WO2021258349A1

WO2021258349A1 - Test configuration method and apparatus for unmanned aerial vehicle, and terminal device

Info

Publication number: WO2021258349A1
Application number: PCT/CN2020/098181
Authority: WO
Inventors: 许晓航; 王璐; 何展鹏; 高雯娟
Original assignee: 深圳市大疆创新科技有限公司
Priority date: 2020-06-24
Filing date: 2020-06-24
Publication date: 2021-12-30

Abstract

A test configuration method and apparatus for an unmanned aerial vehicle, and a terminal device. The method comprises: receiving a configuration instruction input by a user by means of an interactive interface, the configuration instruction being used for indicating an action to be executed by an unmanned aerial vehicle during test and parameters related to the action; and generating, according to the configuration instruction, a configuration file indicating a test process of the unmanned aerial vehicle. According to the present application, by means of operation by a user on an interactive interface, an action to be executed by an unmanned aerial vehicle during test and parameters related to the action can be set, and a configuration file is generated, thereby achieving automatic generation of the configuration file, simplifying test configuration, requiring no manual and repeated modification of the configuration file, improving the test efficiency and reliability, and providing a more instructive test result for development of unmanned aerial vehicles.

Description

Test configuration method and device for unmanned aerial vehicle, terminal equipment

Technical field

This application relates to the field of testing, and in particular to a test configuration method and device for an unmanned aerial vehicle, and terminal equipment.

Background technique

Flight testing is an important link in the development of unmanned aerial vehicles. Its purpose is to verify the functions, performance and stability of unmanned aerial vehicles. Flight testing is mainly carried out manually, and manual testing is entirely dependent on the pilot’s manual control of various actions and parameters. , When there are multiple unmanned aerial vehicles that need to be tested, the pilot can only carry out the flight test of one unmanned aerial vehicle at a time, and cannot simultaneously carry out the flight test of multiple unmanned aerial vehicles. Therefore, the manual method will cost Huge manpower and low efficiency can not guarantee the repeatability and effectiveness of the test case execution. There are risks of missed and mistested tests, and the accuracy of test results is low.

Summary of the invention

This application provides a test configuration method and device for an unmanned aerial vehicle, and terminal equipment.

In the first aspect, an embodiment of the present application provides a test configuration method for an unmanned aerial vehicle, the method including:

Receiving a configuration instruction input by a user through an interactive interface, the configuration instruction being used to instruct the unmanned aerial vehicle to perform an action during the test and the parameters related to the action;

According to the configuration instruction, a configuration file indicating the testing process of the unmanned aerial vehicle is generated.

In the second aspect, an embodiment of the present application provides a test configuration device for an unmanned aerial vehicle, the device including:

Storage device for storing program instructions; and

One or more processors call program instructions stored in the storage device, and when the program instructions are executed, the one or more processors are individually or collectively configured to implement the following operations:

In a third aspect, an embodiment of the present application provides a terminal device that can communicate with an unmanned aerial vehicle, and the terminal device includes:

case;

A display module, arranged in the housing, the display module including an interactive interface; and

The test configuration device of the unmanned aerial vehicle described in the second aspect is supported by the casing and electrically connected to the display module.

According to the technical solutions provided by the embodiments of this application, this application can set the actions performed by the unmanned aerial vehicle during testing and the parameters related to the actions through the user's operation on the interactive interface, and generate a configuration file to realize the configuration file Compared with the method of manually modifying actions and parameters in the configuration file, the configuration file generation method of the embodiment of the present application not only simplifies the test configuration, but also does not have the problem of the name of the test case and the format of the configuration file, which improves The efficiency and reliability of the test provide more instructive test results for the development of UAVs.

Description of the drawings

In order to explain the technical solutions in the embodiments of the present application more clearly, the following will briefly introduce the drawings needed in the description of the embodiments. Obviously, the drawings in the following description are only some embodiments of the present application. For those of ordinary skill in the art, other drawings can be obtained based on these drawings without creative labor.

FIG. 1 is a schematic diagram of a method flow chart of a test configuration method of an unmanned aerial vehicle in an embodiment of the present application;

2A is a schematic diagram of an interactive interface in an embodiment of the present application;

2B is a schematic diagram of an interactive interface in another embodiment of the present application;

2C is a schematic diagram of an interactive interface in another embodiment of the present application;

2D is a schematic diagram of an interactive interface in another embodiment of the present application;

3 is a schematic diagram of a method flow chart of a test configuration method of an unmanned aerial vehicle in another embodiment of the present application;

Fig. 4 is a schematic structural diagram of a test configuration device for an unmanned aerial vehicle in an embodiment of the present application;

Fig. 5 is a schematic structural diagram of a terminal device in an embodiment of the present application.

detailed description

Manual testing requires each pilot to execute corresponding test cases according to requirements. This test method consumes a lot of manpower, is inefficient, cannot guarantee the repeatability and effectiveness of test case execution, and there is a risk of missed and false tests. The effect is less precise.

In this regard, the embodiment of the present application can set the actions performed by the unmanned aerial vehicle during testing and the parameters related to the actions through the operation of the user on the interactive interface, and generate the configuration file, which realizes the automatic generation of the configuration file. Compared with the manual modification of actions and parameters in the configuration file, the configuration file generation method of the embodiment of the present application not only simplifies the test configuration, but also has no problems with the name of the test case and the format of the configuration file, which improves the efficiency and reliability of the test. It provides more instructive test results for the development of unmanned aerial vehicles.

The technical solutions in the embodiments of the present application will be clearly and completely described below in conjunction with the drawings in the embodiments of the present application. Obviously, the described embodiments are only a part of the embodiments of the present application, rather than all the embodiments. Based on the embodiments in this application, all other embodiments obtained by a person of ordinary skill in the art without creative work shall fall within the protection scope of this application.

It should be noted that, in the case of no conflict, the following embodiments and features in the implementation can be combined with each other.

The unmanned aerial vehicle in the embodiment of this application may be an unmanned aerial vehicle, such as a multi-rotor unmanned aerial vehicle, a fixed-wing unmanned aerial vehicle, etc.; the unmanned aerial vehicle in the embodiment of this application may also be other types of unmanned aerial vehicles.

In addition, the flight test in the embodiments of the present application may be an outfield flight test, or may be a flight test in other scenarios.

FIG. 1 is a schematic diagram of the method flow chart of the test configuration method of the unmanned aerial vehicle in an embodiment of the present application; the execution subject of the test configuration method of the unmanned aerial vehicle in the embodiment of the present application is a device terminal, and the device terminal includes an interactive interface (or Called the UI interface). The device terminal in the embodiment of the present application may be a computer, a mobile phone, or other smart terminals. Referring to FIG. 1, the test configuration method of the unmanned aerial vehicle in the embodiment of the present application may include steps S101 to S102.

Among them, in S101, a configuration instruction input by a user through an interactive interface is received, and the configuration instruction is used to instruct the unmanned aerial vehicle to perform an action during a test and an action-related parameter.

The actions performed by the unmanned aerial vehicle during testing (hereinafter referred to as actions) may include the first action performed by the unmanned aerial vehicle itself and/or the second action performed by the load carried on the unmanned aerial vehicle, so as to affect the unmanned aerial vehicle itself and/ Or load the function to be tested. Exemplarily, in some embodiments, the action includes a first action or a second action; in other embodiments, the action includes a first action and a second action. It should be understood that the actions may also include other related actions of the UAV.

In the embodiment of the present application, the first action may include the flight action of the unmanned aerial vehicle and/or the first attitude change of the unmanned aerial vehicle, so as to test the flight and/or attitude change functions of the unmanned aerial vehicle, and obtain the characterization of the unmanned aerial vehicle. Performance and stability data during flight and/or attitude changes; it should be understood that the first action may also be other actions performed by the UAV itself.

Exemplarily, the first action is the flight action of the unmanned aerial vehicle, such as flying in different directions (such as at least two of the forward, backward, left and right sides of the unmanned aerial vehicle), turning around the yaw direction, Return home, landing, hovering, stopping, etc. The parameters related to flight actions may include at least one of flight direction, flight speed, flight distance, flight duration, number of flights, and flightable space range. Of course, the parameters related to flight actions are not limited to the above-listed parameters. It can be other parameters related to flight actions.

The parameters related to the flight action can be determined according to the type of the flight action. Illustratively, the parameters related to the flight in different directions can include the flight direction, flight speed, flight distance, flight duration, number of flights, and the range of space that can be flown. The parameters related to the heading rotation can include the direction of rotation, the angle of rotation, the duration of the rotation, and the number of rotations. The parameters related to the return can include the return speed and the number of return. The parameters related to the landing can include the direction of landing, the speed of landing, the distance of landing and the number of landings. , Hover-related parameters may include hover duration and hover times, and brake-related parameters may include brake distance, brake duration and number of brakes.

