏角, 再通过与无人机进行无线通信的方式 获取无人机的磁偏角; 根据手机的磁罗盘的磁偏角和无人机的磁罗盘的磁偏角 的差值对发送给无人机的偏航角度进行补偿; 偏航角度是用于控制无人机的机 头朝向的, 偏航角度的一个重要参数为磁偏角, 手机的前端代表着无人机的机 头方向, 具体操作如下, 初始吋, 若用户手持手机, 屏幕水平朝上, 手机的前 端朝向用户前方 (假设为正北方向) , 则对应的飞行器的机头方向也朝向用户 的前方 (正北方向) 接下来, 若用户将手机在水平面内转动, 使其前端指向用 户的左手方向 (即正西方向) , 则对应的飞行器的机头也将在其所在的水平面 内转动直到指向正西方向) ; 或者, 若用户将手机在水平面内转动, 使其前端 指向用户的左前方 45度的方向 (即西北向 45度) , 则对应的飞行器的机头也将 在其所在的平面内转动直到指向西北向 45度。 本方案对偏航角度进行了补偿, 手机控制无人机机头朝向吋就不存在夹角, 有效提高了无人机控制的精准度, 保证无人机的飞行安全。  [0074] In a specific embodiment, the calibration method of the yaw angle value of the drone can be applied to the mobile phone application software. As shown in FIG. 2, the mobile terminal can be a magnetic field sensor of the mobile phone, the mobile terminal, and the drone. Both can be magnetic compasses, and users can control the application software of the drone in the mobile phone. The application software has the UAV yaw angle value calibration function, and the magnetic compass assists the calibration interface. The magnetic compass assists the calibration interface to display the outline of a drone. The user places the mobile phone above the drone, and the front end of the mobile phone body is aligned with the head of the drone, and the drone is flat. Placed on the ground, the camera of the mobile phone is aimed at the drone, and the UAV is scanned in real time. When the mobile phone moves to a certain position, the UAV shape and the magnetic compass assisted calibration interface in the screen scanned by the mobile phone The outline of the displayed drone matches, and the handset is in alignment with the drone. After the mobile phone is in the position aligned with the drone, the application software initializes the magnetic compass of the mobile phone, monitors the data related to the magnetic compass, and calculates the magnetic declination of the magnetic compass, and then wirelessly communicates with the drone. Obtaining the magnetic declination of the drone; compensating for the yaw angle sent to the drone according to the difference between the magnetic declination of the magnetic compass of the mobile phone and the magnetic declination of the magnetic compass of the drone; the yaw angle is used In controlling the head orientation of the drone, an important parameter of the yaw angle is the magnetic declination. The front end of the mobile phone represents the head direction of the drone. The specific operation is as follows. Initially, if the user holds the mobile phone, the screen level Upward, the front end of the mobile phone is facing the front of the user (assuming the north direction), and the head direction of the corresponding aircraft is also facing the front of the user (north direction). Next, if the user rotates the mobile phone in the horizontal plane, the front end Pointing to the user's left-hand direction (ie, the west direction), the corresponding aircraft's nose will also rotate in its horizontal plane until it points in the west direction. Or, if the user rotates the phone in a horizontal plane with the front end pointing 45 degrees to the left front of the user (ie, 45 degrees northwest), the nose of the corresponding aircraft will also rotate in the plane in which it is located until pointing The northwest is 45 degrees. The scheme compensates for the yaw angle. The mobile phone controls the head of the drone to face the 吋, there is no angle, which effectively improves the accuracy of the drone control and ensures the flight safety of the drone.
