WO2018028364A1 - Method and device for controlling unmanned aircraft to make return flight - Google Patents

Method and device for controlling unmanned aircraft to make return flight Download PDF

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Publication number
WO2018028364A1
WO2018028364A1 PCT/CN2017/092051 CN2017092051W WO2018028364A1 WO 2018028364 A1 WO2018028364 A1 WO 2018028364A1 CN 2017092051 W CN2017092051 W CN 2017092051W WO 2018028364 A1 WO2018028364 A1 WO 2018028364A1
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WO
WIPO (PCT)
Prior art keywords
drone
return
control signal
control
remote controller
Prior art date
Application number
PCT/CN2017/092051
Other languages
French (fr)
Chinese (zh)
Inventor
刘若鹏
栾琳
林玉娟
Original Assignee
深圳光启空间技术有限公司
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Application filed by 深圳光启空间技术有限公司 filed Critical 深圳光启空间技术有限公司
Publication of WO2018028364A1 publication Critical patent/WO2018028364A1/en

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Classifications

    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/10Simultaneous control of position or course in three dimensions
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/10Simultaneous control of position or course in three dimensions
    • G05D1/101Simultaneous control of position or course in three dimensions specially adapted for aircraft

Definitions

  • the present invention relates to the field of drone control, and in particular to a control method and apparatus for returning a drone.
  • Embodiments of the present invention provide a control method and apparatus for returning a drone to at least solve the technical problem that the current UAV has poor obstacle avoidance performance during the return flight.
  • a method for controlling a return of a drone comprising: controlling, according to a first control signal, the drone to return to a predetermined path; Receiving, in the returning process of the predetermined path, receiving a second control signal sent by the remote controller, wherein the second control signal is used to adjust the predetermined path, so that the drone avoids an obstacle; and the second control And superimposing the signal on the first control signal to obtain a superimposed control signal; and using the superimposed control signal to control the drone to return.
  • the method further includes: detecting, by the preset interval, whether the remote controller sends the second control signal; if the remote controller is detected to be sent Receiving, by the second control signal, the second control signal sent by the remote controller; if the remote controller is not detected to send the second control signal, using the first control signal, controlling the The drone returned.
  • the method further includes: generating an automatic returning trigger signal according to a predefined triggering manner; and the drone is triggered by the automatic returning triggering signal Enter the return flight process.
  • generating an automatic returning trigger signal includes at least one of: generating the automatic returning trigger signal by triggering a return mode of the remote controller; and triggering a returning button of the ground control station by triggering Generating the automatic returning trigger signal; generating the automatic returning trigger signal by detecting the detection signal of the remote controller that the power is insufficient; if the distance between the remote controller and the drone is greater than a preset distance, generating The automatic returning trigger signal; if the energy of the energy management system of the drone is lower than a preset threshold, generating the automatic returning trigger signal.
  • the method further includes: detecting a preset return mode; according to the preset The first control signal is obtained by the flight signal of the drone corresponding to the return mode.
  • the preset return mode includes any one of the following: a right angle return mode, a three-dimensional coordinate axis parabolic return mode, and a round return mode.
  • controlling the return of the drone includes one of: controlling the drone to return to a return point indicated by a position of the mast activated by the remote controller; controlling the drone to return through the remote controller Or the return point set by the ground station; controlling the drone to return to the preset fixed return point.
  • a control device for returning a drone comprising: a returning module, configured to control the drone to return to a predetermined path according to the first control signal a first receiving module, configured to receive a second control signal sent by the remote controller during the return of the drone according to the predetermined path, where the second control signal is used to adjust the predetermined path, so that The supercomputer avoids the obstacle; the superimposing module is configured to superimpose the second control signal and the first control signal to obtain a superimposed control signal, wherein the first control signal is a predetermined control to return the drone
  • the first control module is configured to control the return of the drone by using the superimposed control signal.
  • the device further includes: a detecting module, configured to detect whether the remote controller sends the second control signal every preset interval during the return of the drone; a module, configured to receive the second control signal sent by the remote controller if the remote controller detects that the second control signal is sent, where the second control module is configured to send the remote controller if the remote controller is not detected
  • the second control signal controls the drone to return using the first control signal.
  • the device further includes: a generating module, configured to generate an automatic returning trigger signal according to a preset triggering manner before the drone is in a returning process; and a triggering module, configured to trigger in the automatic returning Under the trigger of the signal, the drone enters the return flight process.
  • a generating module configured to generate an automatic returning trigger signal according to a preset triggering manner before the drone is in a returning process
  • a triggering module configured to trigger in the automatic returning Under the trigger of the signal, the drone enters the return flight process.
  • the remote controller in the process of returning the drone, if an obstacle is encountered, the remote controller sends a second control signal to the drone, and the drone control system then uses the second control signal.
  • the superimposed control signal is used to control the return of the drone, that is, the drone adds a second control signal as a fine adjustment based on the control of the first control signal.
  • the second control signal that can be sent by the remote controller and the predetermined superimposition control of superimposing the first control signal of the drone returning
  • the signal adjusts a predetermined path controlled by the first control signal, so that the drone can avoid obstacles
  • the energy margin is The requirement is relatively low, which can reduce the energy loss, thereby improving the obstacle avoidance performance of the drone during the return flight process, and solving the problem that the current drone avoidance performance of the drone during the return flight process is poor.
  • FIG. 1 is a flow chart of a control method for returning a drone according to an embodiment of the present invention
  • FIG. 2 is a flow chart of an optional method for controlling the return of a drone according to an embodiment of the present invention
  • FIG. 3 is a schematic diagram of a control device for returning a drone according to an embodiment of the invention.
  • an embodiment of a method for controlling the return of a drone is provided. It should be noted that the steps shown in the flowchart of the accompanying drawings may be in a computer such as a set of computer executable instructions. Executed in the system, and although logical sequences are shown in the flowcharts, in some cases the steps shown or described may be performed in a different order than the ones described herein.
  • FIG. 1 is a flowchart of a method for controlling the return of a drone according to an embodiment of the present invention. As shown in FIG. 1, the method includes the following steps:
  • step S102 controlling the drone to return to the predetermined path according to the first control signal
  • Step S104 receiving a second control signal sent by the remote controller during the return of the drone according to the predetermined path, wherein the second control signal is used to adjust the predetermined path, so that the drone avoids the obstacle;
  • Step S106 superimposing the second control signal and the first control signal to obtain a superimposed control signal, where the first control signal is a predetermined signal for controlling the return of the drone;
  • Step S108 using the superimposed control signal, controlling the drone to return.
  • the remote controller sends a second control signal to the drone, and the drone control system then uses the second control signal.
  • the superimposed control signal is used to control the return of the drone, that is, the drone adds a second control signal as a fine adjustment based on the control of the first control signal.
  • the second control signal that can be sent by the remote controller and the predetermined superimposition control of superimposing the first control signal of the drone returning
  • the signal adjusts a predetermined path controlled by the first control signal, so that the drone can avoid obstacles.
  • the energy balance is The requirement of quantity is relatively low, which can reduce the energy loss, thereby improving the obstacle avoidance performance of the drone during the return flight process, and solving the problem that the current drone avoidance performance of the drone during the return flight process is poor.
  • the drone can receive the second control signal sent by the remote controller, and the drone control system
  • the second control signal ie, the control signal of the remote controller
  • the superimposed control signal is used to control the flight of the drone.
  • the drone can be guaranteed to be in the process of automatic returning, and within the control range of the remote controller, when encountering an obstacle, the operator controls the aircraft using the remote controller, and the drone control system receives a control signal to the remote controller (ie, the second control signal described above), and superimposing the control signal of the remote controller and the return control signal (ie, the first control signal described above), and controlling the flight of the drone by using the superimposed signal
  • the drone can be prevented from crashing because of the inability to avoid obstacles during the return flight.
  • the method may further include: detecting, by the preset interval, whether the remote controller sends the second control signal; if detecting the remote controller sending The second control signal receives the second control signal sent by the remote controller; if the remote controller does not detect the second control signal, the first control signal is used to control the drone to return.
  • the remote controller sends a second control signal to the drone.
  • the drone control system detects whether the remote controller sends the second control signal to the drone every predetermined time interval, and if the remote controller detects that the remote control sends the second control signal, That is, during the return flight, the drone encounters an obstacle, and the drone control system receives the second control signal sent by the remote controller, and implements the second control signal and the predetermined control drone return by software programming.
  • the unmanned aerial vehicle adopts different control signals for control in the case of encountering an obstacle and not encountering an obstacle, respectively, and realizes the Intelligent and efficient control of the human-machine return process.
  • the method before the drone is in the returning process, the method further includes: generating an automatic returning trigger signal according to a preset triggering manner; and triggering the automatic returning triggering signal, the drone Enter the return flight process.
  • generating an automatic returning trigger signal includes at least one of the following: generating an automatic returning trigger signal by triggering a return mode of the remote controller; generating a returning button by triggering the ground control station Automatic returning trigger signal; generating an automatic returning trigger signal by detecting a detection signal of insufficient power of the remote controller; if the distance between the remote controller and the drone is greater than a preset distance, generating an automatic returning trigger signal; if the energy management of the drone If the energy of the system is lower than the preset threshold, an automatic return flight trigger signal is generated.
  • the trigger mode of the drone returning is diverse.
  • the auto-return trigger signal can be generated by triggering the return mode of the remote control, or by triggering the return button of the ground control station.
  • the drone control system After receiving the auto-return trigger signal, the drone control system is in the auto-return trigger signal. Under the trigger, the drone enters the returning process; when the power of the remote control is insufficient, the drone control signal is lost, the drone can be triggered to return automatically, that is, the remote controller can be detected by the detecting module installed in the remote controller.
  • the detection signal of the low battery is sent by the remote controller to the drone control system, and the automatic returning trigger signal is generated by the drone control system, and the drone enters the returning process under the trigger of the automatic returning trigger signal;
  • the drone can be triggered to automatically return to the air, that is,
  • the man-machine control system can obtain the distance between the drone and the remote controller, and generate an automatic returning trigger signal when the distance is greater than the preset distance, and the drone enters and returns under the trigger of the automatic returning trigger signal.
  • the drone has an energy management system, when the energy is below a certain threshold (that is, the above-mentioned preset threshold), it is not enough to support the automatic return of the drone, the drone can be triggered to automatically return, that is, The drone control system can be used to detect whether the energy is below a certain threshold, and when the energy is below a certain threshold, an automatic returning trigger signal is generated, and the drone enters and returns under the trigger of the automatic returning trigger signal. process.
  • a certain threshold that is, the above-mentioned preset threshold
  • the drone can be triggered to enter the returning process under the action of various triggering modes, thereby realizing the flexibility of the drone control, thereby improving the user experience.
  • the method before detecting whether the remote controller sends the second control signal every predetermined interval, the method further includes: detecting a preset return mode; according to the preset return mode Corresponding drone flight signals, the first control signal is obtained.
  • the preset return mode includes any one of the following: a right angle return mode, a three-dimensional coordinate parabola return mode, and a round return mode.
  • the drone After the drone enters the return flight process, when the drone is at the current flight altitude, or the ground station is set to the return altitude, the drone is controlled to fly to the set height, the drone The control system detects the return mode selected by the operator (ie, the preset return mode described above), and according to the flight signal corresponding to the return mode, the first control signal can be obtained, that is, the automatic return control signal is obtained.
  • the return mode selected by the operator ie, the preset return mode described above
  • the automatic return route of the aircraft is optional, and the return flight mode may be selected according to the flight environment of the vehicle, that is, the automatic return route is selected.