Among them, the space range that the unmanned aerial vehicle can fly is limited, which can prevent collisions between the unmanned aerial vehicles when multiple unmanned aerial vehicles are undergoing flight tests at the same time. The flying space range can include square space, spherical space or other shapes. Space. Optionally, the flightable space ranges corresponding to different unmanned aerial vehicles do not overlap. It should be noted that when multiple unmanned aerial vehicles are undergoing flight tests at the same time, the interval between the take-off points of the multiple unmanned aerial vehicles must be large enough to ensure that each unmanned aerial vehicle can fly within the corresponding flightable space without Interfere with the flight of other unmanned aerial vehicles.

Exemplarily, the first action is a first attitude change of the unmanned aerial vehicle, where the first attitude may include at least one of a yaw attitude, a pitch attitude, and a pitch attitude. The parameter related to the first posture change may include at least one of the magnitude of the posture change and the direction of the posture change. For example, in some embodiments, the parameter related to the first posture change is the magnitude of the posture change of the first posture. The attitude change direction may be the default attitude change direction; in other embodiments, the parameters related to the first attitude change include the attitude change direction of the first attitude, and the attitude change magnitude of the first attitude may be a default value; in other embodiments, In the embodiment, the parameters related to the first posture change include the magnitude and direction of the posture change of the first posture.

The load may include a photographing device, and the photographing device in the embodiment of the present application may be an integrated camera, or a non-integrated image sensor or others. The second action may include a shooting action of the shooting device, so as to test the shooting function of the shooting device and obtain data that characterizes the performance and stability of the shooting device during shooting. The shooting action in the embodiment of the present application may include photographing or video recording. The parameters related to photographing can include but are not limited to resolution, frame rate, number of frames, delay time, image mode, saturation, exposure compensation, white balance, storage format (e.g. RAW/JEPG), image ratio (e.g. 16:9) , 4:3), at least one of the shooting modes (such as single shooting/continuous shooting/timed shooting), the video-related parameters can include but not limited to resolution, frame rate, video duration, delay time, image mode , At least one of saturation, exposure compensation, white balance, and image ratio. Among them, the image mode can be a panoramic mode or a non-panoramic mode. It should be understood that the second action may also include other actions that can be performed by the camera.

Further, in some embodiments, the load may also include a pan/tilt for mounting the camera on the unmanned aerial vehicle. The pan/tilt in the embodiment of the present application may be a two-axis pan/tilt, a three-axis pan/tilt or other types of pan/tilt. Yuntai. The second action may also include a third action performed by the pan/tilt, so as to test the function of the pan/tilt; of course, the second action may also include other actions that the pan/tilt can perform. In the embodiment of the present application, the third action may include at least one of the second posture change of the pan/tilt and the function setting of the pan/tilt. Illustratively, in some embodiments, the third action is the second change of the pan/tilt. Posture change; in other embodiments, the third action is the function setting of the pan/tilt; in other embodiments, the third action includes the second posture change of the pan/tilt and the function setting of the pan/tilt.

Wherein, the second attitude may include at least one of a yaw attitude, a pitch attitude, and a pitch attitude. The parameter related to the second posture change may include at least one of the magnitude of the posture change and the direction of the posture change. Illustratively, in some embodiments, the parameter related to the second posture change is the magnitude of the posture change of the second posture. The attitude change direction of the attitude may be the default attitude change direction; in other embodiments, the parameter related to the second attitude change is the attitude change direction of the second attitude, and the attitude change magnitude of the second attitude may be the default value; In other embodiments, the parameters related to the second attitude change include the magnitude of the second attitude change and the direction of the attitude change.

Exemplarily, the function setting of the gimbal includes the following mode setting of the gimbal. The following mode of the gimbal may include the mode of the gimbal following the UAV or the mode of the UAV following the gimbal. In the aircraft mode, the control commands of the unmanned aerial vehicle are directly responded to by the unmanned aerial vehicle, and the gimbal reads the attitude of the unmanned aerial vehicle, such as reading the yaw attitude of the unmanned aerial vehicle as the target yaw attitude of the gimbal; In the mode of the aircraft following the gimbal, the UAV's yaw attitude control command is first sent to the gimbal. The gimbal first responds to the UAV's yaw attitude control command, and then the UAV reads the gimbal's yaw attitude as The target yaw attitude of the UAV. It should be understood that the function setting of the pan/tilt may also include other function settings of the pan/tilt, and is not limited to the follow mode setting of the pan/tilt.

In addition, the number of actions can be one or more, and the user can configure the number of actions as needed. Exemplarily, the number of actions is multiple, and the configuration instruction is also used to instruct the UAV to execute the sequence of multiple actions. When an unmanned aerial vehicle is testing, multiple actions can be executed at the same time, or executed sequentially in time, or some actions in the multiple actions are executed at the same time, and some actions are executed sequentially in time. Exemplarily, during the forward flight of the unmanned aerial vehicle, the camera performs video recording, and the second attitude of the pan/tilt changes.

In the embodiment of the present application, the parameter may include the number of executions of the action. For example, when the action is the flight action of the UAV, the parameter may include the number of flights; when the action is the first attitude change of the UAV, the parameter may include the number of the first attitude. The number of changes; when the action is a photo taken by a camera, the parameter can include the number of photos (one or more images can be taken each time); when the action is a video taken by the camera, the parameter can include the number of recordings; the action is the first of the PTZ 2. When the posture changes, the parameter may include the number of changes in the second posture; when the action is the function setting of the pan/tilt, the parameter may include the number of times the pan/tilt performs the function corresponding to the function setting.

The settable range of the size of the parameter is preset, that is, the user can set the size of the parameter within the preset effective value range. Illustratively, the settable range of the flight speed is greater than or equal to 0 m/s and less than or equal to 20 In the range of meters/second, the user can only set the flying speed of the UAV during flight test to be greater than or equal to 0 meters/second and less than or equal to 20 meters/second, thereby automatically limiting the size of the parameters within the effective range to ensure The effectiveness of the UAV test.

It should be understood that, in addition to actions and action-related parameters, configuration instructions can also be used to indicate other relevant information of the unmanned aerial vehicle, such as the model of the unmanned aerial vehicle and/or the hardware version number of the unmanned aerial vehicle and/or the unmanned aerial vehicle. The firmware version number of the aircraft, etc.

Configuration instructions can be completely customized and generated by the user through the interactive interface, or the user can rewrite the actions performed during the test of the UAV corresponding to the historical configuration file displayed on the interactive interface (hereinafter referred to as actions) and/or the parameters related to the actions. Generated by setting.

First, we will introduce the process of customizing the configuration instruction generated by the user through the interactive interface.

Exemplarily, before receiving the configuration instruction input by the user through the interactive interface, the first identifier of the action executable during the test of the unmanned aircraft and the second identifier of the parameter related to the action are displayed on the interactive interface. When receiving the configuration instruction input by the user through the interactive interface, the user's operations on the first identification and the second identification are acquired, and the configuration instructions input by the user are determined according to the operations on the first identification and the second identification. The interactive interface will display the first identification of all optional executable actions. The user can select one or more executable actions as the actions to be executed during the test of the UAV according to the test requirements, that is, the configuration instructions indicate The actions performed by the unmanned aerial vehicle during the test can be one or more of the actions that the unmanned aerial vehicle can perform during the test; at the same time, the user can interact with the selected second identifier of the parameter related to the executable action. The interface edits the parameters related to the selected executable action to complete the input of configuration instructions.

The executable action may include the first action and/or the second action, and may also include other actions. The user's operations on the first identifier and the second identifier may include at least one of click (including at least one of single-click, double-click, and long-press) and drag, and may also include other operations.

Exemplarily, before displaying the first identifier of the action executable by the UAV during the test and the second identifier of the action-related parameter on the interactive interface, the action adding identifier is displayed on the interactive interface. When a user operation (such as clicking, double-clicking or long-pressing and other click operations) adds an identifier, the first identifier of the action executable by the UAV during the test and the second identifier of the parameter related to the action are displayed on the interactive interface. For example, when the user operates an action to add a logo, the first logo of the executable action and the second logo of the parameter related to the action can be displayed by popping up a dialog box or switching to another display page. The display mode of the first logo and the second logo on the interactive interface can be set as required. For example, the first logo and the second logo can be displayed in a display mode such as a drop-down box or a tile. For example, please refer to Figure 2A. The first logo is displayed through a drop-down box. For example, an action addition logo 10 is displayed on the interactive interface. When the user operates an action to add logo 10, a drop-down box for displaying the first logo of the executable action is displayed on the interactive interface. You can click the first mark in the drop-down box as needed to select the actions to be performed when the UAV is tested. Exemplarily, the user clicks the first mark corresponding to the three executable actions of flying forward, hovering, and recording. The actions performed by the UAV during the test include flying forward, hovering, and recording, such as Shown in Figure 2B.