[0075] 根据上述无人机偏航角度值的校准方法, 本发明还提供一种无人机偏航角度值 的校准系统, 以下就本发明的无人机偏航角度值的校准系统的实施例进行详细 说明。 [0075] According to the calibration method of the yaw angle value of the unmanned aerial vehicle, the present invention also provides a calibration system for the yaw angle value of the unmanned aerial vehicle, and the following is an implementation of the calibration system for the yaw angle value of the unmanned aerial vehicle of the present invention. Example for details Description.
[0076] 参见图 3所示, 为本发明一个实施例中无人机偏航角度值的校准系统的结构示 意图。 该实施例中的无人机偏航角度值的校准系统包括以下单元:  Referring to FIG. 3, it is a schematic structural view of a calibration system for a yaw angle value of an unmanned aerial vehicle according to an embodiment of the present invention. The calibration system for the yaw angle value of the drone in this embodiment includes the following units:
[0077] 第一获取单元 210, 用于当移动终端处于与无人机对准的预设位置吋, 获取第 一磁偏角度值, 第一磁偏角度值是移动终端的磁场传感器的磁偏角度值; [0077] The first obtaining unit 210 is configured to acquire a first magnetic bias angle value when the mobile terminal is in a preset position aligned with the drone, and the first magnetic bias angle value is a magnetic bias of the magnetic field sensor of the mobile terminal. Angle value
[0078] 第二获取单元 220, 用于获取第二磁偏角度值, 第二磁偏角度值是无人机的磁 场传感器的磁偏角度值; [0078] The second obtaining unit 220 is configured to obtain a second magnetic bias angle value, where the second magnetic bias angle value is a magnetic bias angle value of the magnetic field sensor of the drone;
[0079] 补偿单元 230, 用于计算第一磁偏角度值与第二磁偏角度值之间的差值, 将移 动终端生成的偏航角度值加上或者减去差值, 获得补偿后的偏航角度值; [0079] The compensation unit 230 is configured to calculate a difference between the first magnetic bias angle value and the second magnetic bias angle value, and add or subtract the difference value from the yaw angle value generated by the mobile terminal to obtain the compensated Yaw angle value;
[0080] 发送单元 240, 用于将补偿后的偏航角度值发送至无人机, 其中, 无人机根据 补偿后的偏航角度值调整机头朝向。 [0080] The sending unit 240 is configured to send the compensated yaw angle value to the drone, wherein the drone adjusts the head orientation according to the compensated yaw angle value.
[0081] 在其中一个实施例中, 如图 4所示, 无人机偏航角度值的校准系统还包括识别 单元 250和第一判断单元 260; [0081] In one embodiment, as shown in FIG. 4, the calibration system of the yaw angle value of the drone further includes an identification unit 250 and a first determining unit 260;
[0082] 识别单元 250用于通过移动终端的拍摄装置对无人机进行扫描, 在扫描画面中 识别无人机的轮廓; [0082] The identification unit 250 is configured to scan the drone by the photographing device of the mobile terminal, and identify the outline of the drone in the scan screen;
[0083] 第一判断单元 260用于判断轮廓是否与预设轮廓相匹配, 若是, 则确定移动终 端当前处于与无人机对准的预设位置。  [0083] The first determining unit 260 is configured to determine whether the contour matches the preset contour, and if so, determine that the mobile terminal is currently in a preset position aligned with the drone.
[0084] 在其中一个实施例中, 如图 5所示, 无人机偏航角度值的校准系统还包括识别 单元 250和第二判断单元 270; [0084] In one embodiment, as shown in FIG. 5, the calibration system of the UAV yaw angle value further includes an identification unit 250 and a second determination unit 270;
[0085] 识别单元 250用于通过移动终端的拍摄装置对无人机进行扫描, 在扫描画面中 识别无人机的轮廓; [0085] The identification unit 250 is configured to scan the drone by the photographing device of the mobile terminal, and identify the outline of the drone in the scan screen;