  • the return mode is various. It can be set at the ground station with a right-angle route, a three-axis route parabola or a circular route, etc., that is, the set return mode can be the right-angle route return mode (ie, the drone moves vertically to the setting).
  • the method ie, the return mode of the arc motion track is determined by the location of the drone, the set return position, and the position of the intermediate flight.
  • the ground station can be selected and set differently.
  • the return mode according to the selected return mode, can achieve flexible control of the drone.
  • controlling the return of the drone includes one of: controlling the drone to return to the return point indicated by the position of the mast start of the remote controller; controlling the drone to return through the remote controller Or the return point set by the ground station; control the drone to return to the preset fixed return point.
  • the drone is controlled to return, and finally the drone is controlled to return to the return point.
  • the design of the return point can be various.
  • the position where the mast of the remote controller is activated can be used as the position of the return point.
  • the user wants to set a certain point in the flight as the return point it can be designed by the remote controller or the ground station.
  • the above two return points are designed as short return points, that is, the user can redesign as needed; if the user wants to return to a fixed position every time the drone can be programmed by software, in the program Set a permanent return point.
  • a remote switch is provided with a switch to indicate whether the return point can be activated by the mast or the remote controller is set, that is, the design of the return point is switched by the switch.
  • the position activated by the mast of the remote control is used as the position of the return point, or the return point is designed by the remote controller during the flight of the drone.
  • the design of the return point is diverse, and based on the diversity of the design of the return point, the flexible control of the drone can be realized, and the user experience is improved.
  • drone in the above embodiment may also be referred to as an aircraft.
  • the embodiment may include the following steps:
  • Step S201 The drone enters a return flight process.
  • the automatic returning trigger signal may be generated according to a preset triggering manner; under the trigger of the automatic returning triggering signal, the drone enters a returning process.
  • the implementation of the automatic returning trigger signal is the same as that in the foregoing embodiment, and is not described here.
  • Step S202 Control the drone to fly to a specified height.
  • the drone is controlled to fly to the set height.
  • Step S203 Detect a return mode selected by the operator.
  • the return mode selected by the operator is the above-mentioned preset return mode, and the return mode is various, which is selected at the ground station by the operator according to the flight environment of the drone.
  • Step S204 obtaining a first flight according to a flight signal of the drone corresponding to the return mode selected by the operator. control signal.
  • the first control signal is a predetermined signal for controlling the return of the drone, that is, the automatic return control signal, the control signal of the automatic return of the drone; and the drone corresponding to the return mode selected by the operator
  • the flight signal is calculated and the first control signal is obtained.
  • Step S205 Detect whether the remote controller sends the second control signal every preset period.
  • step S206 If it is detected that the remote controller sends the second control signal, step S206 is performed; otherwise, step S207 is performed.
  • Step S206 superimposing the second control signal and the first control signal to obtain a superposition control signal.
  • step S208 is performed.
  • Step S207 using the first control signal, controlling the drone to return.
  • the first control signal is used to control the drone to return.
  • Step S208 Control the drone to return by using the superimposed control signal.
  • the superimposed control signal is used to control the flight of the drone to control the drone to avoid obstacles, and after the drone successfully avoids the obstacle, continue to control the drone flight by using the first control signal, Complete the return journey.
  • the aircraft in the flight control program for controlling the flight of the drone, if the aircraft performs the task instruction of automatic returning, the aircraft will follow the setting.
  • the return mode returns, but when the operator finds that the aircraft encounters an obstacle during the return of the aircraft, the operator can control the flight of the aircraft through the remote control.
  • the control signal of the aircraft is the remote control signal (ie, the above)
  • the second control signal is superimposed with the control signal (ie, the first control signal described above) that is automatically returned, and the superimposed signal is used to control the aircraft to return.
  • the aircraft will operate in the headless mode during the return flight with the remote control signal participating in the control, that is, the remote control signal is always used (ie, in the above embodiment)
  • the second control signal enters the direction of the nose of the cymbal in the direction of flight, so as to prevent the operator from correctly manipulating the aircraft and avoiding obstacles after failing to hit the yaw angle. The situation happened.
  • the control of the remote controller in the process of not interrupting the automatic returning, the control of the remote controller is added, the control signal of the remote controller is superimposed with the control signal of the returning, and the superimposed signal is used to control the aircraft to avoid obstacles and complete the return flight. This can prevent the drone from crashing and reduce the loss, and the same can reduce the loss of energy.
  • the device may include: a returning module 32, a first receiving module 34, a superimposing module 36, and a A control module 38.
  • the returning module 32 is configured to control the drone to return to the predetermined path according to the first control signal;
  • the first receiving module 34 is configured to receive the remote controller during the return of the drone according to the predetermined path a second control signal sent, wherein the second control signal is used to adjust a predetermined path to enable the drone to avoid obstacles
  • the superimposing module 36 is configured to superimpose the second control signal and the first control signal to obtain a superimposed control signal, where the first control signal is a predetermined signal for controlling the return of the drone;
  • the first control module 38 is configured to control the drone to return using the superimposed control signal.
  • the remote controller sends a second control signal to the drone, and the drone control system will use the second control signal.
  • the superimposed control signal is used to control the return of the drone, that is, the drone adds a second control signal as a fine adjustment based on the control of the first control signal.
  • the energy balance is The requirement of quantity is relatively low, which can reduce the energy loss, thereby improving the obstacle avoidance performance of the drone during the return flight process, and solving the problem that the current drone avoidance performance of the drone during the return flight process is poor.
  • the drone in the process of returning the drone, if an obstacle is encountered, and within the control range of the remote controller, the drone can receive the second control signal sent by the remote controller, and the drone control system Will pass the software
  • the method of programming realizes superposition of the second control signal (ie, the control signal of the remote controller) with the predetermined first control signal for controlling the return of the drone, and controls the flight of the drone by using the superimposed control signal to control the unmanned The machine avoids obstacles.
  • the drone can be guaranteed to be in the process of automatic returning, and within the control range of the remote controller, when encountering an obstacle, the operator controls the aircraft using the remote controller, and the drone control system receives a control signal to the remote controller (ie, the second control signal described above), and superimposing the control signal of the remote controller and the return control signal (ie, the first control signal described above), and controlling the flight of the drone by using the superimposed signal
  • the drone can be prevented from crashing because of the inability to avoid obstacles during the return flight.
  • the device may further include: a detecting module, configured to detect whether the remote controller sends the second control signal every preset period during the return process of the drone; a receiving module, configured to receive a second control signal sent by the remote controller if the remote controller detects that the second control signal is sent, where the second control module is configured to: if the remote controller does not detect the second control signal, A control signal controls the drone to return.
  • a detecting module configured to detect whether the remote controller sends the second control signal every preset period during the return process of the drone
  • a receiving module configured to receive a second control signal sent by the remote controller if the remote controller detects that the second control signal is sent, where the second control module is configured to: if the remote controller does not detect the second control signal, A control signal controls the drone to return.
  • the remote controller sends a second control signal to the drone.
  • the drone control system detects whether the remote control sends a second control signal to the drone every predetermined interval, and if the remote controller detects that the second control signal is sent, that is, during the return flight, the drone encounters an obstacle.
  • the UAV control system receives the second control signal sent by the remote controller, and realizes superposition of the second control signal and the predetermined first control signal for controlling the return of the drone by software programming, and uses the superposition control Signal, control the flight of the drone to control the drone to avoid obstacles, and after the drone successfully avoids the obstacle, continue to use the first control signal to control the drone flight, complete the return flight process; if no remote control is detected
  • the second control signal is sent, that is, during the return flight, if the drone does not encounter an obstacle, the first control signal is used to control the drone to return.
  • the drone in the return process of the unmanned aerial vehicle, the drone is controlled by different control signals in the case of encountering obstacles and not encountering obstacles, thereby realizing Intelligent and efficient control of the human-machine return process.
  • the apparatus may further include: a generating module, configured at the drone Before the returning process, an automatic returning trigger signal is generated according to a preset triggering manner; and a triggering module is used for triggering the returning process of the drone under the trigger of the automatic returning trigger signal.
  • the trigger mode of the drone returning is diverse.
  • the auto-return trigger signal can be generated by triggering the return mode of the remote control, or by triggering the return button of the ground control station.
  • the drone control system After receiving the auto-return trigger signal, the drone control system is in the auto-return trigger signal. Under the trigger, the drone enters the returning process; when the power of the remote control is insufficient, the drone control signal is lost, the drone can be triggered to return automatically, that is, the remote controller can be detected by the detecting module installed in the remote controller.
  • the detection signal of the low battery is sent by the remote controller to the drone control system, and the automatic returning trigger signal is generated by the drone control system, and the drone enters the returning process under the trigger of the automatic returning trigger signal;
  • the drone control signal is lost, and the drone can be automatically returned, that is, the drone control system can obtain the unmanned The distance between the machine and the remote control, and the distance is greater than the preset distance
  • the auto-return trigger signal is generated, and the drone enters the returning process under the trigger of the auto-return trigger signal; if the drone has an energy management system, the energy is below a certain threshold (ie, the above-mentioned preset threshold) In the case that it is not enough to support the automatic return of the drone, it can trigger the automatic return of the drone, that is, the drone control system can detect whether the energy is below a certain threshold and the energy is below a certain threshold. Next, an automatic returning trigger signal is generated, and the drone enters
  • the drone can be triggered to enter the returning process under the action of various triggering modes, thereby realizing the flexibility of the drone control, thereby improving the user experience.
  • the aircraft in the flight control program for controlling the flight of the drone, if the aircraft performs the task command of the automatic returning flight, the aircraft will follow the setting.
  • the return mode returns, but when the operator finds that the aircraft encounters an obstacle during the return of the aircraft, the operator can control the flight of the aircraft through the remote control.
  • the control signal of the aircraft is the remote control signal (ie, the above)
  • the second control signal is superimposed with the control signal (ie, the first control signal described above) that is automatically returned, and the superimposed signal is used to control the aircraft to return.
  • the aircraft In order to avoid the operator's loss caused by the erroneous operation in an emergency, the aircraft will operate in the headless mode during the return flight with the remote control signal participating in the control, that is, the machine always enters the ⁇ machine with the remote control signal.
  • the direction of the head is forward in the direction of flight, so as to prevent the operator from correctly manipulating the aircraft to avoid obstacles after the yaw angle is missed.
  • the disclosed technical content may be implemented in other manners.
  • the device embodiments described above are only schematic.
  • the division of the unit may be a logical function division.
  • the actual implementation may have another division manner.
  • multiple units or components may be combined or may be Integration into another system, or some features can be ignored, or not executed.
  • the mutual coupling or direct coupling or communication connection shown or discussed may be an indirect coupling or communication connection through some interface, unit or module, and may be electrical or otherwise.
  • the unit described as a separate component may or may not be physically distributed, and the component displayed as a unit may or may not be a physical unit, that is, may be located in one place, or may be distributed to multiple On the unit. Some or all of the units may be selected according to actual needs to achieve the objectives of the embodiment of the present embodiment.
  • each functional unit in each embodiment of the present invention may be integrated into one processing unit, or each unit may exist physically separately, or two or more units may be integrated into one unit.
  • the above integrated unit can be implemented in the form of hardware or in the form of a software functional unit.
  • the integrated unit if implemented in the form of a software functional unit and sold or used as a standalone product, may be stored in a computer readable storage medium.