In addition, the first identification and the second identification can be presented in the form of words, symbols, pictures, etc., wherein the identification content of the first identification of each executable action is unique, thereby distinguishing different executable actions. Wherein, the identification content of the first identifier of each executable action is characterized by the Chinese name of the executable action. Please refer to Figure 2B. The identification content of the first identifier of flying forward is "fly forward", the first record of the video. The identification content of the first identification is "video", etc.; of course, the identification content of the first identification can also be characterized in other ways.

The identification content of the second identification may be determined according to the parameter type, wherein the identification content of the second identification of the same parameter of different executable actions may be the same or different. Exemplarily, the identification content of the second identification of the parameter 1 related to the executable action A is the same as the identification content of the second identification of the parameter 1 related to the executable action B. The identification content of the second identification of each parameter can be characterized by the Chinese name of the parameter and the identification corresponding to the edit box of the parameter. Please refer to Figure 2C. The identification content of the second identification of the number of flights includes "number of flights" and the number of flights. The identifier corresponding to the edit box.

Further, the second identification may be associated with the first identification, because the parameters related to different executable actions may be at least partially different, for example, the parameters related to the first action are different from the parameters related to the second action, and the second The identifier is associated with the first identifier, and the parameters related to each executable action can be displayed more clearly. Optionally, in some embodiments, before displaying the second identifier of the parameter related to the executable action on the interactive interface, it is detected that the first identifier corresponding to the executable action is selected, that is, only The second identifier of the executable action-related parameter corresponding to the currently selected first identifier is beneficial to the interactive interface to more clearly display the relationship between different executable actions and the action-related parameters. Exemplarily, please refer to Fig. 2C. When it is detected that the first sign "Fly forward" is selected, the second sign of forward flight related parameters will be displayed under the first sign of forward flight through the drop-down box. Logo.

The test configuration method of the unmanned aerial vehicle of the embodiment of the present application may further include: displaying the first identification of the selected action on the interactive interface and the sequence of executing the selected action when the unmanned aerial vehicle is performing the test (as shown in FIG. 2B "Order" column). As shown in Figure 2B, the selected actions include forward flying, hovering and recording, and the corresponding first identifiers are "forward flying", "hovering", and "recording" respectively. The corresponding unmanned aerial vehicle is tested The order of execution is "1", "2", "1, 2", respectively.

In some embodiments, the order in which the unmanned aerial vehicle performs the selected actions during the test is related to the order in which the first identifier is selected (the "#" column in Figure 2B). Optionally, the unmanned aerial vehicle performs the test The order in which the selected actions are executed at the time is the same as the order in which the first identifier is selected. Exemplarily, when the user performs the test configuration, he first selects the first indicator that is flying forward, and then selects the first indicator that is hovering. Therefore, when the unmanned aerial vehicle performs the test, it first flies forward and then hoveres. Optionally, numbers are used to characterize the sequence of actions that have been selected when the unmanned aerial vehicle is tested. Illustratively, the smaller the number corresponding to the sequence of the actions that have been selected, indicates that the unmanned aerial vehicle will execute the selected actions when testing. The earlier the selected action is, please refer to Figure 2B. When the UAV is testing, the order of flying forward is 1, and the order of hovering is 2, that is, when the UAV is testing, it will fly forward first, and then fly forward. Hover. It should be understood that other methods can also be used to characterize the sequence of actions that have been selected when the UAV is performing a test.

In other embodiments, the order in which the UAV performs the selected actions during the test is set by the user, and has nothing to do with the order in which the first identifier is selected. Exemplarily, when the user performs the test configuration, the unmanned aerial vehicle needs to perform video recording during the two processes of forward flight and hovering. Then the user performs the test configuration, the order of recording may include the unmanned aerial vehicle The order of flying forward and the order of hovering during the test. Exemplarily, numbers are used to characterize the sequence of actions that have been selected when the unmanned aerial vehicle is tested. Please refer to Figure 2B again. When the user sets the unmanned aerial vehicle for testing, the order of recording is set to 1 and 2, which means that the unmanned aerial vehicle is tested. When the aircraft is being tested, the camera will record video during forward flight and hovering.

The test configuration method of the unmanned aerial vehicle of the embodiment of the present application may further include: displaying on the interactive interface the edit identifier associated with the selected action, as shown in FIG. 2B, the edit identifier associated with the forward flight and the edit identifier associated with the hover And the edit ID associated with the video. When the user operates (such as clicking, double-clicking or long-pressing, etc.) to edit the logo, enter the action setting page. For example, see Figure 2D. When the user clicks the edit logo associated with the forward flight, the user enters the forward flight Action settings page.

In some embodiments, according to the user's operation on the action setting page, the currently associated action of the edit ID is replaced with the reselected action. For example, please refer to Figure 2D again. Actions, such as flying backwards, flying left, flying right, taking photos, recording videos, etc., the user can select on the action setting page of flying forwards (you can select by single-click, or select by other methods) after replacement To replace the forward-flying action with the re-selected action. It should be noted that the forward flying action setting page can also display the forward flying action. If the user selects the forward flying action on the forward flying action setting page, it means that there is no need to replace the forward flying action. action.

In other embodiments, the parameters related to the currently associated action are modified and edited according to the user's operation on the action setting page. In this embodiment, the action setting page displays the parameters related to the action currently associated with the edit ID, and the user can perform operations on the action setting page (this operation can include keyboard or mouse input and/or single-click, double-click, long-press and other clicks) Operation) to modify the size and/or type of the corresponding parameter.

The test configuration method of the unmanned aerial vehicle in the embodiment of the application further includes: displaying the chief editor logo on the interactive interface, see Figures 2A to 2D, the chief editor logo is 20, when the user operates (such as single click, double click or long press Wait for click operation) When the general editing logo, you can modify all the currently selected actions separately, such as replacing some selected actions with reselected actions, and/or changing some parameters related to the selected actions Modify the size of to other values and so on.

The test configuration method of the unmanned aerial vehicle of the embodiment of the present application may further include: displaying the deletion identifier associated with the selected action on the interactive interface. When the user operates (such as clicking, double-clicking, or long-pressing, etc.) to delete the logo, the action associated with the deletion of the logo will be deleted. Exemplarily, please refer to FIG. 2B. When the user operates the forward flight associated deletion identifier, the forward flight action that has been selected during the test configuration is deleted.

The test configuration method of the unmanned aerial vehicle in the embodiment of the application may further include: displaying the total delete flag on the interactive interface, and when the user operates the total delete flag (such as single-click, double-click, or long-press and other click operations), delete all the current deleted flags. The selected action.

The test configuration of the unmanned aerial vehicle in the embodiment of the present application further includes: displaying the update time of the selected action on the interactive interface, so that the user can know the update time of each selected action.

The above is the process of user-defined generation of configuration instructions through the interactive interface.

The following describes the process of the user resetting the actions and/or action-related parameters corresponding to the historical configuration files displayed on the interactive interface to generate configuration instructions.

In this embodiment, the configuration instruction is generated based on the test process of the UAV corresponding to the historical configuration file. Exemplarily, before receiving the configuration instruction input by the user through the interactive interface, the file import instruction input by the user through the interactive interface is obtained, and the file import instruction is used to indicate the file information of the historical configuration file to be imported, such as the name of the historical configuration file , The location information of the location where the historical configuration file is saved, etc. The historical configuration file can be saved locally or on an external device. The terminal device can communicate with the external device to obtain the historical configuration file. Further, according to the file import instruction, the historical configuration file is imported, and the test process of the UAV corresponding to the historical configuration file is displayed on the interactive interface. The test process of the UAV corresponding to the historical configuration file can reflect the historical test configuration information. The user can reconfigure on the basis of the historical test configuration information displayed on the interactive interface to obtain a new configuration file to save the configuration process. time spent. Among them, the file import instruction can be generated by a user operation (such as a click operation such as a single click, double click, or long press) of the file import instruction option displayed on the interactive interface (which can be characterized by a virtual button).