[0086] 第二判断单元 270用于判断轮廓与预设轮廓的偏差是否在预设范围内, 若是, 则确定移动终端当前处于与无人机对准的预设位置。  [0086] The second determining unit 270 is configured to determine whether the deviation of the contour from the preset contour is within a preset range, and if yes, determine that the mobile terminal is currently in a preset position aligned with the drone.
[0087] 在其中一个实施例中, 第一获取单元 210用于初始化移动终端的磁场传感器, 监听移动终端的磁场传感器的传感数据, 根据传感数据获取第一磁偏角度值。 In one embodiment, the first obtaining unit 210 is configured to initialize a magnetic field sensor of the mobile terminal, monitor sensing data of the magnetic field sensor of the mobile terminal, and acquire a first magnetic bias angle value according to the sensing data.
[0088] 在其中一个实施例中, 第二获取单元 220通过与无人机进行无线通信来获取第 二磁偏角度值。 [0088] In one of the embodiments, the second acquisition unit 220 acquires the second magnetic bias angle value by wirelessly communicating with the drone.
[0089] 本发明的无人机偏航角度值的校准系统与本发明的无人机偏航角度值的校准方 法一一对应, 在上述无人机偏航角度值的校准方法的实施例阐述的技术特征及 其有益效果均适用于无人机偏航角度值的校准系统的实施例中。 [0089] The calibration system for the yaw angle value of the UAV of the present invention and the calibrator of the yaw angle value of the UAV of the present invention The technical features and the beneficial effects described in the embodiments of the above-described UAV yaw angle value calibration method are all applicable to the embodiment of the UAV yaw angle value calibration system.
[0090] 以上所述实施例的各技术特征可以进行任意的组合, 为使描述简洁, 未对上述 实施例中的各个技术特征所有可能的组合都进行描述, 然而, 只要这些技术特 征的组合不存在矛盾, 都应当认为是本说明书记载的范围。  [0090] The technical features of the above-described embodiments may be combined in any combination. For the sake of brevity of description, all possible combinations of the technical features in the above embodiments are not described, however, as long as the combination of these technical features is not There are contradictions and should be considered as the scope of this manual.
[0091] 以上所述实施例仅表达了本发明的几种实施方式, 其描述较为具体和详细, 但 并不能因此而理解为对发明专利范围的限制。 应当指出的是, 对于本领域的普 通技术人员来说, 在不脱离本发明构思的前提下, 还可以做出若干变形和改进 , 这些都属于本发明的保护范围。 因此, 本发明专利的保护范围应以所附权利 要求为准。  The above-mentioned embodiments are merely illustrative of several embodiments of the present invention, and the description thereof is more specific and detailed, but is not to be construed as limiting the scope of the invention. It should be noted that a number of variations and modifications may be made by those skilled in the art without departing from the spirit and scope of the invention. Therefore, the scope of the invention should be determined by the appended claims.
工业实用性  Industrial applicability
[0092] 根据上述本发明的无人机偏航角度值的校准方法和系统, 其是分别获取移动终 端和无人机的磁场传感器的磁偏角度值, 利用两者的差值对移动终端生成的操 作无人机的偏航角度值进行补偿, 再将补偿后的偏航角度值发送至无人机, 无 人机根据补偿后的偏航角度值调整机头朝向, 由于对偏航角度值进行了补偿, 移动终端控制无人机机头朝向吋就不存在夹角, 有效提高了无人机控制的精准 度, 保证无人机的飞行安全。  [0092] The method and system for calibrating the yaw angle value of the unmanned aerial vehicle according to the present invention, which are respectively obtaining the magnetic eccentricity angle values of the magnetic field sensors of the mobile terminal and the drone, and generating the mobile terminal by using the difference between the two The yaw angle value of the operating drone is compensated, and the compensated yaw angle value is sent to the drone, and the drone adjusts the head orientation according to the compensated yaw angle value, due to the yaw angle value The compensation is carried out, and the mobile terminal controls the head of the drone to face the 吋 without the angle, which effectively improves the precision of the drone control and ensures the flight safety of the drone.