  • the technical solution of the present invention may contribute to the prior art or all or part of the technical solution may be embodied in the form of a software product stored in a storage medium. , including a number of instructions to make a computer device (can be a personal computer, server or network All or part of the steps of the method described in the various embodiments of the invention are performed.
  • the foregoing storage medium includes: a USB flash drive, a read only memory (ROM, Read-Only)
  • RAM Random Access Memory
  • removable hard disk disk or optical disk, and other media that can store program code.

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  • 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

A method and device for controlling an unmanned aircraft to make a return flight. The method comprises: controlling, according to a first control signal, an unmanned aircraft to make a return flight in a predetermined route (S102); receiving a second control signal sent by a remote control during the process the unmanned aircraft makes the return flight in the predetermined route, the second control signal being used for adjusting the predetermined route so that the unmanned aircraft can avoid obstacles (S104); superimposing the second control signal onto the first control signal to obtain a superimposed control signal (S106); and controlling, by using the superimposed control signal, the unmanned aircraft to make a return flight (S108). By means of the method and device, the existing technical problem of low obstacle avoidance performance of an unmanned aircraft during a return flight is resolved.

Description

无人机返航的控制方法和装置  Control method and device for drone returning
技术领域  Technical field
[0001] 本发明涉及无人机控制领域, 具体而言, 涉及一种无人机返航的控制方法和装 置。  [0001] The present invention relates to the field of drone control, and in particular to a control method and apparatus for returning a drone.
背景技术  Background technique
[0002] 自动返航是目前大多数无人机都具有的一个基本功能, 该功能主要是为了防止 无人机在失控的情况下丢失, 同吋, 使用该功能可以实现无人机的稳定降落, 降低了操纵者控制的难度。 目前无人机的返航控制系统中, 当飞行器 (即无人 机) 执行返航任务吋, 遥控器信号对飞行器不起作用, 只有在中止返航任务之 后, 遥控器才能接管控制, 即遥控器信号才能起作用, 这样将降低无人机在返 航过程中的避障功能。 另外, 目前可以通过记录走过的路径原路返回的机制来 实现避障, 但是这种返航过程并不是最优路线返航, 对飞行器能源的余量要求 高。  [0002] Automatic return is a basic function of most UAVs. This function is mainly to prevent the UAV from being lost in the event of loss of control. At the same time, the function can realize the stable landing of the UAV. Reduces the difficulty of manipulator control. In the current backhaul control system of the drone, when the aircraft (ie, the drone) performs the returning mission, the remote control signal does not work for the aircraft. Only after the returning mission is suspended, the remote controller can take over the control, that is, the remote controller signal. Acting, this will reduce the obstacle avoidance function of the drone during the return flight. In addition, it is now possible to achieve obstacle avoidance by recording the path of the path that has passed through the path, but this return process is not the optimal route return, and the margin for aircraft energy is high.
技术问题  technical problem
[0003] 针对目前无人机在返航过程中避障性能差的问题, 目前尚未提出有效的解决方 案。  [0003] In view of the current problem of poor obstacle avoidance performance during the return flight of the drone, no effective solution has been proposed yet.
问题的解决方案  Problem solution
技术解决方案  Technical solution
[0004] 本发明实施例提供了一种无人机返航的控制方法和装置, 以至少解决目前无人 机在返航过程中避障性能差的技术问题。  Embodiments of the present invention provide a control method and apparatus for returning a drone to at least solve the technical problem that the current UAV has poor obstacle avoidance performance during the return flight.
[0005] 根据本发明实施例的一个方面, 提供了一种无人机返航的控制方法, 该方法包 括: 根据第一控制信号控制所述无人机按预定路径返航; 在无人机按所述预定 路径返航过程中, 接收遥控器发送的第二控制信号, 其中, 所述第二控制信号 用于调整所述预定路径, 以使所述无人机躲避障碍物; 将所述第二控制信号与 所述第一控制信号叠加, 得到叠加控制信号; 利用所述叠加控制信号, 控制所 述无人机返航。 [0006] 进一步地, 在无人机返航过程中, 所述方法还包括: 每隔预设吋间段, 检测所 述遥控器是否发送所述第二控制信号; 若检测到所述遥控器发送所述第二控制 信号, 则接收所述遥控器发送的所述第二控制信号; 若未检测到所述遥控器发 送所述第二控制信号, 则利用所述第一控制信号, 控制所述无人机返航。 [0005] According to an aspect of an embodiment of the present invention, a method for controlling a return of a drone is provided, the method comprising: controlling, according to a first control signal, the drone to return to a predetermined path; Receiving, in the returning process of the predetermined path, receiving a second control signal sent by the remote controller, wherein the second control signal is used to adjust the predetermined path, so that the drone avoids an obstacle; and the second control And superimposing the signal on the first control signal to obtain a superimposed control signal; and using the superimposed control signal to control the drone to return. [0006] Further, in the process of returning the drone, the method further includes: detecting, by the preset interval, whether the remote controller sends the second control signal; if the remote controller is detected to be sent Receiving, by the second control signal, the second control signal sent by the remote controller; if the remote controller is not detected to send the second control signal, using the first control signal, controlling the The drone returned.
[0007] 进一步地, 在无人机处于返航过程之前, 所述方法还包括: 按照预先定义的触 发方式, 生成自动返航触发信号; 在所述自动返航触发信号的触发下, 所述无 人机进入返航过程。  [0007] Further, before the drone is in the returning process, the method further includes: generating an automatic returning trigger signal according to a predefined triggering manner; and the drone is triggered by the automatic returning triggering signal Enter the return flight process.
[0008] 进一步地, 按照预先定义的触发方式, 生成自动返航触发信号至少包括如下之 一: 通过触发遥控器的返航模式幵关, 生成所述自动返航触发信号; 通过触发 地面控制站的返航按钮, 生成所述自动返航触发信号; 通过检测到所述遥控器 电量不足的检测信号, 生成所述自动返航触发信号; 如果所述遥控器与所述无 人机的距离大于预设距离, 则生成所述自动返航触发信号; 如果所述无人机的 能源管理系统的能源低于预设阈值, 则生成所述自动返航触发信号。  [0008] Further, according to the predefined triggering manner, generating an automatic returning trigger signal includes at least one of: generating the automatic returning trigger signal by triggering a return mode of the remote controller; and triggering a returning button of the ground control station by triggering Generating the automatic returning trigger signal; generating the automatic returning trigger signal by detecting the detection signal of the remote controller that the power is insufficient; if the distance between the remote controller and the drone is greater than a preset distance, generating The automatic returning trigger signal; if the energy of the energy management system of the drone is lower than a preset threshold, generating the automatic returning trigger signal.
[0009] 进一步地, 在每隔预设吋间段, 检测所述遥控器是否发送所述第二控制信号之 前, 所述方法还包括: 检测预先设置的返航方式; 按照与所述预先设置的返航 方式对应的所述无人机的飞行信号, 得到所述第一控制信号。  [0009] Further, before detecting, by the preset interval, whether the remote controller sends the second control signal, the method further includes: detecting a preset return mode; according to the preset The first control signal is obtained by the flight signal of the drone corresponding to the return mode.
[0010] 进一步地, 所述预先设置的返航方式包括如下任意一种: 直角路线返航方式、 三维坐标轴抛物线返航方式和圆形返航方式。  [0010] Further, the preset return mode includes any one of the following: a right angle return mode, a three-dimensional coordinate axis parabolic return mode, and a round return mode.
[0011] 进一步地, 控制所述无人机返航包括如下之一: 控制所述无人机返回通过遥控 器的掰杆启动的位置所指示的返航点; 控制所述无人机返回通过遥控器或地面 站设置的返航点; 控制所述无人机返回预先设定的固定返航点。  [0011] Further, controlling the return of the drone includes one of: controlling the drone to return to a return point indicated by a position of the mast activated by the remote controller; controlling the drone to return through the remote controller Or the return point set by the ground station; controlling the drone to return to the preset fixed return point.
[0012] 根据本发明实施例的另一方面, 还提供了一种无人机返航的控制装置, 该装置 包括: 返航模块, 用于根据第一控制信号控制所述无人机按预定路径返航; 第 一接收模块, 用于在无人机按所述预定路径返航过程中, 接收遥控器发送的第 二控制信号, 其中, 所述第二控制信号用于调整所述预定路径, 以使所述无人 机躲避障碍物; 叠加模块, 用于将所述第二控制信号与第一控制信号叠加, 得 到叠加控制信号, 其中, 所述第一控制信号为预定的控制所述无人机返航的信 号; 第一控制模块, 用于利用所述叠加控制信号, 控制所述无人机返航。 [0013] 进一步地, 所述装置还包括: 检测模块, 用于在无人机返航过程中, 每隔预设 吋间段, 检测所述遥控器是否发送所述第二控制信号; 第二接收模块, 用于若 检测到所述遥控器发送所述第二控制信号, 则接收所述遥控器发送的所述第二 控制信号; 第二控制模块, 用于若未检测到所述遥控器发送所述第二控制信号 , 则利用所述第一控制信号, 控制所述无人机返航。 [0012] According to another aspect of the present invention, a control device for returning a drone is provided, the device comprising: a returning module, configured to control the drone to return to a predetermined path according to the first control signal a first receiving module, configured to receive a second control signal sent by the remote controller during the return of the drone according to the predetermined path, where the second control signal is used to adjust the predetermined path, so that The supercomputer avoids the obstacle; the superimposing module is configured to superimpose the second control signal and the first control signal to obtain a superimposed control signal, wherein the first control signal is a predetermined control to return the drone The first control module is configured to control the return of the drone by using the superimposed control signal. [0013] Further, the device further includes: a detecting module, configured to detect whether the remote controller sends the second control signal every preset interval during the return of the drone; a module, configured to receive the second control signal sent by the remote controller if the remote controller detects that the second control signal is sent, where the second control module is configured to send the remote controller if the remote controller is not detected The second control signal controls the drone to return using the first control signal.
[0014] 进一步地, 所述装置还包括: 生成模块, 用于在无人机处于返航过程之前, 按 照预先定义的触发方式, 生成自动返航触发信号; 触发模块, 用于在所述自动 返航触发信号的触发下, 所述无人机进入返航过程。  [0014] Further, the device further includes: a generating module, configured to generate an automatic returning trigger signal according to a preset triggering manner before the drone is in a returning process; and a triggering module, configured to trigger in the automatic returning Under the trigger of the signal, the drone enters the return flight process.
发明的有益效果  Advantageous effects of the invention
有益效果  Beneficial effect
[0015] 在本发明实施例中, 在无人机返航过程中, 若遇到障碍物, 遥控器则发送第二 控制信号给无人机, 无人机控制系统则会将该第二控制信号与预定的控制无人 机返航的第一控制信号叠加, 利用叠加控制信号, 控制无人机返航, 即无人机 在第一控制信号所控制的基础上, 加入第二控制信号作为微调。 通过上述实施 例, 在无人机返航过程中, 且在不中断返航过程的情况下, 可以通过遥控器发 送的第二控制信号和预定的控制无人机返航的第一控制信号叠加的叠加控制信 号, 调整第一控制信号所控制的预定路径, 使得无人机可以躲避障碍物, 此外 , 与现有技术中采取原路返回的机制来实现躲避障碍物的方案相比, 对能量余 量的要求比较低, 可以减少能量损耗, 从而提高了无人机在返航过程中的避障 性能, 解决了目前无人机在返航过程中避障性能差的问题。  [0015] In the embodiment of the present invention, in the process of returning the drone, if an obstacle is encountered, the remote controller sends a second control signal to the drone, and the drone control system then uses the second control signal. Superimposed with a predetermined first control signal for controlling the return of the drone, the superimposed control signal is used to control the return of the drone, that is, the drone adds a second control signal as a fine adjustment based on the control of the first control signal. Through the above embodiment, in the return process of the drone, and without interrupting the returning process, the second control signal that can be sent by the remote controller and the predetermined superimposition control of superimposing the first control signal of the drone returning The signal adjusts a predetermined path controlled by the first control signal, so that the drone can avoid obstacles, and in addition, compared with the prior art adopting the mechanism of returning the original path to implement the obstacle avoidance scheme, the energy margin is The requirement is relatively low, which can reduce the energy loss, thereby improving the obstacle avoidance performance of the drone during the return flight process, and solving the problem that the current drone avoidance performance of the drone during the return flight process is poor.