The configuration instruction in this embodiment may include at least one of a modification instruction, a new instruction, and a deletion instruction, but is not limited thereto. Among them, the modification instruction is used to instruct to replace the actions included in the test process of the UAV corresponding to the historical configuration file with new actions, and/or to change the relevant parameters of the actions included in the test process of the UAV corresponding to the historical configuration file The size of is set to the new value size. The new instruction is used to instruct to add new actions during the test process of the UAV corresponding to the historical configuration file, and/or add new related parameters to the actions included in the test process of the UAV corresponding to the historical configuration file. The delete instruction is used to instruct to delete the actions included in the test process of the UAV corresponding to the historical configuration file, and/or delete related parameters of the actions included in the test process of the UAV corresponding to the historical configuration file. By modifying, adding, and/or deleting historical test configuration information, this test configuration method is more convenient.

In S102, according to the configuration instruction, a configuration file indicating the testing process of the unmanned aerial vehicle is generated.

In this embodiment of the application, the configuration file can be a preset template file, such as a json (JavaScript Object Notation, JS object notation, which is a lightweight data exchange format) file; of course, the template file can also be an unmanned aerial vehicle Other template files that can be recognized.

The content of the preset field in the template file can be modified. The embodiment of the present application implements the modification of the content of the preset field through an interactive interface. The modification method of the embodiment of the present application is more intuitive, convenient, and has a lower error rate. Exemplarily, the preset fields include fields corresponding to actions and fields corresponding to action-related parameters. The user can modify the content of actions and action-related parameters through an interactive interface to realize the configuration of actions and action-related parameters. In this way, the content of the preset fields in the configuration file can be determined through the configuration instructions, so that different configuration files can be generated according to different configuration instructions. It should be understood that the preset field may also include other fields, such as a field corresponding to the model number of the unmanned aerial vehicle and/or the hardware version number of the unmanned aerial vehicle and/or the firmware version number of the unmanned aerial vehicle.

The configuration file can be generated by different triggering methods. For example, when the file generation instruction input by the user through the interactive interface is obtained, the configuration file indicating the testing process of the unmanned aerial vehicle is generated according to the configuration instruction. Among them, the file generation instruction can be generated by user operations (such as click operations such as single-click, double-click, or long-press) of the file generation instruction options displayed on the interactive interface (which can be characterized by virtual buttons). Exemplarily, when the user finishes configuring the return home and return home related parameters, according to the configuration instruction, a configuration file indicating the test process of the unmanned aerial vehicle is generated.

It should be noted that if the configuration command is generated based on a historical configuration file, then the configuration file generated based on the configuration command can be modified on the basis of the historical configuration file, or it can be a historical configuration file without any modification. .

Further, in some embodiments, after generating the configuration file indicating the test process of the UAV according to the configuration instruction, the configuration file is exported and saved, and the configuration file can be exported and saved locally, which is convenient for subsequent direct import and editing. It is suitable for common test scenarios; the configuration file can also be exported to an external device and saved, depending on the specific needs to select the save location of the configuration file.

The configuration file can be exported and saved in different triggering methods. For example, when the file export instruction input by the user through the interactive interface is obtained, the configuration file is exported. Wherein, the file export instruction is used to indicate the location information of the location of the configuration file to be saved. According to the location information, save the configuration file. The file export instruction can be generated by the user's operation (such as clicking, double-clicking, or long-pressing, etc.) of the option of the file export instruction displayed on the interactive interface (which can be characterized by a virtual button). Referring to Figures 2A to 2D, when the user clicks option 30 of the file export instruction, the configuration file is exported and the configuration file is saved to the location of the configuration file designated by the user. Of course, other methods can also be used to trigger the export and save the configuration file.

After the configuration file is generated, the automatic test of the unmanned aerial vehicle can be triggered. In the embodiment of the present application, after the configuration file indicating the test process of the unmanned aerial vehicle is generated according to the configuration instruction, the configuration file is imported to the unmanned aerial vehicle to make the unmanned aerial vehicle Test based on the configuration file. In this way, compared to manual testing, a set of configuration files can be applied to multiple unmanned aerial vehicles, without the need for individual pilots to manually operate the unmanned aerial vehicles, so as to avoid the problem of inconsistent operation of each pilot, and can also achieve simultaneous pairing. The test of multiple unmanned aerial vehicles is helpful to improve the test efficiency.

The configuration file can be imported into the UAV using different triggering methods. For example, after the configuration file is generated, if a test trigger instruction input by the user through the interactive interface is received, the configuration file is imported into the UAV. Among them, the test trigger instruction can be generated by a user operation (such as a click operation such as a single click, double tap, or long press) of the test trigger instruction option displayed on the interactive interface (which can be characterized by a virtual button). Exemplarily, after the configuration file is generated, the configuration file is directly imported into the unmanned aerial vehicle.

Before the automatic test of the unmanned aerial vehicle, the user is required to place the unmanned aerial vehicle in a designated position and turn it on, and then the unmanned aerial vehicle automatically executes actions according to the configuration file; when the action is completed, the unmanned aerial vehicle will automatically return to the take-off point.

In addition, in some embodiments, the test configuration method of the unmanned aerial vehicle may further include: after importing the configuration file into the unmanned aerial vehicle so that the unmanned aerial vehicle performs tests based on the configuration file, importing the new configuration file into the unmanned aerial vehicle, This allows the unmanned aerial vehicle to replace the configuration file with a new configuration file and perform tests based on the new configuration file. Exemplarily, after the configuration file is imported into the unmanned aerial vehicle so that the unmanned aerial vehicle performs a test based on the configuration file, the new configuration file is imported into the unmanned aerial vehicle through the operation interactive interface, so that the unmanned aerial vehicle replaces the configuration file with the new one. The configuration file is tested based on the new configuration file. The configuration file in the UAV can be replaced through the operation of the interactive interface. The replacement method is simple and quick.

The current flight test also relies heavily on manual operation in terms of result statistics, which is not only inefficient, but also has the risk of error. It is not suitable for large-scale unmanned aerial vehicle flight tests. On the other hand, due to massive data and manpower constraints, it is difficult to Analyze and display a large amount of test data over a period of time, and it does not support the quality scoring of each unmanned aerial vehicle. Regarding this, in the embodiment of the present application, after the test is completed, the test data of the unmanned aerial vehicle can be collected, summarized and analyzed for visual display, which is suitable for large-scale unmanned aerial vehicle flight testing. Exemplarily, referring to Fig. 3, after the configuration file is imported into the unmanned aerial vehicle, the test configuration method of the unmanned aerial vehicle may further include steps S301 to S302.

Among them, in S301, the test data of the unmanned aerial vehicle stored in the storage device of the unmanned aerial vehicle is acquired.

The storage device in the embodiment of the application may be an SD card (Secure Digital Memory Card) of an unmanned aerial vehicle. During the test of the unmanned aerial vehicle, the test data will be saved in the SD card; of course, the storage device can also be Other equipment used to save test data during the testing of unmanned aerial vehicles.

The test data may include at least one of the first performance data when the unmanned aerial vehicle performs the first action and the second performance data when the load mounted on the unmanned aerial vehicle performs the second result of the second action. Exemplarily, the first performance data may include the overall performance data of the unmanned aerial vehicle and/or the performance data of different functional modules of the unmanned aerial vehicle, etc., where the overall performance data may include the power consumption and flight control of the unmanned aerial vehicle. The usage rate of the device, the operating frequency of the memory, etc. The functional modules may include software modules and/or hardware modules of the unmanned aerial vehicle. Illustratively, the performance data of the different functional modules of the unmanned aerial vehicle may include the performance data of the battery of the unmanned aerial vehicle, the obstacle avoidance module, etc., and the performance data of the battery. It may include the current, voltage, power consumption, maximum current value, etc. of each cell, and the performance data of the obstacle avoidance module may include the success rate of obstacle avoidance.

Exemplarily, the load is a photographing device, and the second performance data may include image information of the image photographed by the photographing device, such as the degree of color cast and brightness. Exemplarily, the load is a gimbal, and the second performance data may include changes in the angle of the gimbal, such as changes in yaw angle, pitch angle, and so on.

The test data of the UAV stored in the storage device of one or more UAVs can be obtained, so the test data can include the test data of the same UAV or the same type of UAV in different time periods, and the test data of different types of unmanned aerial vehicles. At least one of the test data of a human aircraft in the same time period, and the test data of the same UAV or UAV of the same model using different versions of firmware or hardware.

It should be noted that the test data of the unmanned aerial vehicle stored in the storage device is classified data, that is, the unmanned aerial vehicle classifies the test data during the test process, and saves the classified test data in the storage device. Exemplarily, the unmanned aerial vehicle may classify the test data according to the functional modules. For example, the test data of the same functional module is stored in the same file, and the test data of different functional files are stored in different files.

In S302, the test result obtained based on the test data analysis is displayed through the interactive interface.