Claims

权利要求书 Claim
一种无人机偏航角度值的校准方法, 包括以下步骤: A method for calibrating a yaw angle value of a drone includes the following steps:
当移动终端处于与无人机对准的预设位置吋, 获取第一磁偏角度值, 所述第一磁偏角度值是所述移动终端的磁场传感器的磁偏角度值; 获取第二磁偏角度值, 所述第二磁偏角度值是所述无人机的磁场传感 器的磁偏角度值; Obtaining a first magnetic bias angle value when the mobile terminal is in a preset position aligned with the drone, wherein the first magnetic bias angle value is a magnetic bias angle value of the magnetic field sensor of the mobile terminal; acquiring the second magnetic a bias value, wherein the second magnetic bias angle value is a magnetic bias angle value of the magnetic field sensor of the drone;
计算所述第一磁偏角度值与所述第二磁偏角度值之间的差值; 将所述移动终端生成的偏航角度值加上或者减去所述差值, 获得补偿 后的偏航角度值; Calculating a difference between the first magnetic bias angle value and the second magnetic bias angle value; adding or subtracting the difference value from a yaw angle value generated by the mobile terminal to obtain a compensated bias Navigation angle value;
将所述补偿后的偏航角度值发送至所述无人机, 以使得所述无人机根 据所述补偿后的偏航角度值调整机头朝向。 And transmitting the compensated yaw angle value to the drone such that the drone adjusts the head orientation according to the compensated yaw angle value.
根据权利要求 1所述的无人机偏航角度值的校准方法, 其中, 在所述 获取第一磁偏角度值的步骤之前还包括以下步骤: The method for calibrating a yaw angle value of the unmanned aerial vehicle according to claim 1, wherein the step of acquiring the first magnetic eccentricity angle value further comprises the following steps:
通过移动终端的拍摄装置对所述无人机进行扫描, 在扫描画面中识别 所述无人机的轮廓; Scanning the drone by a photographing device of the mobile terminal, and identifying an outline of the drone in a scan screen;
判断所述轮廓是否与预设轮廓相匹配, 若是, 则确定所述移动终端当 前处于与无人机对准的预设位置。 It is judged whether the contour matches the preset contour, and if so, it is determined that the mobile terminal is currently in a preset position aligned with the drone.
根据权利要求 1所述的无人机偏航角度值的校准方法, 其中, 在所述 获取第一磁偏角度值的步骤之前还包括以下步骤: The method for calibrating a yaw angle value of the unmanned aerial vehicle according to claim 1, wherein the step of acquiring the first magnetic eccentricity angle value further comprises the following steps:
通过移动终端的拍摄装置对所述无人机进行扫描, 在扫描画面中识别 所述无人机的轮廓; Scanning the drone by a photographing device of the mobile terminal, and identifying an outline of the drone in a scan screen;
判断所述轮廓是否与预设轮廓的偏差是否在预设范围内, 若是, 则确 定所述移动终端处于与无人机对准的预设位置。 It is judged whether the deviation of the contour from the preset contour is within a preset range, and if so, it is determined that the mobile terminal is in a preset position aligned with the drone.
根据权利要求 1至 3中任意一项所述的无人机偏航角度值的校准方法, 其中, 所述获取第一磁偏角度值的步骤包括以下步骤: The method for calibrating a yaw angle value of a drone according to any one of claims 1 to 3, wherein the step of acquiring the first magnetic eccentricity angle value comprises the following steps:
初始化所述移动终端的磁场传感器, 监听所述移动终端的磁场传感器 的传感数据, 根据所述传感数据获取所述第一磁偏角度值。 Initializing a magnetic field sensor of the mobile terminal, monitoring sensing data of the magnetic field sensor of the mobile terminal, and acquiring the first magnetic bias angle value according to the sensing data.
根据权利要求 1至 3中任意一项所述的无人机偏航角度值的校准方法, 其中, 所述获取第二磁偏角度值的步骤包括以下步骤: 通过与所述无人机进行无线通信来获取所述第二磁偏角度值。 The method for calibrating a yaw angle value of a drone according to any one of claims 1 to 3, The step of acquiring the second magnetic bias angle value includes the following steps: acquiring the second magnetic bias angle value by performing wireless communication with the drone.
[权利要求 6] —种无人机偏航角度值的校准系统, 包括以下单元:  [Claim 6] A calibration system for a UAV yaw angle value, comprising the following units:
第一获取单元, 用于当移动终端处于与无人机对准的预设位置吋, 获 取第一磁偏角度值, 所述第一磁偏角度值是所述移动终端的磁场传感 器的磁偏角度值;  a first acquiring unit, configured to acquire a first magnetic bias angle value when the mobile terminal is in a preset position aligned with the drone, wherein the first magnetic bias angle value is a magnetic bias of the magnetic field sensor of the mobile terminal Angle value