对附图的简要说明  Brief description of the drawing
附图说明  DRAWINGS
[0016] 此处所说明的附图用来提供对本发明的进一步理解, 构成本申请的一部分, 本 发明的示意性实施例及其说明用于解释本发明, 并不构成对本发明的不当限定 。 在附图中:  The accompanying drawings are intended to provide a further understanding of the invention, and the invention is not intended to limit the invention. In the drawing:
[0017] 图 1是根据本发明实施例的一种无人机返航的控制方法的流程图;  1 is a flow chart of a control method for returning a drone according to an embodiment of the present invention;
[0018] 图 2是根据本发明实施例的一种可选的无人机返航的控制方法的流程图; 2 is a flow chart of an optional method for controlling the return of a drone according to an embodiment of the present invention;
[0019] 图 3是根据本发明实施例的一种无人机返航的控制装置的示意图。 本发明的实施方式 3 is a schematic diagram of a control device for returning a drone according to an embodiment of the invention. Embodiments of the invention
[0020] 为了使本技术领域的人员更好地理解本发明方案, 下面将结合本发明实施例中 的附图, 对本发明实施例中的技术方案进行清楚、 完整地描述, 显然, 所描述 的实施例仅仅是本发明一部分的实施例, 而不是全部的实施例。 基于本发明中 的实施例, 本领域普通技术人员在没有做出创造性劳动前提下所获得的所有其 他实施例, 都应当属于本发明保护的范围。  The technical solutions in the embodiments of the present invention will be clearly and completely described in the following with reference to the accompanying drawings in the embodiments of the present invention. The embodiments are merely a part of the embodiments of the invention, and not all of the embodiments. All other embodiments obtained by a person of ordinary skill in the art based on the embodiments of the present invention without departing from the inventive scope should fall within the scope of the present invention.
[0021] 需要说明的是, 本发明的说明书和权利要求书及上述附图中的术语"第一"、 " 第二"等是用于区别类似的对象, 而不必用于描述特定的顺序或先后次序。 应该 理解这样使用的数据在适当情况下可以互换, 以便这里描述的本发明的实施例 能够以除了在这里图示或描述的那些以外的顺序实施。 此外, 术语"包括"和"具 有"以及他们的任何变形, 意图在于覆盖不排他的包含, 例如, 包含了一系列步 骤或单元的过程、 方法、 系统、 产品或设备不必限于清楚地列出的那些步骤或 单元, 而是可包括没有清楚地列出的或对于这些过程、 方法、 产品或设备固有 的其它步骤或单元。  [0021] It should be noted that the terms "first", "second", and the like in the specification and claims of the present invention and the above drawings are used to distinguish similar objects, and are not necessarily used to describe a specific order or Prioritization. It is to be understood that the data so used may be interchanged as appropriate, so that the embodiments of the invention described herein can be implemented in a sequence other than those illustrated or described herein. In addition, the terms "comprises" and "comprising" and "comprises" and "the" are intended to cover a non-exclusive inclusion, for example, a process, method, system, product, or device that comprises a series of steps or units is not necessarily limited to Those steps or units may include other steps or units not explicitly listed or inherent to such processes, methods, products or devices.
[0022] 实施例 1  Embodiment 1
[0023] 根据本发明实施例, 提供了一种无人机返航的控制方法的实施例, 需要说明的 是, 在附图的流程图示出的步骤可以在诸如一组计算机可执行指令的计算机系 统中执行, 并且, 虽然在流程图中示出了逻辑顺序, 但是在某些情况下, 可以 以不同于此处的顺序执行所示出或描述的步骤。  [0023] According to an embodiment of the present invention, an embodiment of a method for controlling the return of a drone is provided. It should be noted that the steps shown in the flowchart of the accompanying drawings may be in a computer such as a set of computer executable instructions. Executed in the system, and although logical sequences are shown in the flowcharts, in some cases the steps shown or described may be performed in a different order than the ones described herein.
[0024] 图 1是根据本发明实施例的一种无人机返航的控制方法的流程图, 如图 1所示, 该方法包括如下步骤:  1 is a flowchart of a method for controlling the return of a drone according to an embodiment of the present invention. As shown in FIG. 1, the method includes the following steps:
[0025] 步骤 S 102, 根据第一控制信号控制无人机按预定路径返航;  [0025] step S102, controlling the drone to return to the predetermined path according to the first control signal;
[0026] 步骤 S104, 在无人机按预定路径返航过程中, 接收遥控器发送的第二控制信号 , 其中, 第二控制信号用于调整预定路径, 以使无人机躲避障碍物;  [0026] Step S104, receiving a second control signal sent by the remote controller during the return of the drone according to the predetermined path, wherein the second control signal is used to adjust the predetermined path, so that the drone avoids the obstacle;
[0027] 步骤 S106, 将第二控制信号与第一控制信号叠加, 得到叠加控制信号, 其中, 第一控制信号为预定的控制无人机返航的信号;  [0027] Step S106, superimposing the second control signal and the first control signal to obtain a superimposed control signal, where the first control signal is a predetermined signal for controlling the return of the drone;
[0028] 步骤 S 108, 利用叠加控制信号, 控制无人机返航。 [0029] 采用本发明的实施例, 在无人机返航过程中, 若遇到障碍物, 遥控器则发送第 二控制信号给无人机, 无人机控制系统则会将该第二控制信号与预定的控制无 人机返航的第一控制信号叠加, 利用叠加控制信号, 控制无人机返航, 即无人 机在第一控制信号所控制的基础上, 加入第二控制信号作为微调。 通过上述实 施例, 在无人机返航过程中, 且在不中断返航过程的情况下, 可以通过遥控器 发送的第二控制信号和预定的控制无人机返航的第一控制信号叠加的叠加控制 信号, 调整第一控制信号所控制的预定路径, 使得无人机可以躲避障碍物, 此 夕卜, 与现有技术中采取原路返回的机制来实现躲避障碍物的方案相比, 对能量 余量的要求比较低, 可以减少能量损耗, 从而提高了无人机在返航过程中的避 障性能, 解决了目前无人机在返航过程中避障性能差的问题。 [0028] Step S108, using the superimposed control signal, controlling the drone to return. [0029] With the embodiment of the present invention, in the process of returning the drone, if an obstacle is encountered, the remote controller sends a second control signal to the drone, and the drone control system then uses the second control signal. Superimposed with a predetermined first control signal for controlling the return of the drone, the superimposed control signal is used to control the return of the drone, that is, the drone adds a second control signal as a fine adjustment based on the control of the first control signal. Through the above embodiment, in the return process of the drone, and without interrupting the returning process, the second control signal that can be sent by the remote controller and the predetermined superimposition control of superimposing the first control signal of the drone returning The signal adjusts a predetermined path controlled by the first control signal, so that the drone can avoid obstacles. In addition, compared with the prior art adopting the mechanism of returning the original path to implement the obstacle avoidance scheme, the energy balance is The requirement of quantity is relatively low, which can reduce the energy loss, thereby improving the obstacle avoidance performance of the drone during the return flight process, and solving the problem that the current drone avoidance performance of the drone during the return flight process is poor.
[0030] 具体地, 在无人机返航过程中, 若遇到障碍物, 且在遥控器的控制范围内, 无 人机则可以接收到遥控器发送的第二控制信号, 无人机控制系统则会通过软件 编程的方式实现该第二控制信号 (即遥控器的控制信号) 与预定的控制无人机 返航的第一控制信号的叠加, 并利用叠加控制信号, 控制无人机的飞行, 以控 制无人机躲避障碍物。 [0030] Specifically, in the process of returning the drone, if an obstacle is encountered, and within the control range of the remote controller, the drone can receive the second control signal sent by the remote controller, and the drone control system The second control signal (ie, the control signal of the remote controller) is superimposed with the predetermined first control signal for controlling the return of the drone by software programming, and the superimposed control signal is used to control the flight of the drone. To control the drone to avoid obstacles.
[0031] 通过上述实施例, 可以保证无人机在自动返航的过程中, 并在遥控器的控制范 围内, 当遇到障碍物吋, 操纵者使用遥控器控制飞行器, 无人机控制系统接收 到遥控器的控制信号 (即上述的第二控制信号) , 并将遥控器的控制信号与返 航的控制信号 (即上述的第一控制信号) 叠加, 利用叠加后的信号控制无人机 的飞行, 从而达到躲避障碍物的目的, 避免无人机在返航的过程中因为无法躲 避障碍物而坠机。  [0031] Through the above embodiment, the drone can be guaranteed to be in the process of automatic returning, and within the control range of the remote controller, when encountering an obstacle, the operator controls the aircraft using the remote controller, and the drone control system receives a control signal to the remote controller (ie, the second control signal described above), and superimposing the control signal of the remote controller and the return control signal (ie, the first control signal described above), and controlling the flight of the drone by using the superimposed signal In order to avoid obstacles, the drone can be prevented from crashing because of the inability to avoid obstacles during the return flight.
[0032] 在本发明的上述实施例中, 在无人机返航过程中, 上述方法还可以包括: 每隔 预设吋间段, 检测遥控器是否发送第二控制信号; 若检测到遥控器发送第二控 制信号, 则接收遥控器发送的第二控制信号; 若未检测到遥控器发送第二控制 信号, 则利用第一控制信号, 控制无人机返航。  [0032] In the above embodiment of the present invention, in the return process of the drone, the method may further include: detecting, by the preset interval, whether the remote controller sends the second control signal; if detecting the remote controller sending The second control signal receives the second control signal sent by the remote controller; if the remote controller does not detect the second control signal, the first control signal is used to control the drone to return.
[0033] 具体地, 在无人机返航过程中, 若遇到障碍物, 且在遥控器的控制范围内, 遥 控器则会发送第二控制信号至无人机。 无人机控制系统每隔预设吋间段, 检测 遥控器是否发送第二控制信号至无人机, 若检测到遥控器发送第二控制信号, 也即在返航过程中, 无人机遇到障碍物, 无人机控制系统则接收遥控器发送的 第二控制信号, 并通过软件编程的方式实现该第二控制信号与预定的控制无人 机返航的第一控制信号的叠加, 并利用叠加控制信号, 控制无人机的飞行, 以 控制无人机躲避障碍物, 并在无人机成功躲避障碍物之后, 继续利用第一控制 信号控制无人机飞行, 完成返航过程; 若未检测到遥控器发送第二控制信号, 也即在返航过程中, 无人机没有遇到障碍物, 则利用第一控制信号, 控制无人 机返航。 [0033] Specifically, in the process of returning the drone, if an obstacle is encountered and within the control range of the remote controller, the remote controller sends a second control signal to the drone. The drone control system detects whether the remote controller sends the second control signal to the drone every predetermined time interval, and if the remote controller detects that the remote control sends the second control signal, That is, during the return flight, the drone encounters an obstacle, and the drone control system receives the second control signal sent by the remote controller, and implements the second control signal and the predetermined control drone return by software programming. Superimposing the first control signal, and using the superimposed control signal to control the flight of the drone to control the drone to avoid obstacles, and after the drone successfully avoids the obstacle, continue to use the first control signal to control the unmanned The flight of the aircraft completes the return flight process; if the remote control does not detect the second control signal, that is, during the return flight, the drone does not encounter an obstacle, then the first control signal is used to control the drone to return.