Through automatic analysis of test data, the test results obtained are highly reliable. This method can quickly analyze massive test data and improve efficiency.

The test result may include at least one of the first result of the first action performed by the unmanned aerial vehicle, the second result of the second action performed by the load, the change information of the first performance data over time, and the change information of the second performance data over time. A sort of. The first result can be used to indicate the success of the UAV in performing the first action, and the second result can be used to indicate the success of the load in the second action.

The test results can be presented in the form of curves, data, etc., for example, the first result and the second result are represented by data, and the change information of the first performance data over time and the change information of the second performance data over time are represented by a change curve.

After obtaining the test data, the terminal device analyzes the test data offline and obtains the test result, or after obtaining the test data, the terminal device uploads the test data to the server, and the server analyzes the test data online to obtain the test result. The terminal device offline analyzes the test data and obtains the test result, which makes other terminal devices unable to obtain the test result in time, and the server analyzes the test data and obtains the test result online, so that other terminal devices can also obtain the test result in time.

Exemplarily, after acquiring the test data of the unmanned aerial vehicle stored in the storage device of the unmanned aerial vehicle, and before displaying the test result obtained based on the analysis of the test data, upload the test data to the server for analysis, and the acquisition server analyzes the test data to obtain The test results are convenient for sharing test results. Optionally, the terminal device may upload the test data to the server through the user operation interactive interface after acquiring the test data; optionally, the terminal device may directly upload the test data to the server after acquiring the test data. In addition, the terminal device can obtain the test results obtained by analyzing the test data by the server through a request method. Illustratively, after the terminal device uploads the test data to the server, it sends an acquisition request to the server to obtain the server's analysis of the test data. It should be understood that the terminal device can also obtain the test results obtained by the server's analysis of the test data in other ways. For example, after the server analyzes the test data to obtain the test results, it actively sends the test results to the uploader of the test data. Terminal Equipment.

Further, in some embodiments, after obtaining the test data of the unmanned aerial vehicle stored in the storage device of the unmanned aerial vehicle, the score of the unmanned aerial vehicle obtained based on the test result is displayed through the interactive interface, thereby visually presenting the unmanned aerial vehicle to the user The quality of the product, to provide users with instructive conclusions. Among them, the process of obtaining an unmanned aerial vehicle's score based on the test result can be implemented through a terminal device or through a server.

The score may include the score of the entire UAV and/or the scores of different functional modules of the UAV, where the entire aircraft includes all the functional modules of the UAV, and the functional modules can perform corresponding actions. Exemplarily, in some embodiments, the score is the score of the entire UAV; in other embodiments, the score is the score of different functional modules of the UAV; in other embodiments, the score includes no The score of the whole aircraft of the human aircraft and the score of the different functional modules of the unmanned aircraft.

The score can be characterized by a score method, or by a degree of excellence (such as excellent, fair, or poor). In the embodiments of the present application, the score is characterized by a score method.

Optionally, the score of the whole machine is obtained by weighting based on the scores of each functional module. The weight of each functional module can be set according to needs. Illustratively, the weight of each functional module is positively related to the degree of importance, such as the importance of the battery. The degree is higher than the importance of the obstacle avoidance module, so the weight of the battery is greater than the weight of the obstacle avoidance module. Of course, the score of the whole machine can also be obtained by directly adding the scores of each functional module.

Optionally, the score of the function module is determined based on the first score and the second score, where the first score is determined based on the result of the function module performing the corresponding action, and the second score is determined based on the function module performing the corresponding action. The performance data is determined, and the result is used to indicate the success or failure of the function module to perform the corresponding action. Exemplarily, the score of the functional module is obtained by weighting based on the first score and the second score; exemplary, the score of the functional module is obtained based on the direct addition of the first score and the second score. It should be understood that the scoring of the functional modules may also adopt other methods.

According to the difference between the scores of multiple unmanned aerial vehicles of the same model, it can be judged whether the unmanned aerial vehicle is qualified. For example, a large difference in score indicates that the corresponding unmanned aerial vehicle is unqualified; a small difference in score indicates that the corresponding unmanned aerial vehicle is unqualified. The unmanned aerial vehicle is qualified. According to the average value of the scores of multiple UAVs of the same model, it can be determined whether the score difference is large or small. When the difference between the mean values is less than or equal to the preset threshold, it means that the score difference is small.

According to the difference between the scores of different versions of software (including firmware) and/or hardware for the same model of UAV, it can be judged whether the UAV's performance has improved after using different versions of software and/or hardware. . For example, after the software and/or hardware of the unmanned aerial vehicle is updated, it can be determined whether the software and/or hardware of the unmanned aerial vehicle has achieved the expected optimization effect according to the scores of the unmanned aerial vehicle before and after the software and/or hardware update. Exemplarily, according to the difference between the scores of the same type of UAV using different versions of firmware, it is determined whether the performance of the UAV is improved after using different versions of the firmware, so as to realize the evaluation of the different versions of the firmware; Exemplarily, according to the difference between the scores of the same model of UAV using different versions of hardware, it is judged whether the performance of the UAV is improved after using different versions of hardware, so as to realize the evaluation of different versions of hardware. If the hardware is a hardware structure of an unmanned aerial vehicle that is more sensitive to vibration, the shape of the hardware structure can be improved to determine whether the vibration is reduced according to the difference between the ratings of the unmanned aerial vehicle before and after the shape of the hardware structure is changed.

The performance of the unmanned aerial vehicle can be judged according to the difference between the ratings of different types of unmanned aerial vehicles.

Further, in some embodiments, a historical test database can also be generated to save historical test results. In this embodiment, the test configuration method of the unmanned aerial vehicle may further include: storing test results in a historical test database. Exemplarily, the historical test database is used to store the identity information of the unmanned aerial vehicle, the test related information when the unmanned aerial vehicle is being tested, and the test result of the unmanned aerial vehicle in a one-to-one correspondence. Among them, the identity information may include information such as the model, SN (Serial Number), batch, and department of the unmanned aerial vehicle, and the test-related information may include at least one of test time, test location, and firmware version information. kind.

In addition, the user can query historical test results. Illustratively, the UAV test configuration method may further include: acquiring historical data query instructions input by the user through the interactive interface, where the historical data query instructions are used to indicate the query to be queried The identity information and/or test-related information of the unmanned aerial vehicle. According to the identity information and/or test-related information, the corresponding test results are obtained from the historical test database, and the currently obtained test results are displayed through the interactive interface, realizing the query and visual display of the historical test results. Exemplarily, in some embodiments, the historical data query instruction is used to indicate the identity information of the unmanned aerial vehicle to be queried; in other embodiments, the historical data query instruction is used to indicate the test related information of the unmanned aerial vehicle to be queried In other embodiments, the historical data query instruction is used to indicate the identity information and test-related information of the unmanned aerial vehicle to be queried.

Further, in some embodiments, the test configuration method of the unmanned aerial vehicle may further include: displaying the associated identification of each test result in the currently obtained test results on the interactive interface, and when the user operates (including single click, double click, Long press and other click operations) When the associated identifier is associated, the corresponding test result is processed based on the indication content of the associated identifier. The associated identifier may include a download identifier, a favorite identifier, or others. For example, the associated identifier is a download identifier. When the user operates the download identifier, the corresponding test result is downloaded; for example, the associated identifier is a favorite identifier, when the user operates the favorite identifier. When, collect the corresponding structure.

In addition, the user can also perform batch processing on multiple test results selected by the user through the interactive interface, such as batch download or batch, by operating the batch processing identifier displayed on the interactive interface (including click operations such as single-click, double-click, long-press, etc.) Collection etc.

The user can also compare multiple test results selected by the user through the interactive interface by operating the comparison mark displayed on the interactive interface, and obtain the comparison results of the test results of the same unmanned aerial vehicle or the same model of unmanned aerial vehicle in different time periods , And/or the comparison results of the test results of different types of unmanned aerial vehicles at the same time period, and/or the comparison results of the test results of the same unmanned aerial vehicle or the same type of unmanned aerial vehicle using different versions of firmware or hardware , So as to provide users with instructive conclusions.

The embodiment of this application automatically summarizes and displays the test results of unmanned aerial vehicles, so that users can see the test results more quickly and intuitively; at the same time, the embodiments of this application provide a mechanism for scoring the quality of unmanned aerial vehicles, and the results are accurate and reliable, and can be more accurate and reliable. It directly reflects the quality of the UAV's performance and stability, and provides more reference information for the development of unmanned aerial vehicles, which can greatly improve the efficiency and effectiveness of testing.