第二获取单元, 用于获取第二磁偏角度值, 所述第二磁偏角度值是所 述无人机的磁场传感器的磁偏角度值;  a second acquiring unit, configured to acquire a second magnetic bias angle value, where the second magnetic bias angle value is a magnetic bias angle value of the magnetic field sensor of the unmanned aerial vehicle;
补偿单元, 用于计算所述第一磁偏角度值与所述第二磁偏角度值之间 的差值, 将所述移动终端生成的偏航角度值加上或者减去所述差值, 获得补偿后的偏航角度值;  a compensation unit, configured to calculate a difference between the first magnetic bias angle value and the second magnetic bias angle value, and add or subtract the difference value from a yaw angle value generated by the mobile terminal, Obtaining the yaw angle value after compensation;
发送单元, 用于将补偿后的偏航角度值发送至所述无人机, 其中, 所 述无人机根据所述补偿后的偏航角度值调整机头朝向。  And a sending unit, configured to send the compensated yaw angle value to the drone, wherein the drone adjusts the head orientation according to the compensated yaw angle value.
[权利要求 7] 根据权利要求 6所述的无人机偏航角度值的校准系统, 其中, 所述系 统还包括识别单元和第一判断单元; [Claim 7] The calibration system for the yaw angle value of the unmanned aerial vehicle according to claim 6, wherein the system further comprises an identification unit and a first determination unit;
所述识别单元用于通过移动终端的拍摄装置对所述无人机进行扫描, 在扫描画面中识别所述无人机的轮廓;  The identification unit is configured to scan the drone by a photographing device of the mobile terminal, and identify an outline of the drone in a scan screen;
所述第一判断单元用于判断所述轮廓是否与预设轮廓相匹配, 若是, 则确定所述移动终端当前处于与无人机对准的预设位置。  The first determining unit is configured to determine whether the contour matches a preset contour, and if yes, determine that the mobile terminal is currently in a preset position aligned with the drone.
[权利要求 8] 根据权利要求 6所述的无人机偏航角度值的校准系统, 其中, 所述系 统还包括识别单元和第二判断单元; [Claim 8] The calibration system for the yaw angle value of the unmanned aerial vehicle according to claim 6, wherein the system further comprises an identification unit and a second determination unit;
所述识别单元用于通过移动终端的拍摄装置对所述无人机进行扫描, 在扫描画面中识别所述无人机的轮廓;  The identification unit is configured to scan the drone by a photographing device of the mobile terminal, and identify an outline of the drone in a scan screen;
所述第二判断单元用于判断所述轮廓是否与预设轮廓的偏差是否在预 设范围内, 若是, 则确定所述移动终端当前处于与无人机对准的预设 位置。  The second determining unit is configured to determine whether the deviation of the contour from the preset contour is within a preset range, and if yes, determine that the mobile terminal is currently in a preset position aligned with the drone.
[权利要求 9] 根据权利要求 6至 8中任意一项所述的无人机偏航角度值的校准系统, 其中, 所述第一获取单元用于初始化所述移动终端的磁场传感器, 监 听所述移动终端的磁场传感器的传感数据, 根据所述传感数据获取所 述第一磁偏角度值。 [Claim 9] The calibration system for the yaw angle value of the unmanned aerial vehicle according to any one of claims 6 to 8, wherein the first acquisition unit is configured to initialize a magnetic field sensor of the mobile terminal, Listening to the sensing data of the magnetic field sensor of the mobile terminal, and acquiring the first magnetic bias angle value according to the sensing data.
[权利要求 10] 根据权利要求 6至 8中任意一项所述的无人机偏航角度值的校准系统, 其中, 所述第二获取单元通过与所述无人机进行无线通信来获取所述 第二磁偏角度值。  [Claim 10] The calibration system for the yaw angle value of the unmanned aerial vehicle according to any one of claims 6 to 8, wherein the second acquisition unit acquires the wireless communication by performing wireless communication with the unmanned aerial vehicle The second magnetic bias angle value is described.
PCT/CN2017/082975 2016-07-26 2017-05-04 Yaw angle value calibration method and system for unmanned aerial vehicle WO2018018982A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CN201610602339.8A CN107655470B (en) 2016-07-26 2016-07-26 Method and system for calibrating yaw angle value of unmanned aerial vehicle
CN201610602339.8 2016-07-26