[0034] 通过上述实施例, 在无人机返航过程中, 对无人机在遇到障碍物和没有遇到障 碍物的两种情况下, 分别采用不同的控制信号进行控制, 实现了对无人机返航 过程的智能化和高效化的控制。  [0034] Through the above embodiment, in the return process of the unmanned aerial vehicle, the unmanned aerial vehicle adopts different control signals for control in the case of encountering an obstacle and not encountering an obstacle, respectively, and realizes the Intelligent and efficient control of the human-machine return process.
[0035] 在本发明的上述实施例中, 在无人机处于返航过程之前, 方法还包括: 按照预 先定义的触发方式, 生成自动返航触发信号; 在自动返航触发信号的触发下, 无人机进入返航过程。 [0035] In the above embodiment of the present invention, before the drone is in the returning process, the method further includes: generating an automatic returning trigger signal according to a preset triggering manner; and triggering the automatic returning triggering signal, the drone Enter the return flight process.
[0036] 进一步地, 按照预先定义的触发方式, 生成自动返航触发信号至少包括如下之 一: 通过触发遥控器的返航模式幵关, 生成自动返航触发信号; 通过触发地面 控制站的返航按钮, 生成自动返航触发信号; 通过检测到遥控器电量不足的检 测信号, 生成自动返航触发信号; 如果遥控器与无人机的距离大于预设距离, 则生成自动返航触发信号; 如果无人机的能源管理系统的能源低于预设阈值, 则生成自动返航触发信号。  [0036] Further, according to the predefined triggering manner, generating an automatic returning trigger signal includes at least one of the following: generating an automatic returning trigger signal by triggering a return mode of the remote controller; generating a returning button by triggering the ground control station Automatic returning trigger signal; generating an automatic returning trigger signal by detecting a detection signal of insufficient power of the remote controller; if the distance between the remote controller and the drone is greater than a preset distance, generating an automatic returning trigger signal; if the energy management of the drone If the energy of the system is lower than the preset threshold, an automatic return flight trigger signal is generated.
[0037] 具体地, 无人机返航的触发方式是多样的。 可以通过触发遥控器的返航模式幵 关, 也可以通过触发地面控制站的返航按钮, 产生自动返航触发信号, 无人机 控制系统在接收到该自动返航触发信号之后, 在该自动返航触发信号的触发下 , 无人机进入返航过程; 在遥控器电量不足引起无人机控制信号丢失的情况下 , 可以触发无人机自动返航, 即可以通过安装在遥控器中的检测模块, 检测得 到遥控器电量不足的检测信号, 遥控器将该检测信号发送给无人机控制系统, 并通过无人机控制系统生成自动返航触发信号, 在该自动返航触发信号的触发 下, 无人机进入返航过程; 在无人机与遥控器之间的距离太远 (即大于预设距 离) 引起无人机控制信号丢失的情况下, 可以触发无人机自动返航, 即通过无 人机控制系统可以得到无人机与遥控器之间的距离, 并在该距离大于预设距离 的情况下, 生成自动返航触发信号, 在该自动返航触发信号的触发下, 无人机 进入返航过程; 如果无人机带有能源管理系统, 在能源低于某一阈值 (即上述 的预设阈值) , 即将不足以支持无人机自动返航的情况下, 可以触发无人机自 动返航, 即可以通过无人机控制系统来检测能源是否低于某一阈值, 并在能源 低于某一阈值的情况下, 生成自动返航触发信号, 在该自动返航触发信号的触 发下, 无人机进入返航过程。 [0037] Specifically, the trigger mode of the drone returning is diverse. The auto-return trigger signal can be generated by triggering the return mode of the remote control, or by triggering the return button of the ground control station. After receiving the auto-return trigger signal, the drone control system is in the auto-return trigger signal. Under the trigger, the drone enters the returning process; when the power of the remote control is insufficient, the drone control signal is lost, the drone can be triggered to return automatically, that is, the remote controller can be detected by the detecting module installed in the remote controller. The detection signal of the low battery is sent by the remote controller to the drone control system, and the automatic returning trigger signal is generated by the drone control system, and the drone enters the returning process under the trigger of the automatic returning trigger signal; When the distance between the drone and the remote controller is too far (ie, greater than the preset distance), causing the drone control signal to be lost, the drone can be triggered to automatically return to the air, that is, The man-machine control system can obtain the distance between the drone and the remote controller, and generate an automatic returning trigger signal when the distance is greater than the preset distance, and the drone enters and returns under the trigger of the automatic returning trigger signal. If the drone has an energy management system, when the energy is below a certain threshold (that is, the above-mentioned preset threshold), it is not enough to support the automatic return of the drone, the drone can be triggered to automatically return, that is, The drone control system can be used to detect whether the energy is below a certain threshold, and when the energy is below a certain threshold, an automatic returning trigger signal is generated, and the drone enters and returns under the trigger of the automatic returning trigger signal. process.
[0038] 通过上述实施例, 可以在多种触发方式的作用下, 触发无人机进入返航过程, 实现了对无人机控制的灵活性, 从而可以提高使用者的使用体验。  [0038] Through the above embodiments, the drone can be triggered to enter the returning process under the action of various triggering modes, thereby realizing the flexibility of the drone control, thereby improving the user experience.
[0039] 在本发明的上述实施例中, 在每隔预设吋间段, 检测遥控器是否发送第二控制 信号之前, 方法还包括: 检测预先设置的返航方式; 按照与预先设置的返航方 式对应的无人机的飞行信号, 得到第一控制信号。  [0039] In the above embodiment of the present invention, before detecting whether the remote controller sends the second control signal every predetermined interval, the method further includes: detecting a preset return mode; according to the preset return mode Corresponding drone flight signals, the first control signal is obtained.
[0040] 进一步地, 预先设置的返航方式包括如下任意一种: 直角路线返航方式、 三维 坐标轴抛物线返航方式和圆形返航方式。  [0040] Further, the preset return mode includes any one of the following: a right angle return mode, a three-dimensional coordinate parabola return mode, and a round return mode.
[0041] 具体地, 在无人机进入返航过程之后, 当无人机处于当前飞行高度, 或者在地 面站设置返航高度的情况下, 控制无人机飞到设置的指定高度之后, 无人机控 制系统检测操作者选择的返航方式 (即上述的预先设置的返航方式) , 并根据 与该返航方式对应的飞行信号, 可以得到第一控制信号, 也即得到自动返航控 制信号。  [0041] Specifically, after the drone enters the return flight process, when the drone is at the current flight altitude, or the ground station is set to the return altitude, the drone is controlled to fly to the set height, the drone The control system detects the return mode selected by the operator (ie, the preset return mode described above), and according to the flight signal corresponding to the return mode, the first control signal can be obtained, that is, the automatic return control signal is obtained.
[0042] 进一步地, 在遥控器不参与任何控制的情况下, 飞行器的自动返航路线是可选 的, 可以根据当吋的飞行环境选择返航方式, 即选择自动返航路线。 返航方式 是多样的, 可以在地面站设置以直角路线, 三坐标轴路线抛物线或者圆形路线 等不同的路线返航, 即设置的返航方式可以为直角路线返航方式 (即无人机垂 直移动到设置高度以及水平地直线位移的方航方式) 、 三维坐标轴抛物线返航 方式 (即以无人机所在位置、 设置的返航位置以及中间飞行经过的位置拟定出 抛物线运动轨迹的返航方式) 或圆形返航方式 (即以无人机所在位置、 设置的 返航位置以及中间飞行经过的位置拟定出圆弧运动轨迹的返航方式) 。  [0042] Further, in the case that the remote controller does not participate in any control, the automatic return route of the aircraft is optional, and the return flight mode may be selected according to the flight environment of the vehicle, that is, the automatic return route is selected. The return mode is various. It can be set at the ground station with a right-angle route, a three-axis route parabola or a circular route, etc., that is, the set return mode can be the right-angle route return mode (ie, the drone moves vertically to the setting). The altitude and horizontal linear displacement of the voyage mode), the three-dimensional axis parabolic return mode (ie, the return position of the parabolic trajectory is determined by the location of the drone, the set return position and the position of the intermediate flight) or round return The method (ie, the return mode of the arc motion track is determined by the location of the drone, the set return position, and the position of the intermediate flight).
[0043] 通过上述实施例, 可以根据无人机当吋的飞行环境, 在地面站选择设置不同的 返航方式, 根据选择的返航方式, 可以实现对无人机的灵活控制。 [0043] According to the above embodiment, according to the flying environment of the drone, the ground station can be selected and set differently. The return mode, according to the selected return mode, can achieve flexible control of the drone.
[0044] 在本发明的上述实施例中, 控制无人机返航包括如下之一: 控制无人机返回通 过遥控器的掰杆启动的位置所指示的返航点; 控制无人机返回通过遥控器或地 面站设置的返航点; 控制无人机返回预先设定的固定返航点。 [0044] In the above embodiment of the present invention, controlling the return of the drone includes one of: controlling the drone to return to the return point indicated by the position of the mast start of the remote controller; controlling the drone to return through the remote controller Or the return point set by the ground station; control the drone to return to the preset fixed return point.
[0045] 具体地, 控制无人机返航, 最终是控制无人机返回返航点。 返航点的设计可以 有多种, 例如, 可以将遥控器的掰杆启动的位置作为返航点的位置; 如果使用 者想要设置飞行中的某一点为返航点, 可以通过遥控器或者地面站设计; 上述 两种返航点的设计为短暂返航点, 即使用者可以根据需要进行重新设计; 如果 使用者想要每次无人机都回到固定的位置, 可以通过软件编程的方式, 在程序 中设置永久返航点。 此外, 在该实施例中, 遥控器上设置有一个切换幵关, 用 于指示能不能通过掰杆启动或者遥控器设置返航点, 也即通过该切换幵关, 切 换返航点的设计方式, 是通过遥控器的掰杆启动的位置作为返航点的位置, 还 是在无人机飞行的过程中, 通过遥控器设计返航点。 [0045] Specifically, the drone is controlled to return, and finally the drone is controlled to return to the return point. The design of the return point can be various. For example, the position where the mast of the remote controller is activated can be used as the position of the return point. If the user wants to set a certain point in the flight as the return point, it can be designed by the remote controller or the ground station. The above two return points are designed as short return points, that is, the user can redesign as needed; if the user wants to return to a fixed position every time the drone can be programmed by software, in the program Set a permanent return point. In addition, in this embodiment, a remote switch is provided with a switch to indicate whether the return point can be activated by the mast or the remote controller is set, that is, the design of the return point is switched by the switch. The position activated by the mast of the remote control is used as the position of the return point, or the return point is designed by the remote controller during the flight of the drone.
[0046] 通过上述实施例, 返航点的设计是多样的, 基于返航点的设计的多样性, 可以 实现对无人机的灵活控制, 提高使用者的使用体验。 [0046] Through the above embodiments, the design of the return point is diverse, and based on the diversity of the design of the return point, the flexible control of the drone can be realized, and the user experience is improved.