Corresponding to the test configuration method of the unmanned aerial vehicle in the foregoing embodiment, the embodiment of the present application also provides a test configuration device of the unmanned aerial vehicle. Referring to FIG. 4, the test configuration device of the unmanned aerial vehicle in the embodiment of the present application may include a storage device and one or more processors.

Among them, the storage device is used to store program instructions. The storage device stores a computer program of executable instructions for the test configuration method of the UAV, and the storage device may include at least one type of storage medium. The storage medium includes flash memory, hard disk, multimedia card, card-type memory (for example, , SD or DX memory, etc.), random access memory (RAM), static random access memory (SRAM), read-only memory (ROM), electrically erasable programmable read-only memory (EEPROM), programmable read-only memory ( PROM), magnetic storage, magnetic disks, optical disks, etc. Moreover, the test configuration device of the UAV can cooperate with a network storage device that performs the storage function of the memory through a network connection. The memory may be an internal storage unit of the test configuration device of the unmanned aerial vehicle, such as the hard disk or memory of the test configuration device of the unmanned aerial vehicle. The memory can also be an external storage device of the test configuration device of the UAV, such as the plug-in hard disk equipped on the test configuration device of the UAV, Smart Media Card (SMC), Secure Digital (SD) ) Card, Flash Card, etc. Further, the memory may also include both the internal storage unit of the test configuration device of the unmanned aerial vehicle and the external storage device. The memory is used to store computer programs and other programs and data required by the device. The memory can also be used to temporarily store data that has been output or will be output.

One or more processors call the program instructions stored in the storage device. When the program instructions are executed, the one or more processors are individually or collectively configured to perform the following operations: receive user input through the interactive interface Configuration instructions, the configuration instructions are used to instruct the unmanned aerial vehicle to perform actions and parameters related to the actions; according to the configuration instructions, a configuration file indicating the testing process of the unmanned aerial vehicle is generated.

The processor of this embodiment can implement the test configuration method of the unmanned aerial vehicle in the embodiments shown in FIGS. 1 and 3 of this application. For details, please refer to the test configuration method of the unmanned aerial vehicle in the above embodiment for the test configuration of the unmanned aerial vehicle in this embodiment. The configuration device is explained.

The processor may be a central processing unit (Central Processing Unit, CPU), or other general-purpose processors, digital signal processors (Digital Signal Processor, DSP), application specific integrated circuits (ASIC), on-site Field-Programmable Gate Array (FPGA) or other programmable logic devices, discrete gates or transistor logic devices, discrete hardware components, etc. The general-purpose processor may be a microprocessor or the processor may also be any conventional processor or the like.

An embodiment of the present application also provides a terminal device, which can be communicatively connected with an unmanned aerial vehicle. Referring to FIG. 5, the terminal device may include a housing, a display module, and the test configuration device of the unmanned aerial vehicle in the foregoing embodiment. Wherein, the display module is arranged on the casing, and the display module includes an interactive interface. The test configuration device of the unmanned aerial vehicle is supported by the casing and is electrically connected to the display module.

In addition, an embodiment of the present application also provides a computer-readable storage medium on which a computer program is stored, and when the program is executed by a processor, the steps of the test configuration method of the unmanned aerial vehicle of the foregoing embodiment are implemented.

The computer-readable storage medium may be an internal storage unit of the terminal device described in any of the foregoing embodiments, such as a hard disk or a memory. The computer-readable storage medium may also be an external storage device of the terminal device, such as a plug-in hard disk, a smart media card (SMC), an SD card, a flash memory card (Flash Card), etc. equipped on the device . Further, the computer-readable storage medium may also include both an internal storage unit of the terminal device and an external storage device. The computer-readable storage medium is used to store the computer program and other programs and data required by the terminal device, and can also be used to temporarily store data that has been output or will be output.

Those of ordinary skill in the art can understand that all or part of the processes in the above-mentioned embodiment methods can be implemented by instructing relevant hardware through a computer program. The program can be stored in a computer readable storage medium. During execution, it may include the processes of the above-mentioned method embodiments. Wherein, the storage medium can be a magnetic disk, an optical disc, a read-only memory (Read-Only Memory, ROM), or a random access memory (Random Access Memory, RAM), etc.

The above-disclosed are only some of the embodiments of this application, which of course cannot be used to limit the scope of rights of this application. Therefore, equivalent changes made in accordance with the claims of this application still fall within the scope of this application.

Claims

An unmanned aerial vehicle test configuration method, characterized in that the method includes:

Receiving a configuration instruction input by a user through an interactive interface, the configuration instruction being used to instruct the unmanned aerial vehicle to perform an action during the test and the parameters related to the action;

According to the configuration instruction, a configuration file indicating the testing process of the unmanned aerial vehicle is generated.
The method according to claim 1, wherein the configuration file is a preset template file, and the content of the preset fields in the template file can be modified.
The method according to claim 2, wherein the preset field includes a field corresponding to the action and a field corresponding to a parameter related to the action.
The method according to claim 1, wherein the action comprises a first action performed by the UAV itself and/or a second action performed by a load carried on the UAV.
The method according to claim 4, wherein the first action includes a flight action of the UAV.
The method according to claim 5, wherein the parameters related to the flight maneuver include at least one of a flight direction, a flight speed, a flight distance, a flight duration, a number of flights, and a flightable space range.
The method according to claim 4, wherein the first action includes a first attitude change of the UAV.
The method according to claim 7, wherein the parameter related to the first attitude change includes at least one of the magnitude of the attitude change and the direction of the attitude change.
The method according to claim 4, wherein the load includes a photographing device, and the second action includes a photographing action of the photographing device.
The method according to claim 9, wherein the shooting action includes taking a photo or video.
The method according to claim 10, wherein the parameters related to the photographing include resolution, frame rate, number of frames, delay time, image mode, saturation, exposure compensation, white balance, storage format, image ratio , At least one of the camera modes; or

The video-related parameters include at least one of resolution, frame rate, video duration, delay time, image mode, saturation, exposure compensation, white balance, and image ratio.
The method according to claim 9, wherein the load further comprises a pan/tilt used to mount the camera on the unmanned aerial vehicle, and the second action further comprises a pan/tilt performed by the pan/tilt. The third action.
The method according to claim 12, wherein the third action includes at least one of a second posture change of the pan/tilt and a function setting of the pan/tilt.
The method according to claim 13, wherein the parameter related to the second attitude change includes at least one of the magnitude of the attitude change and the direction of the attitude change.
The method according to claim 1, wherein the parameter includes the number of executions of the action.
The method according to claim 1, wherein the settable range of the size of the parameter is preset.
The method according to claim 1, wherein the actions include multiple, and the configuration instruction is further used to instruct the UAV to perform multiple sequences of the actions.
The method according to claim 1, wherein before the receiving a configuration instruction input by a user through an interactive interface, the method further comprises:

Displaying a first identifier of an action executable by the UAV during testing and a second identifier of the parameter related to the action on the interactive interface;

The receiving the configuration instruction input by the user through the interactive interface includes:

Acquiring the user's operations on the first identifier and the second identifier;

According to the operations on the first identifier and the second identifier, the configuration instruction input by the user is determined.
The method according to claim 18, characterized in that before the first identifier of the action executable by the UAV during the test and the second identifier of the parameter related to the action are displayed on the interactive interface ,Also includes:

Displaying an action addition mark on the interactive interface;

The displaying on the interactive interface the first identifier of the action executable by the UAV during the test and the second identifier of the parameter related to the action includes:

When the user operates the action to add an identifier, the first identifier of the action executable by the UAV during the test and the second identifier of the parameter related to the action are displayed on the interactive interface.
The method according to claim 18, wherein before displaying the second identifier of the parameter related to the action on the interactive interface, the method further comprises:

It is detected that the first identifier corresponding to the action is selected.
The method according to claim 18, further comprising:

The first identifier of the selected action and the sequence in which the selected action is executed when the UAV is performing a test are displayed on the interactive interface.
The method according to claim 21, further comprising:

Displaying the edit identifier associated with the selected action on the interactive interface;

When the user operates the edit flag, enter the action setting page;

According to the user's operation on the action setting page, the action currently associated with the edit ID is replaced with a reselected action, or the parameters related to the action currently associated with the edit ID are modified.
The method according to claim 21, further comprising:

Displaying the deletion identifier associated with the selected action on the interactive interface;

When the user operates the deletion indicator, the action associated with the deletion indicator is deleted.
The method according to claim 21, further comprising:

The update time of the selected action is displayed on the interactive interface.
The method according to claim 21, wherein the order is related to the order in which the first identifier is selected.
The method according to claim 1, wherein the generating a configuration file indicating the testing process of the unmanned aerial vehicle according to the configuration instruction comprises:

When the file generation instruction input by the user through the interactive interface is obtained, a configuration file indicating the testing process of the unmanned aerial vehicle is generated according to the configuration instruction.
The method according to claim 1, wherein after generating a configuration file indicating a test process of the UAV according to the configuration instruction, the method further comprises:

Export and save the configuration file.
The method according to claim 27, wherein said exporting and saving said configuration file comprises:

Export the configuration file when the file export instruction input by the user through the interactive interface is obtained, where the file export instruction is used to indicate the location information of the location where the configuration file is to be saved;

Save the configuration file according to the location information.
The method according to claim 1, wherein before the receiving a configuration instruction input by a user through an interactive interface, the method further comprises:

Acquiring a file import instruction input by the user through the interactive interface, where the file import instruction is used to indicate the file information of the historical configuration file to be imported;

Import the historical configuration file according to the file import instruction;

Displaying the test process of the unmanned aerial vehicle corresponding to the historical configuration file on the interactive interface;

Wherein, the configuration instruction is generated based on the test process of the unmanned aerial vehicle corresponding to the historical configuration file.
The method according to claim 29, wherein the configuration instruction includes at least one of a modification instruction, a new addition instruction, and a deletion instruction;

Wherein, the modification instruction is used to instruct to replace the actions included in the test process of the UAV corresponding to the historical configuration file with new actions, and/or to change the unmanned aerial vehicle corresponding to the historical configuration file. The size of the related parameters of the actions included in the test process of the aircraft is set to a new value;

The newly added instruction is used to instruct to add a new action in the test process of the UAV corresponding to the historical configuration file, and/or the test process of the UAV corresponding to the historical configuration file includes Add new relevant parameters for the action;

The deletion instruction is used to instruct to delete the actions included in the test process of the UAV corresponding to the historical configuration file, and/or delete the actions included in the test process of the UAV corresponding to the historical configuration file Related parameters.
The method according to claim 1, wherein after generating a configuration file indicating a test process of the UAV according to the configuration instruction, the method further comprises:

Import the configuration file into the unmanned aerial vehicle, so that the unmanned aerial vehicle performs a test based on the configuration file.
The method according to claim 31, wherein said importing said configuration file into said unmanned aerial vehicle comprises:

When a test trigger instruction input by the user through the interactive interface is received, the configuration file is imported into the unmanned aerial vehicle.
The method according to claim 31, wherein after the importing the configuration file into the UAV, the method further comprises:

Acquiring the test data of the unmanned aerial vehicle stored in the storage device of the unmanned aerial vehicle;

The interactive interface displays the test results obtained based on the test data analysis.
The method according to claim 33, wherein after said acquiring the test data of the unmanned aerial vehicle stored in the storage device of the unmanned aerial vehicle, before the displaying the test result obtained based on the analysis of the test data ,Also includes:

Upload the test data to the server for analysis;

Obtain the test result obtained by the server analyzing the test data.
The method according to claim 33, wherein after said obtaining the test data of the unmanned aerial vehicle stored in the storage device of the unmanned aerial vehicle, the method further comprises:

The score of the unmanned aerial vehicle obtained based on the test result is displayed through the interactive interface.
The method according to claim 35, wherein the score includes the score of the entire aircraft of the UAV and/or the score of different functional modules of the UAV;

Wherein, the whole machine includes all the functional modules of the UAV, and the functional modules can perform corresponding actions.
The method according to claim 36, wherein the score of the whole machine is obtained by weighting based on the score of each functional module; and/or

The score of the functional module is determined based on a first score and a second score, wherein the first score is determined based on the result of the functional module executing the corresponding action, and the second score is determined based on The performance data when the function module executes the corresponding action is determined, and the result is used to indicate the success or failure of the function module in executing the corresponding action.
The method according to claim 36, wherein the functional module comprises a software module and/or a hardware module of the UAV.
The method according to claim 33 or 35, wherein the test data includes first performance data when the UAV performs the first action and the load mounted on the UAV performs the second action The second result is at least one of the second performance data.
The method according to claim 39, wherein the test result includes a first result of the UAV performing the first action, a second result of the load performing the second action, and the At least one of first performance data change information over time and the second performance data change information over time.
The method according to claim 33 or 35, wherein the test data includes test data of the same UAV or UAV of the same model in different time periods; or

The test data includes test data of different types of unmanned aerial vehicles at the same time period; or

The test data includes test data when the same unmanned aerial vehicle or the same type of unmanned aerial vehicle uses different versions of firmware or hardware.
The method according to claim 33, further comprising:

Store the test result in the historical test database.
The method according to claim 42, wherein the historical test database is used to combine the identity information of the unmanned aerial vehicle, the test-related information when the unmanned aerial vehicle is being tested, and the testing of the unmanned aerial vehicle. The results are saved in one-to-one correspondence;

Wherein, the test-related information includes at least one of test time, test location, and firmware version information.
The method according to claim 43, further comprising:

Acquiring the historical data query instruction input by the user through the interactive interface, wherein the historical data query instruction is used to indicate the identity information and/or test related information of the unmanned aerial vehicle to be queried;

Obtaining corresponding test results from the historical test database according to the identity information and/or the test-related information;

The currently acquired test result is displayed through the interactive interface.
The method according to claim 44, further comprising:

Displaying the associated identification of each test result in the currently obtained test results on the interactive interface;

When the user operates the associated identifier, the corresponding test result is processed based on the indication content of the associated identifier.
The method according to claim 31, wherein after importing the configuration file to the UAV so that the UAV performs a test based on the configuration file, the method further comprises:

Import a new configuration file into the unmanned aerial vehicle, so that the unmanned aerial vehicle replaces the configuration file with the new configuration file, and performs a test based on the new configuration file.
A test configuration device for an unmanned aerial vehicle, characterized in that the device comprises:

Storage device for storing program instructions; and

One or more processors call program instructions stored in the storage device, and when the program instructions are executed, the one or more processors are individually or collectively configured to implement the following operations:

Receiving a configuration instruction input by a user through an interactive interface, the configuration instruction being used to instruct the unmanned aerial vehicle to perform an action during the test and the parameters related to the action;

According to the configuration instruction, a configuration file indicating the testing process of the unmanned aerial vehicle is generated.
The device according to claim 47, wherein the configuration file is a preset template file, and the content of the preset fields in the template file can be modified.
The device according to claim 48, wherein the preset field comprises a field corresponding to the action and a field corresponding to the parameter related to the action.
The device according to claim 47, wherein the action comprises a first action performed by the UAV itself and/or a second action performed by a load carried on the UAV.
The apparatus of claim 50, wherein the first action includes a flight action of the UAV.
The device according to claim 51, wherein the parameters related to the flight maneuver include at least one of flight direction, flight speed, flight distance, flight duration, number of flights, and flightable space range.
The apparatus of claim 50, wherein the first action includes a first attitude change of the UAV.
The device according to claim 53, wherein the parameter related to the first posture change includes at least one of a magnitude of the posture change and a direction of the posture change.
The device according to claim 50, wherein the load comprises a photographing device, and the second action comprises a photographing action of the photographing device.
The device according to claim 55, wherein the shooting action comprises taking a photo or video.
The device according to claim 56, wherein the parameters related to photographing include resolution, frame rate, number of frames, delay time, image mode, saturation, exposure compensation, white balance, storage format, image ratio , At least one of the camera modes; or

The video-related parameters include at least one of resolution, frame rate, video duration, delay time, image mode, saturation, exposure compensation, white balance, and image ratio.
The device according to claim 55, wherein the load further comprises a pan/tilt used to mount the photographing device on the UAV, and the second action further comprises a pan/tilt performed by the pan/tilt. The third action.
The device according to claim 58, wherein the third action includes at least one of a second posture change of the pan/tilt and a function setting of the pan/tilt.
The device according to claim 59, wherein the parameter related to the second posture change includes at least one of a magnitude of the posture change and a direction of the posture change.
The device of claim 47, wherein the parameter includes the number of times the action is performed.
The device according to claim 47, wherein the settable range of the size of the parameter is preset.
The device according to claim 47, wherein the actions include multiple, and the configuration instruction is further used to instruct the UAV to perform multiple sequences of the actions.
The device according to claim 47, wherein the one or more processors are separately or collectively configured to perform the following operations before receiving the configuration instruction input by the user through the interactive interface:

Displaying a first identifier of an action executable by the UAV during testing and a second identifier of the parameter related to the action on the interactive interface;

When the one or more processors receive the configuration instruction input by the user through the interactive interface, they are individually or collectively further configured to implement the following operations:

Acquiring the user's operations on the first identifier and the second identifier;