Publications (1)

Publication Number Publication Date
WO2018018982A1 true WO2018018982A1 (en) 2018-02-01

Family

ID=61016303

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/CN2017/082975 WO2018018982A1 (en) 2016-07-26 2017-05-04 Yaw angle value calibration method and system for unmanned aerial vehicle

Country Status (2)

Country Link
CN (2) CN107655470B (en)
WO (1) WO2018018982A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112985461A (en) * 2021-03-25 2021-06-18 成都纵横自动化技术股份有限公司 Magnetic sensor calibration method based on GNSS direction finding

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107655470B (en) * 2016-07-26 2020-02-21 广州亿航智能技术有限公司 Method and system for calibrating yaw angle value of unmanned aerial vehicle
CN111795673A (en) * 2020-07-09 2020-10-20 杭州海康微影传感科技有限公司 Azimuth angle display method and device
CN113055598B (en) * 2021-03-25 2022-08-05 浙江商汤科技开发有限公司 Orientation data compensation method and device, electronic equipment and readable storage medium

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20090076665A1 (en) * 2007-09-14 2009-03-19 Hoisington Zachary C Method and System to Control Operation of a Device Using an Integrated Simulation with a Time Shift Option
CN102650887A (en) * 2011-02-25 2012-08-29 鸿富锦精密工业(深圳)有限公司 Unmanned flying carrier and method for adjusting control signals thereof
CN102650884A (en) * 2011-02-25 2012-08-29 鸿富锦精密工业(深圳)有限公司 Controller and method for adjusting control signals by utilizing controller
US20120221180A1 (en) * 2011-02-24 2012-08-30 Hon Hai Precision Industry Co., Ltd. Unmanned aerial vehicle and control method thereof
CN105717930A (en) * 2016-01-19 2016-06-29 深圳一电科技有限公司 Method, device and system for controlling drone
CN105739514A (en) * 2016-03-23 2016-07-06 普宙飞行器科技(深圳)有限公司 Operation and control method of unmanned aerial vehicle and unmanned aerial vehicle system

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE9900113L (en) * 1999-01-18 2000-05-02 Saab Ab Method and apparatus for calculating the reserve attitude and the reserve price for an aircraft
EP2511781A1 (en) * 2011-04-14 2012-10-17 Hexagon Technology Center GmbH Method and system for controlling an unmanned aircraft
CN102785780B (en) * 2011-05-19 2016-06-08 鸿富锦精密工业(深圳)有限公司 Unmanned vehicle Controlling System and method
WO2013033756A1 (en) * 2011-09-06 2013-03-14 Leica Geosystems Ag A method and system of determining an inertial sensor orientation offset
US9476734B2 (en) * 2013-03-15 2016-10-25 Innovative Solutions And Support, Inc. Systems and methods for calibrating and adjusting a heading reference system
US9157747B2 (en) * 2013-03-15 2015-10-13 Innovative Solutions And Support, Inc. Method of calibrating a heading reference system
CN103487052B (en) * 2013-09-17 2016-05-04 哈尔滨工程大学 A kind of aircraft attitude measurement method based on Magnetic Sensor combination
US9939532B2 (en) * 2015-01-09 2018-04-10 Honeywell International Inc. Heading for a hybrid navigation solution based on magnetically calibrated measurements
CN104808675B (en) * 2015-03-03 2018-05-04 广州亿航智能技术有限公司 Body-sensing flight control system and terminal device based on intelligent terminal
CN104906805B (en) * 2015-06-03 2017-05-17 南京邮电大学 Safe remote model aerocraft control method and safe remote model aerocraft control system based on active attitude detection
CN105278541B (en) * 2015-09-02 2018-08-17 盐城智博科技有限公司 A kind of aircraft auxiliary landing control method and system
CN105148541A (en) * 2015-10-15 2015-12-16 王丽芸 Remote control flight toy and remote control flight method
CN105511484A (en) * 2015-11-27 2016-04-20 深圳一电航空技术有限公司 Method and device for controlling unmanned plane to fly stably
CN105468013A (en) * 2016-01-08 2016-04-06 丁云广 Method of controlling mini unmanned aerial vehicle by embedded device
CN105629990B (en) * 2016-01-25 2019-01-11 谭圆圆 A kind of calibration method and device of unmanned vehicle
CN107655470B (en) * 2016-07-26 2020-02-21 广州亿航智能技术有限公司 Method and system for calibrating yaw angle value of unmanned aerial vehicle
CN110672092B (en) * 2019-09-24 2021-05-25 北京理工大学 Flight path generation method for reducing magnetic interference of fixed-wing unmanned aerial vehicle platform