[0047] 在此需要说明的是, 上述实施例中的无人机也可以称为飞行器。 [0047] It should be noted that the drone in the above embodiment may also be referred to as an aircraft.
[0048] 下面结合图 2详述本发明的上述实施例。 如图 2所示, 该实施例可以包括如下步 骤: [0048] The above embodiment of the present invention will be described in detail below with reference to FIG. As shown in FIG. 2, the embodiment may include the following steps:
[0049] 步骤 S201 , 无人机进入返航过程。  [0049] Step S201: The drone enters a return flight process.
[0050] 具体地, 可以按照预先定义的触发方式, 生成自动返航触发信号; 在自动返航 触发信号的触发下, 无人机进入返航过程。 其中, 按照预先定义的触发方式, 生成自动返航触发信号的实施与上述实施例中的一致, 在此不再赘述。  [0050] Specifically, the automatic returning trigger signal may be generated according to a preset triggering manner; under the trigger of the automatic returning triggering signal, the drone enters a returning process. The implementation of the automatic returning trigger signal is the same as that in the foregoing embodiment, and is not described here.
[0051] 步骤 S202, 控制无人机飞到指定高度。  [0051] Step S202: Control the drone to fly to a specified height.
[0052] 可选地, 在地面站设置返航高度的情况下, 控制无人机飞到设置的指定高度。  [0052] Optionally, in the case that the ground station sets the return altitude, the drone is controlled to fly to the set height.
[0053] 步骤 S203 , 检测操作者选择的返航方式。 [0053] Step S203: Detect a return mode selected by the operator.
[0054] 具体地, 操作者选择的返航方式, 即为上述的预先设置的返航方式, 返航方式 是多样的, 是在地面站, 由操作者根据无人机当吋的飞行环境选择的。  [0054] Specifically, the return mode selected by the operator is the above-mentioned preset return mode, and the return mode is various, which is selected at the ground station by the operator according to the flight environment of the drone.
[0055] 步骤 S204, 按照与操作者选择的返航方式对应的无人机的飞行信号, 得到第一 控制信号。 [0055] Step S204, obtaining a first flight according to a flight signal of the drone corresponding to the return mode selected by the operator. control signal.
[0056] 其中, 第一控制信号为预定的控制无人机返航的信号, 即自动返航控制信号, 无人机自动返航应有的控制信号; 对与操作者选择的返航方式对应的无人机的 飞行信号进行实吋计算, 得到第一控制信号。  [0056] wherein, the first control signal is a predetermined signal for controlling the return of the drone, that is, the automatic return control signal, the control signal of the automatic return of the drone; and the drone corresponding to the return mode selected by the operator The flight signal is calculated and the first control signal is obtained.
[0057] 步骤 S205 , 每隔预设吋间段, 检测遥控器是否发送第二控制信号。 [0057] Step S205: Detect whether the remote controller sends the second control signal every preset period.
[0058] 具体地, 每隔一个周期, 检测是否有遥控器控制信号介入, 即每隔一个周期, 检测是否接收到遥控器控制信号 (即上述的第二控制信号) 。 [0058] Specifically, every other period, it is detected whether there is a remote control signal intervention, that is, every other period, whether or not the remote control signal (ie, the second control signal described above) is received is detected.
[0059] 若检测到遥控器发送第二控制信号, 则执行步骤 S206; 否则, 执行步骤 S207。 [0059] If it is detected that the remote controller sends the second control signal, step S206 is performed; otherwise, step S207 is performed.
[0060] 步骤 S206, 将第二控制信号与第一控制信号叠加, 得到叠加控制信号。 [0060] Step S206, superimposing the second control signal and the first control signal to obtain a superposition control signal.
[0061] 具体地, 通过软件编程的方式实现遥控器发送的第二控制信号与预定的控制无 人机返航的第一控制信号的叠加。 执行步骤 S206之后, 执行步骤 S208。 [0061] Specifically, the superposition of the second control signal sent by the remote controller and the predetermined first control signal for controlling the return of the human-machine is realized by software programming. After step S206 is performed, step S208 is performed.
[0062] 步骤 S207, 利用第一控制信号, 控制无人机返航。 [0062] Step S207, using the first control signal, controlling the drone to return.
[0063] 具体地, 若未检测到遥控器发送第二控制信号, 也即在返航过程中, 无人机没 有遇到障碍物, 则利用第一控制信号, 控制无人机返航。  [0063] Specifically, if it is not detected that the remote controller sends the second control signal, that is, during the return flight, the drone does not encounter an obstacle, the first control signal is used to control the drone to return.
[0064] 步骤 S208 , 利用叠加控制信号, 控制无人机返航。 [0064] Step S208: Control the drone to return by using the superimposed control signal.
[0065] 具体地, 利用叠加控制信号, 控制无人机的飞行, 以控制无人机躲避障碍物, 并在无人机成功躲避障碍物之后, 继续利用第一控制信号控制无人机飞行, 完 成返航过程。  [0065] Specifically, the superimposed control signal is used to control the flight of the drone to control the drone to avoid obstacles, and after the drone successfully avoids the obstacle, continue to control the drone flight by using the first control signal, Complete the return journey.
[0066] 在上述实施例中, 与目前现有的无人机自动返航过程不一样的是, 在控制无人 机飞行的飞行控制程序中, 如果飞行器执行自动返航的任务指令, 飞行器会按 照设置的返航方式返航, 但是当操作者发现在飞行器返航的过程中, 飞行器遇 到障碍物吋, 操纵者可以通过遥控器来控制飞行器的飞行, 此吋飞行器的控制 信号是遥控器控制信号 (即上述的第二控制信号) 与自动返航应有的控制信号 (即上述的第一控制信号) 的叠加, 利用叠加后的信号控制飞行器返航。 为了 避免操作者在紧急情况下的误操作带来的损失, 在上述的有遥控器信号参与控 制的返航过程中, 飞行器会以无头模式运行, 即始终以遥控器信号 (即上述实 施例中的第二控制信号) 进入吋的机头方向为飞行方向前行, 这样避免操作者 在误打偏航角后, 因找不到机头朝向而无法正确操纵飞行器顺利躲避障碍物的 情况发生。 [0066] In the above embodiment, unlike the current automatic returning process of the unmanned aerial vehicle, in the flight control program for controlling the flight of the drone, if the aircraft performs the task instruction of automatic returning, the aircraft will follow the setting. The return mode returns, but when the operator finds that the aircraft encounters an obstacle during the return of the aircraft, the operator can control the flight of the aircraft through the remote control. The control signal of the aircraft is the remote control signal (ie, the above The second control signal is superimposed with the control signal (ie, the first control signal described above) that is automatically returned, and the superimposed signal is used to control the aircraft to return. In order to avoid the loss caused by the operator's erroneous operation in an emergency, the aircraft will operate in the headless mode during the return flight with the remote control signal participating in the control, that is, the remote control signal is always used (ie, in the above embodiment) The second control signal) enters the direction of the nose of the cymbal in the direction of flight, so as to prevent the operator from correctly manipulating the aircraft and avoiding obstacles after failing to hit the yaw angle. The situation happened.
[0067] 通过上述实施例, 在不中断自动返航的过程中, 加入遥控器的控制, 将遥控器 的控制信号与返航的控制信号叠加, 利用叠加后的信号控制飞行器躲避障碍物 , 完成返航, 从而可以避免无人机坠机的情况发生而减少损失, 同吋也可以减 少能量的损耗。  [0067] Through the above embodiment, in the process of not interrupting the automatic returning, the control of the remote controller is added, the control signal of the remote controller is superimposed with the control signal of the returning, and the superimposed signal is used to control the aircraft to avoid obstacles and complete the return flight. This can prevent the drone from crashing and reduce the loss, and the same can reduce the loss of energy.
[0068] 实施例 2  Example 2
[0069] 图 3是根据本发明实施例的一种无人机返航的控制装置的示意图, 如图 3所示, 该装置可以包括: 返航模块 32、 第一接收模块 34、 叠加模块 36和第一控制模块 3 8。  3 is a schematic diagram of a control device for returning a drone according to an embodiment of the present invention. As shown in FIG. 3, the device may include: a returning module 32, a first receiving module 34, a superimposing module 36, and a A control module 38.
[0070] 其中, 返航模块 32, 用于根据第一控制信号控制无人机按预定路径返航; [0071] 第一接收模块 34, 用于在无人机按预定路径返航过程中, 接收遥控器发送的第 二控制信号, 其中, 第二控制信号用于调整预定路径, 以使无人机躲避障碍物  [0070] wherein, the returning module 32 is configured to control the drone to return to the predetermined path according to the first control signal; [0071] the first receiving module 34 is configured to receive the remote controller during the return of the drone according to the predetermined path a second control signal sent, wherein the second control signal is used to adjust a predetermined path to enable the drone to avoid obstacles
[0072] 叠加模块 36, 用于将第二控制信号与第一控制信号叠加, 得到叠加控制信号, 其中, 第一控制信号为预定的控制无人机返航的信号; [0072] The superimposing module 36 is configured to superimpose the second control signal and the first control signal to obtain a superimposed control signal, where the first control signal is a predetermined signal for controlling the return of the drone;
[0073] 第一控制模块 38, 用于利用叠加控制信号, 控制无人机返航。 [0073] The first control module 38 is configured to control the drone to return using the superimposed control signal.
[0074] 采用本发明的实施例, 在无人机返航过程中, 若遇到障碍物, 遥控器则发送第 二控制信号给无人机, 无人机控制系统则会将该第二控制信号与预定的控制无 人机返航的第一控制信号叠加, 利用叠加控制信号, 控制无人机返航, 即无人 机在第一控制信号所控制的基础上, 加入第二控制信号作为微调。 通过上述实 施例, 在无人机返航过程中, 且在不中断返航过程的情况下, 可以通过遥控器 发送的第二控制信号和预定的控制无人机返航的第一控制信号叠加的叠加控制 信号, 调整第一控制信号所控制的预定路径, 使得无人机可以躲避障碍物, 此 夕卜, 与现有技术中采取原路返回的机制来实现躲避障碍物的方案相比, 对能量 余量的要求比较低, 可以减少能量损耗, 从而提高了无人机在返航过程中的避 障性能, 解决了目前无人机在返航过程中避障性能差的问题。 [0074] With the embodiment of the present invention, in the process of returning the drone, if an obstacle is encountered, the remote controller sends a second control signal to the drone, and the drone control system will use the second control signal. Superimposed with a predetermined first control signal for controlling the return of the drone, the superimposed control signal is used to control the return of the drone, that is, the drone adds a second control signal as a fine adjustment based on the control of the first control signal. Through the above embodiment, in the return process of the drone, and without interrupting the returning process, the second control signal that can be sent by the remote controller and the predetermined superimposition control of superimposing the first control signal of the drone returning The signal adjusts a predetermined path controlled by the first control signal, so that the drone can avoid obstacles. In addition, compared with the prior art adopting the mechanism of returning the original path to implement the obstacle avoidance scheme, the energy balance is The requirement of quantity is relatively low, which can reduce the energy loss, thereby improving the obstacle avoidance performance of the drone during the return flight process, and solving the problem that the current drone avoidance performance of the drone during the return flight process is poor.