According to the operations on the first identifier and the second identifier, the configuration instruction input by the user is determined.
The device according to claim 54, wherein the one or more processors display on the interactive interface a first identifier of an action that can be performed by the UAV during a test and the action-related Before the second identification of the parameters, individually or collectively, they are also configured to implement the following operations:

Displaying an action addition mark on the interactive interface;

When the one or more processors display on the interactive interface the first identifiers of the actions executable by the UAV during the test and the second identifiers of the parameters related to the actions, they are individually or jointly It is further configured to implement the following operations:

When the user operates the action to add an identifier, the first identifier of the action executable by the UAV during the test and the second identifier of the parameter related to the action are displayed on the interactive interface.
The device according to claim 54, wherein the one or more processors are separately or collectively configured to use To implement the following operations:

It is detected that the first identifier corresponding to the action is selected.
The device according to claim 54, wherein the one or more processors, individually or collectively, are further configured to perform the following operations:

The first identifier of the selected action and the sequence in which the selected action is executed when the UAV is performing a test are displayed on the interactive interface.
The device according to claim 67, wherein the one or more processors, individually or collectively, are further configured to perform the following operations:

Displaying the edit identifier associated with the selected action on the interactive interface;

When the user operates the edit flag, enter the action setting page;

According to the user's operation on the action setting page, the action currently associated with the edit ID is replaced with a reselected action, or the parameters related to the action currently associated with the edit ID are modified.
The device according to claim 67, wherein the one or more processors, individually or collectively, are further configured to perform the following operations:

Displaying the deletion identifier associated with the selected action on the interactive interface;

When the user operates the deletion indicator, the action associated with the deletion indicator is deleted.
The device according to claim 67, wherein the one or more processors, individually or collectively, are further configured to perform the following operations:

The update time of the selected action is displayed on the interactive interface.
The device according to claim 67, wherein the order is related to the order in which the first identifier is selected.
The device according to claim 47, wherein when the one or more processors generate a configuration file indicating the test process of the UAV according to the configuration instruction, they are further individually or collectively further Configured to perform the following operations:

When the file generation instruction input by the user through the interactive interface is obtained, a configuration file indicating the testing process of the unmanned aerial vehicle is generated according to the configuration instruction.
The device according to claim 47, wherein the one or more processors generate a configuration file indicating the testing process of the unmanned aerial vehicle according to the configuration instruction, and then separately or collectively restore the configuration file. Configured to perform the following operations:

Export and save the configuration file.
The device according to claim 73, wherein the one or more processors export and save the configuration file, and are separately or collectively further configured to perform the following operations:

Export the configuration file when the file export instruction input by the user through the interactive interface is obtained, where the file export instruction is used to indicate the location information of the location where the configuration file is to be saved;

Save the configuration file according to the location information.
The device according to claim 47, wherein the one or more processors are separately or collectively configured to perform the following operations before receiving the configuration instruction input by the user through the interactive interface:

Acquiring a file import instruction input by the user through the interactive interface, where the file import instruction is used to indicate the file information of the historical configuration file to be imported;

Import the historical configuration file according to the file import instruction;

Displaying the test process of the unmanned aerial vehicle corresponding to the historical configuration file on the interactive interface;

Wherein, the configuration instruction is generated based on the test process of the unmanned aerial vehicle corresponding to the historical configuration file.
The device according to claim 75, wherein the configuration instruction includes at least one of a modification instruction, a new addition instruction, and a deletion instruction;

Wherein, the modification instruction is used to instruct to replace the actions included in the test process of the UAV corresponding to the historical configuration file with new actions, and/or to change the unmanned aerial vehicle corresponding to the historical configuration file. The size of the related parameters of the actions included in the test process of the aircraft is set to a new value;

The newly added instruction is used to instruct to add a new action in the test process of the UAV corresponding to the historical configuration file, and/or the test process of the UAV corresponding to the historical configuration file includes Add new relevant parameters for the action;

The deletion instruction is used to instruct to delete the actions included in the test process of the UAV corresponding to the historical configuration file, and/or delete the actions included in the test process of the UAV corresponding to the historical configuration file Related parameters.
The apparatus according to claim 47, wherein the one or more processors, after generating a configuration file indicating the test process of the UAV according to the configuration instruction, are individually or collectively returned Configured to perform the following operations:

Import the configuration file into the unmanned aerial vehicle, so that the unmanned aerial vehicle performs a test based on the configuration file.
The device according to claim 77, wherein when the one or more processors import the configuration file into the UAV, individually or collectively, they are further configured to perform the following operations:

When a test trigger instruction input by the user through the interactive interface is received, the configuration file is imported into the unmanned aerial vehicle.
The apparatus according to claim 77, wherein the one or more processors are separately or collectively configured to perform the following operations after importing the configuration file into the UAV:

Acquiring the test data of the unmanned aerial vehicle stored in the storage device of the unmanned aerial vehicle;

The interactive interface displays the test results obtained based on the test data analysis.
The device according to claim 79, wherein the one or more processors, after obtaining the test data of the unmanned aerial vehicle stored in the storage device of the unmanned aerial vehicle, display an analysis based on the test data Before the obtained test results, individually or collectively, they are also configured to implement the following operations:

Upload the test data to the server for analysis;

Obtain the test result obtained by the server analyzing the test data.
The device according to claim 79, wherein the one or more processors, after obtaining the test data of the unmanned aerial vehicle stored in the storage device of the unmanned aerial vehicle, are individually or collectively returned Configured to perform the following operations:

The score of the unmanned aerial vehicle obtained based on the test result is displayed through the interactive interface.
The device according to claim 81, wherein the score comprises a score of the entire UAV and/or a score of different functional modules of the UAV;

Wherein, the whole machine includes all the functional modules of the UAV, and the functional modules can perform corresponding actions.
The device according to claim 82, wherein the score of the whole machine is obtained by weighting based on the scores of each functional module; and/or

The score of the functional module is determined based on a first score and a second score, wherein the first score is determined based on the result of the functional module executing the corresponding action, and the second score is determined based on The performance data when the function module executes the corresponding action is determined, and the result is used to indicate the success or failure of the function module in executing the corresponding action.
The device according to claim 82, wherein the functional module comprises a software module and/or a hardware module of the UAV.
The device according to claim 79 or 81, wherein the test data includes first performance data when the UAV performs the first action and the load mounted on the UAV performs the second action The second result is at least one of the second performance data.
The device of claim 85, wherein the test result includes a first result of the UAV performing the first action, a second result of the load performing the second action, and the At least one of first performance data change information over time and the second performance data change information over time.
The device according to claim 79 or 81, wherein the test data includes test data of the same UAV or UAV of the same model in different time periods; or

The test data includes test data of different types of unmanned aerial vehicles at the same time period; or

The test data includes test data when the same unmanned aerial vehicle or the same type of unmanned aerial vehicle uses different versions of firmware or hardware.
The device according to claim 79, wherein the one or more processors, individually or collectively, are further configured to perform the following operations:

Store the test result in the historical test database.
The device according to claim 88, wherein the historical test database is used to combine the identity information of the unmanned aerial vehicle, the test related information when the unmanned aerial vehicle is being tested, and the testing of the unmanned aerial vehicle. The results are saved in one-to-one correspondence;

Wherein, the test-related information includes at least one of test time, test location, and firmware version information.
The device according to claim 89, wherein the one or more processors, individually or collectively, are further configured to perform the following operations:

Acquiring the historical data query instruction input by the user through the interactive interface, wherein the historical data query instruction is used to indicate the identity information and/or test related information of the unmanned aerial vehicle to be queried;

Obtaining corresponding test results from the historical test database according to the identity information and/or the test-related information;

The currently acquired test result is displayed through the interactive interface.
The device according to claim 90, wherein the one or more processors, individually or collectively, are further configured to perform the following operations:

Displaying the associated identification of each test result in the currently obtained test results on the interactive interface;

When the user operates the associated identifier, the corresponding test result is processed based on the indication content of the associated identifier.
The apparatus according to claim 77, wherein the one or more processors import the configuration file to the unmanned aerial vehicle, so that the unmanned aerial vehicle performs a test based on the configuration file, Separately or collectively, it is also configured to perform the following operations:

Import a new configuration file into the unmanned aerial vehicle, so that the unmanned aerial vehicle replaces the configuration file with the new configuration file, and performs a test based on the new configuration file.
A terminal device, characterized in that the terminal device can be communicably connected with an unmanned aerial vehicle, and the terminal device includes:

case;

A display module, arranged in the housing, the display module including an interactive interface; and

The test configuration device for an unmanned aerial vehicle according to any one of claims 47 to 92, which is supported by the casing and electrically connected to the display module.