Pre-flight inspection method, device, apparatus and storage medium

Abstract

Embodiments of the present application provide a pre-flight inspection method, device, equipment and storage medium, wherein the method comprises: when a flight body is in a pre-flight inspection stage of a control mechanism, controlling a display device associated with the flight body to display an inspection guide interface of the control mechanism; the inspection guide interface displays a control guide animation of the control mechanism and corresponding prompt information; when response data fed back by the control mechanism being inspected is received, determining whether a current inspection operation of the control mechanism is consistent with an inspection operation prompted by a current inspection guide interface according to the response data; when the current inspection operation of the control mechanism is consistent with the inspection operation prompted by the current inspection guide interface, and the current inspection guide interface is not the last inspection guide interface in the pre-flight inspection stage, controlling the display device to display a next inspection guide interface of the control mechanism.

Description

TECHNICAL FIELD

[0001] The present application relates to the technical field of flight bodies, in particular to a pre-flight inspection method, device, equipment and storage medium. BACKGROUND

[0002] Before a manned flight body takes off, in order to ensure flight safety, the manned flight body usually needs to be pre-flight inspected, and the pre-flight inspection includes flight body external inspection, flight body endurance state inspection, flight body internal hardware inspection, flight body logbook inspection and other links. These pre-flight inspection links are completed by crew personnel according to standard operation files such as operation manuals, maintenance manuals and flight inspection sheets. The operation manuals, maintenance manuals and flight inspection sheets generally need to be understood by personnel with relevant experience or relevant professional knowledge, and non-professionals are difficult to complete pre-flight inspection according to these manuals. It can be seen that the pre-flight inspection threshold is high. In addition, this step-by-step manual checking and understanding operation mode not only brings a certain inspection burden to the inspector, but also leads to low pre-flight inspection efficiency. SUMMARY

[0003] Therefore, the purpose of the present application is to provide a pre-flight inspection method, device, equipment and storage medium to reduce the pre-flight inspection threshold and improve the pre-flight inspection efficiency.

[0004] In order to achieve the above purpose, the technical scheme adopted by the embodiments of the present application is as follows:

[0005] The first aspect of the embodiments of the present application provides a pre-flight inspection method, comprising:

[0006] When the flight body is in the pre-flight inspection stage of the control mechanism, a display device associated with the flight body is controlled to display an inspection guide interface of the control mechanism; the inspection guide interface displays a control guide animation of the control mechanism and corresponding prompt information;

[0007] When receiving response data fed back by the control mechanism being inspected, it is determined whether the current inspection operation of the control mechanism is consistent with the inspection operation prompted by the current inspection guide interface according to the response data;

[0008] When the current inspection operation of the control mechanism is consistent with the inspection operation prompted by the current inspection guide interface, and the current inspection guide interface is not the last inspection guide interface in the pre-flight inspection stage, the display device is controlled to display the next inspection guide interface of the control mechanism;

[0009] The method further comprises, when the response data fed back by the handling mechanism under inspection is received, determining, according to the response data, whether the current inspection operation of the handling mechanism is consistent with the inspection operation prompted by the current inspection guidance interface until the current inspection guidance interface is the last inspection guidance interface.

[0010] In an optional embodiment, when the response data fed back by the handling mechanism under inspection is received, the method further comprises:

[0011] Controlling the model of the handling mechanism in the current inspection guidance interface to display the state corresponding to the current response data in real time.

[0012] In an optional embodiment, when the current inspection operation of the handling mechanism is consistent with the inspection operation prompted by the current inspection guidance interface, the method further comprises:

[0013] Controlling the current inspection guidance interface to display an inspection success prompt;

[0014] And / or, when the current inspection operation of the handling mechanism is inconsistent with the inspection operation prompted by the current inspection guidance interface, the method further comprises:

[0015] Controlling the current inspection guidance interface to display an inspection error prompt.

[0016] In an optional embodiment, the current inspection guidance interface further displays a plurality of inspection progress bars, and different inspection progress bars correspond to different inspection operations.

[0017] In an optional embodiment, when the current inspection operation of the handling mechanism is consistent with the inspection operation prompted by the current inspection guidance interface, the method further comprises:

[0018] Updating the progress bar corresponding to the inspection operation prompted by the current inspection guidance interface from an uncompleted state to a completed state among the plurality of inspection progress bars.