[0075] 具体地, 在无人机返航过程中, 若遇到障碍物, 且在遥控器的控制范围内, 无 人机则可以接收到遥控器发送的第二控制信号, 无人机控制系统则会通过软件 编程的方式实现该第二控制信号 (即遥控器的控制信号) 与预定的控制无人机 返航的第一控制信号的叠加, 并利用叠加控制信号, 控制无人机的飞行, 以控 制无人机躲避障碍物。 [0075] Specifically, in the process of returning the drone, if an obstacle is encountered, and within the control range of the remote controller, the drone can receive the second control signal sent by the remote controller, and the drone control system Will pass the software The method of programming realizes superposition of the second control signal (ie, the control signal of the remote controller) with the predetermined first control signal for controlling the return of the drone, and controls the flight of the drone by using the superimposed control signal to control the unmanned The machine avoids obstacles.
[0076] 通过上述实施例, 可以保证无人机在自动返航的过程中, 并在遥控器的控制范 围内, 当遇到障碍物吋, 操纵者使用遥控器控制飞行器, 无人机控制系统接收 到遥控器的控制信号 (即上述的第二控制信号) , 并将遥控器的控制信号与返 航的控制信号 (即上述的第一控制信号) 叠加, 利用叠加后的信号控制无人机 的飞行, 从而达到躲避障碍物的目的, 避免无人机在返航的过程中因为无法躲 避障碍物而坠机。  [0076] Through the above embodiments, the drone can be guaranteed to be in the process of automatic returning, and within the control range of the remote controller, when encountering an obstacle, the operator controls the aircraft using the remote controller, and the drone control system receives a control signal to the remote controller (ie, the second control signal described above), and superimposing the control signal of the remote controller and the return control signal (ie, the first control signal described above), and controlling the flight of the drone by using the superimposed signal In order to avoid obstacles, the drone can be prevented from crashing because of the inability to avoid obstacles during the return flight.
[0077] 在本发明的上述实施例中, 上述装置还可以包括: 检测模块, 用于在无人机返 航过程中, 每隔预设吋间段, 检测遥控器是否发送第二控制信号; 第二接收模 块, 用于若检测到遥控器发送第二控制信号, 则接收遥控器发送的第二控制信 号; 第二控制模块, 用于若未检测到遥控器发送第二控制信号, 则利用第一控 制信号, 控制无人机返航。  [0077] In the above embodiment of the present invention, the device may further include: a detecting module, configured to detect whether the remote controller sends the second control signal every preset period during the return process of the drone; a receiving module, configured to receive a second control signal sent by the remote controller if the remote controller detects that the second control signal is sent, where the second control module is configured to: if the remote controller does not detect the second control signal, A control signal controls the drone to return.
[0078] 具体地, 在无人机返航过程中, 若遇到障碍物, 且在遥控器的控制范围内, 遥 控器则会发送第二控制信号至无人机。 无人机控制系统每隔预设吋间段, 检测 遥控器是否发送第二控制信号至无人机, 若检测到遥控器发送第二控制信号, 也即在返航过程中, 无人机遇到障碍物, 无人机控制系统则接收遥控器发送的 第二控制信号, 并通过软件编程的方式实现该第二控制信号与预定的控制无人 机返航的第一控制信号的叠加, 并利用叠加控制信号, 控制无人机的飞行, 以 控制无人机躲避障碍物, 并在无人机成功躲避障碍物之后, 继续利用第一控制 信号控制无人机飞行, 完成返航过程; 若未检测到遥控器发送第二控制信号, 也即在返航过程中, 无人机没有遇到障碍物, 则利用第一控制信号, 控制无人 机返航。  [0078] Specifically, in the process of returning the drone, if an obstacle is encountered and within the control range of the remote controller, the remote controller sends a second control signal to the drone. The drone control system detects whether the remote control sends a second control signal to the drone every predetermined interval, and if the remote controller detects that the second control signal is sent, that is, during the return flight, the drone encounters an obstacle. The UAV control system receives the second control signal sent by the remote controller, and realizes superposition of the second control signal and the predetermined first control signal for controlling the return of the drone by software programming, and uses the superposition control Signal, control the flight of the drone to control the drone to avoid obstacles, and after the drone successfully avoids the obstacle, continue to use the first control signal to control the drone flight, complete the return flight process; if no remote control is detected The second control signal is sent, that is, during the return flight, if the drone does not encounter an obstacle, the first control signal is used to control the drone to return.
[0079] 通过上述实施例, 在无人机返航过程中, 对无人机在遇到障碍物和没有遇到障 碍物的两种情况下, 分别采用不同的控制信号进行控制, 实现了对无人机返航 过程的智能化和高效化的控制。  [0079] Through the above embodiment, in the return process of the unmanned aerial vehicle, the drone is controlled by different control signals in the case of encountering obstacles and not encountering obstacles, thereby realizing Intelligent and efficient control of the human-machine return process.
[0080] 在本发明的上述实施例中, 上述装置还可以包括: 生成模块, 用于在无人机处 于返航过程之前, 按照预先定义的触发方式, 生成自动返航触发信号; 触发模 块, 用于在自动返航触发信号的触发下, 无人机进入返航过程。 [0080] In the above embodiment of the present invention, the apparatus may further include: a generating module, configured at the drone Before the returning process, an automatic returning trigger signal is generated according to a preset triggering manner; and a triggering module is used for triggering the returning process of the drone under the trigger of the automatic returning trigger signal.
[0081] 具体地, 无人机返航的触发方式是多样的。 可以通过触发遥控器的返航模式幵 关, 也可以通过触发地面控制站的返航按钮, 产生自动返航触发信号, 无人机 控制系统在接收到该自动返航触发信号之后, 在该自动返航触发信号的触发下 , 无人机进入返航过程; 在遥控器电量不足引起无人机控制信号丢失的情况下 , 可以触发无人机自动返航, 即可以通过安装在遥控器中的检测模块, 检测得 到遥控器电量不足的检测信号, 遥控器将该检测信号发送给无人机控制系统, 并通过无人机控制系统生成自动返航触发信号, 在该自动返航触发信号的触发 下, 无人机进入返航过程; 在无人机与遥控器之间的距离太远 (即大于预设距 离) 引起无人机控制信号丢失的情况下, 可以触发无人机自动返航, 即通过无 人机控制系统可以得到无人机与遥控器之间的距离, 并在该距离大于预设距离 的情况下, 生成自动返航触发信号, 在该自动返航触发信号的触发下, 无人机 进入返航过程; 如果无人机带有能源管理系统, 在能源低于某一阈值 (即上述 的预设阈值) , 即将不足以支持无人机自动返航的情况下, 可以触发无人机自 动返航, 即可以通过无人机控制系统来检测能源是否低于某一阈值, 并在能源 低于某一阈值的情况下, 生成自动返航触发信号, 在该自动返航触发信号的触 发下, 无人机进入返航过程。  [0081] Specifically, the trigger mode of the drone returning is diverse. The auto-return trigger signal can be generated by triggering the return mode of the remote control, or by triggering the return button of the ground control station. After receiving the auto-return trigger signal, the drone control system is in the auto-return trigger signal. Under the trigger, the drone enters the returning process; when the power of the remote control is insufficient, the drone control signal is lost, the drone can be triggered to return automatically, that is, the remote controller can be detected by the detecting module installed in the remote controller. The detection signal of the low battery is sent by the remote controller to the drone control system, and the automatic returning trigger signal is generated by the drone control system, and the drone enters the returning process under the trigger of the automatic returning trigger signal; When the distance between the drone and the remote controller is too far (that is, greater than the preset distance), the drone control signal is lost, and the drone can be automatically returned, that is, the drone control system can obtain the unmanned The distance between the machine and the remote control, and the distance is greater than the preset distance The auto-return trigger signal is generated, and the drone enters the returning process under the trigger of the auto-return trigger signal; if the drone has an energy management system, the energy is below a certain threshold (ie, the above-mentioned preset threshold) In the case that it is not enough to support the automatic return of the drone, it can trigger the automatic return of the drone, that is, the drone control system can detect whether the energy is below a certain threshold and the energy is below a certain threshold. Next, an automatic returning trigger signal is generated, and the drone enters the returning process under the trigger of the automatic returning trigger signal.
[0082] 通过上述实施例, 可以在多种触发方式的作用下, 触发无人机进入返航过程, 实现了对无人机控制的灵活性, 从而可以提高使用者的使用体验。  [0082] Through the above embodiments, the drone can be triggered to enter the returning process under the action of various triggering modes, thereby realizing the flexibility of the drone control, thereby improving the user experience.
[0083] 在上述实施例中, 与目前现有的无人机自动返航过程不一样的是, 在控制无人 机飞行的飞行控制程序中, 如果飞行器执行自动返航的任务指令, 飞行器会按 照设置的返航方式返航, 但是当操作者发现在飞行器返航的过程中, 飞行器遇 到障碍物吋, 操纵者可以通过遥控器来控制飞行器的飞行, 此吋飞行器的控制 信号是遥控器控制信号 (即上述的第二控制信号) 与自动返航应有的控制信号 (即上述的第一控制信号) 的叠加, 利用叠加后的信号控制飞行器返航。 为了 避免操作者在紧急情况下的误操作带来的损失, 在上述的有遥控器信号参与控 制的返航过程中, 飞行器会以无头模式运行, 即始终以遥控器信号进入吋的机 头方向为飞行方向前行, 这样避免操作者在误打偏航角后, 因找不到机头朝向 而无法正确操纵飞行器顺利躲避障碍物的情况发生。 [0083] In the above embodiment, unlike the current automatic returning process of the unmanned aerial vehicle, in the flight control program for controlling the flight of the drone, if the aircraft performs the task command of the automatic returning flight, the aircraft will follow the setting. The return mode returns, but when the operator finds that the aircraft encounters an obstacle during the return of the aircraft, the operator can control the flight of the aircraft through the remote control. The control signal of the aircraft is the remote control signal (ie, the above The second control signal is superimposed with the control signal (ie, the first control signal described above) that is automatically returned, and the superimposed signal is used to control the aircraft to return. In order to avoid the operator's loss caused by the erroneous operation in an emergency, the aircraft will operate in the headless mode during the return flight with the remote control signal participating in the control, that is, the machine always enters the 以 machine with the remote control signal. The direction of the head is forward in the direction of flight, so as to prevent the operator from correctly manipulating the aircraft to avoid obstacles after the yaw angle is missed.
[0084] 通过上述实施例, 在不中断自动返航的过程中, 加入遥控器的控制, 将遥控器 的控制信号与返航的控制信号叠加, 利用叠加后的信号控制飞行器躲避障碍物 , 完成返航, 从而可以避免无人机坠机的情况发生而减少损失, 同吋也可以减 少能量的损耗。 上述本发明实施例序号仅仅为了描述, 不代表实施例的优劣。  [0084] Through the above embodiment, in the process of not interrupting the automatic returning, the control of the remote controller is added, the control signal of the remote controller is superimposed with the control signal of the returning, and the superimposed signal is used to control the aircraft to avoid obstacles and complete the return flight. This can prevent the drone from crashing and reduce the loss, and the same can reduce the loss of energy. The serial numbers of the embodiments of the present invention are merely for the description, and do not represent the advantages and disadvantages of the embodiments.
[0085] 在本发明的上述实施例中, 对各个实施例的描述都各有侧重, 某个实施例中没 有详述的部分, 可以参见其他实施例的相关描述。  [0085] In the above-described embodiments of the present invention, the descriptions of the various embodiments are different, and the details are not described in detail in an embodiment, and the related descriptions of other embodiments may be referred to.