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20090076665A1 (en) * 2007-09-14 2009-03-19 Hoisington Zachary C Method and System to Control Operation of a Device Using an Integrated Simulation with a Time Shift Option
US20120221180A1 (en) * 2011-02-24 2012-08-30 Hon Hai Precision Industry Co., Ltd. Unmanned aerial vehicle and control method thereof
CN102650887A (en) * 2011-02-25 2012-08-29 鸿富锦精密工业(深圳)有限公司 Unmanned flying carrier and method for adjusting control signals thereof
CN102650884A (en) * 2011-02-25 2012-08-29 鸿富锦精密工业(深圳)有限公司 Controller and method for adjusting control signals by utilizing controller
CN105717930A (en) * 2016-01-19 2016-06-29 深圳一电科技有限公司 Method, device and system for controlling drone
CN105739514A (en) * 2016-03-23 2016-07-06 普宙飞行器科技(深圳)有限公司 Operation and control method of unmanned aerial vehicle and unmanned aerial vehicle system

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112985461A (en) * 2021-03-25 2021-06-18 成都纵横自动化技术股份有限公司 Magnetic sensor calibration method based on GNSS direction finding
CN112985461B (en) * 2021-03-25 2023-11-03 成都纵横自动化技术股份有限公司 GNSS direction finding based magnetic sensor calibration method

Also Published As

Publication number Publication date
CN111207736A (en) 2020-05-29
CN107655470B (en) 2020-02-21
CN107655470A (en) 2018-02-02
CN111207736B (en) 2021-11-30

Similar Documents

Publication Publication Date Title
US10942529B2 (en) Aircraft information acquisition method, apparatus and device
WO2018018982A1 (en) Yaw angle value calibration method and system for unmanned aerial vehicle
CN108351690B (en) Information processing apparatus, information processing system, and information processing method
US9631956B2 (en) Methods and systems for calibrating sensors of a computing device
CN110967024A (en) Method, device, equipment and storage medium for detecting travelable area
WO2021159529A1 (en) Mobile device, control terminal, method for measuring temperature by using infrared thermal imager in mobile device, and mobile system
US10356301B2 (en) Imaging system, angle-of-view adjustment method, and angle-of-view adjustment program
CN107925713B (en) Image pickup system and image pickup control method
CN111625764B (en) Mobile data calibration method, device, electronic equipment and storage medium
CN110146106B (en) Inertial navigation equipment calibration method and device, electronic equipment and storage medium
US10337863B2 (en) Survey system
EP3399276B1 (en) Survey system
WO2016000194A1 (en) Photographing control method, device and pan-tilt device
JP2018084528A (en) Aerial photograph surveying device and aerial photograph surveying method
JPWO2018180954A1 (en) Image processing device, growth survey image creation system and program
WO2021212278A1 (en) Data processing method and apparatus, and mobile platform and wearable device
KR20210071193A (en) Apparatus for Autonomous Driving and Method and System for calibrating Sensor thereof
JP6422077B2 (en) Overhead image display system, terminal device, and program thereof
WO2019227410A1 (en) Attitude conversion method, attitude display method, and pan-tilt system
JP5776212B2 (en) Image processing apparatus, method, program, and recording medium
WO2020062024A1 (en) Distance measurement method and device based on unmanned aerial vehicle and unmanned aerial vehicle
CN110008671B (en) Data verification method and device
WO2019127303A1 (en) Method for prompting and determining orientation of unmanned aerial vehicle, and control terminal
WO2017030694A1 (en) Camera zoom based on sensor data
US11441897B2 (en) Barometric pressure sensor calibration in an electronic device

Legal Events

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

Ref document number: 17833288

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: 17833288

Country of ref document: EP

Kind code of ref document: A1