[0019] In an optional embodiment, the handling mechanism comprises a joystick, a throttle and an auxiliary key assembly, and the auxiliary key assembly comprises a plurality of keys.

[0020] The inspection guidance interfaces are provided in plurality, including an inspection guidance interface for guiding the forward pushing and clockwise rotation of the joystick for one round, an inspection guidance interface for guiding the left and right twisting of the joystick, an inspection guidance interface for guiding the upward and downward pushing of the throttle, and an inspection guidance interface for guiding the sequential operation of the plurality of keys in the auxiliary key assembly.

[0021] In an optional embodiment, before the flight body enters the pre-flight inspection stage of the handling mechanism, the method further comprises:

[0022] Upon receiving a take-off instruction, the display device is controlled to display a manual inspection sheet guidance interface; the manual inspection sheet guidance interface displays a plurality of inspection items and respective corresponding guidance controls, and a model display area; different inspection items are used to indicate different parts of the flight body that need to be inspected;

[0023] Upon receiving an instruction generated by the triggering of a guidance control, the target flight body part indicated by the inspection item corresponding to the triggered guidance control is acquired, and the model display area is controlled to display the target flight body part and corresponding prompt information.

[0024] In an optional implementation, after the inspection of the pre-flight inspection phase of the flight body in the handling mechanism is completed, the method further comprises:

[0025] The display device is controlled to display a dynamic inspection guidance interface; the dynamic inspection guidance interface displays a start control for starting dynamic inspection, and a model display area;

[0026] Upon receiving an instruction generated by the triggering of the start control, the rotors of the flight body are controlled to rotate, and the rotation data of the rotors is acquired in real time, and the flight body model displayed in the model display area is controlled to perform corresponding actions according to the rotation data.

[0027] In an optional implementation, before the rotors of the flight body are controlled to rotate, the method further comprises:

[0028] The display device is controlled to display a three-dimensional map interface of the environment in which the flight body is located, and the three-dimensional map interface displays a safety confirmation control;

[0029] Correspondingly, the step of controlling the rotors of the flight body to rotate and acquiring the rotation data of the rotors in real time is performed upon receiving an instruction generated by the triggering of the start control and an instruction generated by the triggering of the safety confirmation control.

[0030] In a second aspect of the embodiments of the application, a pre-flight inspection device is provided, comprising:

[0031] The guidance module is configured to, when the flight body is in a pre-flight inspection phase of a handling mechanism, control a display device associated with the flight body to display an inspection guidance interface of the handling mechanism; the inspection guidance interface displays a handling guidance animation of the handling mechanism and corresponding prompt information;

[0032] The determination module is configured to, upon receiving response data fed back by the handling mechanism being inspected, determine whether the current inspection operation of the handling mechanism is consistent with the inspection operation prompted by the current inspection guidance interface according to the response data.

[0033] The switching module is configured to: when the current inspection operation of the control mechanism is consistent with the inspection operation prompted by the current inspection guidance interface, and the current inspection guidance interface is not the last inspection guidance interface in the pre-flight inspection stage, control the display device to display the next inspection guidance interface of the control mechanism.

[0034] The cycling module is configured to: return to execute the step of determining whether the current inspection operation of the control mechanism is consistent with the inspection operation prompted by the current inspection guidance interface according to the response data fed back by the control mechanism being inspected until the current inspection guidance interface is the last inspection guidance interface.

[0035] In a third aspect, an electronic device is provided, including a processor and a memory, the memory storing machine executable instructions capable of being executed by the processor, and the processor is capable of executing the machine executable instructions to implement the pre-flight inspection method provided in the first aspect.

[0036] In a fourth aspect, a computer readable storage medium is provided, and the computer readable storage medium stores a computer program, and the computer program is executed by a processor to implement the pre-flight inspection method provided in the first aspect.