[0086] 在本申请所提供的几个实施例中, 应该理解到, 所揭露的技术内容, 可通过其 它的方式实现。 其中, 以上所描述的装置实施例仅仅是示意性的, 例如所述单 元的划分, 可以为一种逻辑功能划分, 实际实现吋可以有另外的划分方式, 例 如多个单元或组件可以结合或者可以集成到另一个系统, 或一些特征可以忽略 , 或不执行。 另一点, 所显示或讨论的相互之间的耦合或直接耦合或通信连接 可以是通过一些接口, 单元或模块的间接耦合或通信连接, 可以是电性或其它 的形式。  [0086] In the several embodiments provided by the present application, it should be understood that the disclosed technical content may be implemented in other manners. The device embodiments described above are only schematic. For example, the division of the unit may be a logical function division. The actual implementation may have another division manner. For example, multiple units or components may be combined or may be Integration into another system, or some features can be ignored, or not executed. In addition, the mutual coupling or direct coupling or communication connection shown or discussed may be an indirect coupling or communication connection through some interface, unit or module, and may be electrical or otherwise.
[0087] 所述作为分离部件说明的单元可以是或者也可以不是物理上分幵的, 作为单元 显示的部件可以是或者也可以不是物理单元, 即可以位于一个地方, 或者也可 以分布到多个单元上。 可以根据实际的需要选择其中的部分或者全部单元来实 现本实施例方案的目的。  [0087] The unit described as a separate component may or may not be physically distributed, and the component displayed as a unit may or may not be a physical unit, that is, may be located in one place, or may be distributed to multiple On the unit. Some or all of the units may be selected according to actual needs to achieve the objectives of the embodiment of the present embodiment.
[0088] 另外, 在本发明各个实施例中的各功能单元可以集成在一个处理单元中, 也可 以是各个单元单独物理存在, 也可以两个或两个以上单元集成在一个单元中。 上述集成的单元既可以采用硬件的形式实现, 也可以采用软件功能单元的形式 实现。  [0088] In addition, each functional unit in each embodiment of the present invention may be integrated into one processing unit, or each unit may exist physically separately, or two or more units may be integrated into one unit. The above integrated unit can be implemented in the form of hardware or in the form of a software functional unit.
[0089] 所述集成的单元如果以软件功能单元的形式实现并作为独立的产品销售或使用 吋, 可以存储在一个计算机可读取存储介质中。 基于这样的理解, 本发明的技 术方案本质上或者说对现有技术做出贡献的部分或者该技术方案的全部或部分 可以以软件产品的形式体现出来, 该计算机软件产品存储在一个存储介质中, 包括若干指令用以使得一台计算机设备 (可为个人计算机、 服务器或者网络设 备等) 执行本发明各个实施例所述方法的全部或部分步骤。 而前述的存储介质 包括: U盘、 只读存储器 (ROM, Read-Only [0089] The integrated unit, if implemented in the form of a software functional unit and sold or used as a standalone product, may be stored in a computer readable storage medium. Based on such understanding, the technical solution of the present invention may contribute to the prior art or all or part of the technical solution may be embodied in the form of a software product stored in a storage medium. , including a number of instructions to make a computer device (can be a personal computer, server or network All or part of the steps of the method described in the various embodiments of the invention are performed. The foregoing storage medium includes: a USB flash drive, a read only memory (ROM, Read-Only)
Memory) 、 随机存取存储器 (RAM, Random Access Memory) 、 移动硬盘、 磁 碟或者光盘等各种可以存储程序代码的介质。  Memory, Random Access Memory (RAM), removable hard disk, disk or optical disk, and other media that can store program code.
以上所述仅是本发明的优选实施方式, 应当指出, 对于本技术领域的普通技术 人员来说, 在不脱离本发明原理的前提下, 还可以做出若干改进和润饰, 这些 改进和润饰也应视为本发明的保护范围。  The above description is only a preferred embodiment of the present invention, and it should be noted that those skilled in the art can also make several improvements and retouchings without departing from the principles of the present invention. It should be considered as the scope of protection of the present invention.

Claims

权利要求书 Claim
[权利要求 1] 一种无人机返航的控制方法, 其特征在于, 包括:  [Claim 1] A method for controlling the return of a drone, comprising:
根据第一控制信号控制所述无人机按预定路径返航;  Controlling the drone to return to the predetermined path according to the first control signal;
在所述无人机按所述预定路径返航过程中, 接收遥控器发送的第二控 制信号, 其中, 所述第二控制信号用于调整所述预定路径, 以使所述 无人机躲避障碍物;  Receiving a second control signal sent by the remote controller during the return of the drone according to the predetermined path, wherein the second control signal is used to adjust the predetermined path, so that the drone avoids obstacles Object
将所述第二控制信号与所述第一控制信号叠加, 得到叠加控制信号; 利用所述叠加控制信号, 控制所述无人机返航。  Superimposing the second control signal and the first control signal to obtain a superimposed control signal; and using the superimposed control signal to control the drone to return.
[权利要求 2] 根据权利要求 1所述的方法, 其特征在于, 在无人机返航过程中, 所 述方法还包括:  [Claim 2] The method according to claim 1, wherein during the return of the drone, the method further comprises:
每隔预设吋间段, 检测所述遥控器是否发送所述第二控制信号; 若检测到所述遥控器发送所述第二控制信号, 则接收所述遥控器发送 的所述第二控制信号;  Detecting whether the remote controller sends the second control signal every predetermined time interval; receiving the second control sent by the remote controller if detecting that the remote controller sends the second control signal Signal
若未检测到所述遥控器发送所述第二控制信号, 则利用所述第一控制 信号, 控制所述无人机返航。  If the remote controller is not detected to send the second control signal, the first control signal is used to control the drone to return.
[权利要求 3] 根据权利要求 1所述的方法, 其特征在于, 在无人机处于返航过程之 前, 所述方法还包括: [Claim 3] The method according to claim 1, wherein the method further comprises: before the drone is in the returning process, the method further comprises:
按照预先定义的触发方式, 生成自动返航触发信号;  Generate an automatic return trigger signal according to a predefined trigger mode;
在所述自动返航触发信号的触发下, 所述无人机进入返航过程。  The drone enters a return flight process triggered by the automatic return flight trigger signal.
[权利要求 4] 根据权利要求 3所述的方法, 其特征在于, 按照预先定义的触发方式[Claim 4] The method according to claim 3, characterized by: according to a predefined triggering method
, 生成自动返航触发信号至少包括如下之一: , generating an automatic returning trigger signal includes at least one of the following:
通过触发所述遥控器的返航模式幵关, 生成所述自动返航触发信号; 通过触发地面控制站的返航按钮, 生成所述自动返航触发信号; 通过检测到所述遥控器电量不足的检测信号, 生成所述自动返航触发 信号;  The automatic returning trigger signal is generated by triggering a return mode of the remote controller; generating the automatic returning trigger signal by triggering a return button of the ground control station; by detecting a detection signal of the remote controller that the power is insufficient, Generating the automatic returning trigger signal;
如果所述遥控器与所述无人机的距离大于预设距离, 则生成所述自动 返航触发信号;  Generating the automatic returning trigger signal if the distance between the remote controller and the drone is greater than a preset distance;
如果所述无人机的能源管理系统的能源低于预设阈值, 则生成所述自 动返航触发信号。 Generating the self if the energy of the energy management system of the drone is lower than a preset threshold The return flight trigger signal.
[权利要求 5] 根据权利要求 2所述的方法, 其特征在于, 在每隔预设吋间段, 检测 所述遥控器是否发送所述第二控制信号之前, 所述方法还包括: 检测预先设置的返航方式;  [Claim 5] The method according to claim 2, wherein before the remote controller detects whether the remote controller sends the second control signal, the method further includes: detecting the advance Set the return mode;
按照与所述预先设置的返航方式对应的所述无人机的飞行信号, 得到 所述第一控制信号。  The first control signal is obtained according to a flight signal of the drone corresponding to the preset return mode.
[权利要求 6] 根据权利要求 5所述的方法, 其特征在于, 所述预先设置的返航方式 包括如下任意一种:  [Claim 6] The method according to claim 5, wherein the preset return mode includes any one of the following:
直角路线返航方式、 三维坐标轴抛物线返航方式和圆形返航方式。  Right-angle route return mode, three-dimensional axis parabolic return mode and round return mode.
[权利要求 7] 根据权利要求 1或 2所述的方法, 其特征在于, 控制所述无人机返航包 括如下之一: [Claim 7] The method according to claim 1 or 2, wherein controlling the return of the drone includes one of the following:
控制所述无人机返回通过所述遥控器的掰杆启动的位置所指示的返航 点; 控制所述无人机返回通过所述遥控器或地面站设置的返航点; 控制所述无人机返回预先设定的固定返航点。  Controlling the drone to return to a return point indicated by a position activated by the mast of the remote controller; controlling the drone to return to a return point set by the remote controller or the ground station; controlling the drone Returns the preset fixed return point.
[权利要求 8] —种无人机返航的控制装置, 其特征在于, 包括: [Claim 8] A control device for returning a drone, comprising:
返航模块, 用于根据第一控制信号控制所述无人机按预定路径返航; 第一接收模块, 用于在所述无人机按所述预定路径返航过程中, 接收 遥控器发送的第二控制信号, 其中, 所述第二控制信号用于调整所述 预定路径, 以使所述无人机躲避障碍物;  a returning module, configured to control the drone to return to the predetermined path according to the first control signal; the first receiving module, configured to receive the second sent by the remote controller during the return of the drone according to the predetermined path a control signal, wherein the second control signal is used to adjust the predetermined path to enable the drone to avoid obstacles;
叠加模块, 用于将所述第二控制信号与第一控制信号叠加, 得到叠加 控制信号, 其中, 所述第一控制信号为预定的控制所述无人机返航的 信号;  a superimposing module, configured to superimpose the second control signal and the first control signal to obtain a superimposed control signal, where the first control signal is a predetermined signal for controlling the return of the drone;
第一控制模块, 用于利用所述叠加控制信号, 控制所述无人机返航。  And a first control module, configured to control, by using the superposition control signal, the return of the drone.
[权利要求 9] 根据权利要求 8所述的装置, 其特征在于, 所述装置还包括: [Claim 9] The device according to claim 8, wherein the device further comprises:
检测模块, 用于在所述无人机返航过程中, 每隔预设吋间段, 检测所 述遥控器是否发送所述第二控制信号;  a detecting module, configured to detect, during every return period of the drone, whether the remote controller sends the second control signal;
第二接收模块, 用于若检测到所述遥控器发送所述第二控制信号, 则 接收所述遥控器发送的所述第二控制信号; a second receiving module, configured to: if it is detected that the remote controller sends the second control signal, Receiving the second control signal sent by the remote controller;
第二控制模块, 用于若未检测到所述遥控器发送所述第二控制信号, 则利用所述第一控制信号, 控制所述无人机返航。  a second control module, configured to control, by the first control signal, the return of the drone if the remote controller does not detect the second control signal being sent.
[权利要求 10] 根据权利要求 9所述的装置, 其特征在于, 所述装置还包括:  [Claim 10] The device according to claim 9, wherein the device further comprises:
生成模块, 用于在所述无人机处于返航过程之前, 按照预先定义的触 发方式, 生成自动返航触发信号;  a generating module, configured to generate an automatic returning trigger signal according to a predefined triggering manner before the drone is in a returning process;
触发模块, 用于在所述自动返航触发信号的触发下, 所述无人机进入 返航过程。  And a triggering module, configured to: when triggered by the automatic returning trigger signal, the drone enters a returning process.
PCT/CN2017/092051 2016-08-11 2017-07-06 Method and device for controlling unmanned aircraft to make return flight WO2018028364A1 (en)

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