[0037] The pre-flight inspection method, device, equipment and storage medium provided by the embodiments of the present application, on the one hand, by controlling the display interface associated with the flight body to display the control guidance animation and the corresponding prompt information of the control mechanism when the flight body is in the pre-flight inspection stage of the control mechanism, this kind of using animation to combine the prompt information to the user to indicate the pre-flight inspection content of the control mechanism, it is more intuitive and clear, even if it is not the flight body professional and technical ordinary user, also can understand the current required control check and related inspection operation of the control mechanism through the control guidance animation, it can be seen that the threshold of pre-flight inspection is effectively reduced. On the other hand, by automatically determining whether the current inspection operation of the control mechanism is consistent with the inspection operation prompted by the current inspection guidance interface according to the response data fed back by the control mechanism being inspected by the user when the response data is received, as long as the current is not the last inspection process of the control mechanism, the next inspection guidance interface will be automatically switched to guide the user to perform the next step of inspection on the control mechanism. This kind of response data generated by the user to the control mechanism is linked with the switching of the inspection process and the inspection guidance interface, without relying on artificial judgment of whether the current inspection process is completed and whether the control mechanism is faulty, and the problem of low pre-flight inspection efficiency caused by the user needing to query the relevant manual for the next step of inspection after completing the current inspection process can be avoided, which is helpful to ensure the smooth progress of the inspection process and improve the pre-flight inspection efficiency.

[0038] In order to make the above objectives, characteristics and advantages of the present application more apparent, more comprehensible, the following preferred embodiments are specifically described in detail below, together with the accompanying drawings. BRIEF DESCRIPTION OF DRAWINGS

[0039] In order to more clearly illustrate the technical solutions of the embodiments of the present application, the following will briefly introduce the drawings needed to be used in the embodiments, and it should be understood that the following drawings only show some of the embodiments of the present application, and therefore should not be regarded as a limitation to the scope, and for those skilled in the art, other related drawings can also be obtained without paying creative labor on the basis of these drawings.

[0040] Figure 1 A structural block diagram of an electronic device provided by the embodiments of the present application is shown;

[0041] Figure 2 A flow chart of a pre-flight inspection method provided by the embodiments of the present application is shown;

[0042] Figure 3 A schematic diagram of an artificial inspection single instruction interface provided by the embodiments of the present application is shown;

[0043] Figure 4 A schematic diagram of another artificial inspection single instruction interface provided by the embodiments of the present application is shown;

[0044] Figure 5 A schematic diagram of an inspection instruction interface for instructing to push the control stick forward and rotate it clockwise for one round provided by the embodiments of the present application is shown;

[0045] Figure 6a A schematic diagram of an inspection instruction interface for instructing to twist the control stick left provided by the embodiments of the present application is shown;

[0046] Figure 6b A schematic diagram of an inspection instruction interface for instructing to twist the control stick right provided by the embodiments of the present application is shown;

[0047] Figure 7a A schematic diagram of an inspection instruction interface for instructing to push the control stick up provided by the embodiments of the present application is shown;

[0048] Figure 7b A schematic diagram of an inspection instruction interface for instructing to push the control stick down provided by the embodiments of the present application is shown;

[0049] Figure 8a A schematic diagram of an inspection instruction interface for instructing to switch the control mode button provided by the embodiments of the present application is shown;

[0050] Figure 8bA schematic diagram of a check guide interface for guiding manipulation of a front flying switch key is shown;

[0051] Figure 8c A schematic diagram of a check guide interface for guiding manipulation of a left turn switch key is shown;

[0052] Figure 8d A schematic diagram of a check guide interface for guiding manipulation of a lift switch pull-up is shown;

[0053] Figure 8e A schematic diagram of a check guide interface for guiding manipulation of a lift switch push-down is shown;

[0054] Figure 8f A schematic diagram of a check guide interface for guiding manipulation of a mode key back switch is shown;

[0055] Figure 9 A schematic diagram of a check guide interface for prompting a joystick front push and a clockwise rotation for one round is shown;

[0056] Figure 10 A schematic diagram of a check guide interface for prompting a joystick left twist and a right twist is shown;

[0057] Figure 11 A schematic diagram of a check guide interface for prompting a throttle check is shown;

[0058] Figure 12a A schematic diagram of a check guide interface for prompting a mode key switch check is shown;

[0059] Figure 12b A schematic diagram of a state for indicating that a front flying switch is pressed in a check is shown;

[0060] Figure 12c A schematic diagram of a check guide interface for indicating that a front flying switch and a back flying switch pass a check is shown;

[0061] Figure 12d A schematic diagram of a check guide interface for indicating that a left turn switch and a right turn switch pass a check is shown;

[0062] Figure 12e A schematic diagram of a check guide interface for indicating that a lift switch passes a check is shown;

[0063] Figure 12f Fig. 1 shows a schematic diagram of an inspection guidance interface for indicating that the mode key return check is qualified according to an embodiment of the present application;

[0064] Figure 13 Fig. 2 shows a schematic diagram of a flight log form according to an embodiment of the present application;

[0065] Figure 14 Fig. 3 shows a schematic diagram of a dynamic inspection guidance interface according to an embodiment of the present application;

[0066] Figure 15 Fig. 4 shows a functional module diagram of a pre-flight inspection device according to an embodiment of the present application. DETAILED DESCRIPTION

[0067] The technical solutions in the embodiments of the present application will be clearly and completely described below with reference to the accompanying drawings of the embodiments of the present application. Obviously, the described embodiments are only some of the embodiments of the present application, but not all the embodiments of the present application. The components of the embodiments of the present application described and shown in the accompanying drawings can be arranged and designed in various different configurations.

[0068] Therefore, the detailed description of the embodiments of the present application provided in the accompanying drawings below is not intended to limit the scope of the claimed present application, but only represents selected embodiments of the present application. Based on the embodiments of the present application, all other embodiments obtained by those skilled in the art without creative work are within the scope of protection of the present application.

[0069] It should be noted that the relational terms such as "first" and "second" and the like are used only to distinguish one entity or operation from another entity or operation, and do not necessarily require or imply that these entities or operations have any such actual relationship or order. Moreover, the terms "comprising", "including" or any other variant thereof are intended to cover non-exclusive inclusion, so that a process, method, article or apparatus including a series of elements includes not only those elements, but also other elements not explicitly listed, or other elements inherent in such a process, method, article or apparatus. Without more limitations, the element defined by the statement "comprising a" does not exclude the presence of additional identical elements in the process, method, article or apparatus including the element.

[0070] To solve the technical problems of high threshold and low efficiency of pre-flight inspection in the prior art, which is caused by the need to rely on professional personnel to complete the pre-flight inspection of the flight body according to the standard operation files such as operation manual, maintenance manual and flight check sheet, the present application provides a pre-flight inspection method, on the one hand, by controlling the display interface associated with the flight body to display the steering mechanism steering guide animation and the corresponding prompt information when the flight body is in the pre-flight inspection stage of the steering mechanism, this kind of using animation combined with prompt information to guide the user to the pre-flight inspection content of the steering mechanism is more intuitive and clear, even if the ordinary user who is not a professional technical user of the flight body, can also quickly understand the current required steering inspection of the steering mechanism and the related inspection operation through the steering guide animation, so the threshold of pre-flight inspection is effectively reduced. On the other hand, by receiving the response data fed back by the user when the steering mechanism is inspected, the current inspection operation of the steering mechanism is automatically determined according to the response data whether it is consistent with the inspection operation prompted by the current inspection guide interface, when the determination result is consistent, as long as the current is not the last inspection process of the steering mechanism, it will automatically jump to the next inspection guide interface to guide the user to perform the next step inspection on the steering mechanism. This kind of linkage between the response data generated by the user's steering inspection of the steering mechanism and the switching of the inspection process and the inspection guide interface, without relying on manual judgment of whether the current inspection process is completed and whether the steering mechanism is faulty, can avoid the problem of low efficiency of pre-flight inspection caused by the need for the user to query the relevant manual for the next step inspection after completing the current inspection process, and is beneficial to ensure the smooth progress of the inspection process and improve the efficiency of pre-flight inspection.

[0071] The pre-flight inspection method provided by the present application can be applied to an electronic device, please refer to Figure 1 is a structural block diagram of an electronic device. The electronic device 100 includes a memory 110, a processor 120 and a communication module 130. The memory 110, the processor 120 and the communication module 130 are directly or indirectly electrically connected to each other to realize the transmission or interaction of data. For example, these elements can be electrically connected to each other through one or more communication buses or signal lines.

[0072] The memory is used to store programs or data. The memory may be, but is not limited to, Random Access Memory (RAM), Read Only Memory (ROM), Programmable Read-Only Memory (PROM), Erasable Programmable Read-Only Memory (EPROM), Electrically Erasable Programmable Read-Only Memory (EEPROM), etc.

[0073] The processor is used to read / write data or programs stored in memory and to perform the corresponding functions.

[0074] The communication module is used to establish communication connections between electronic devices and other communication terminals via a network, and to send and receive data via the network.

[0075] It should be understood that, Figure 1 The structure shown is only a schematic diagram of an electronic device; the electronic device may also include components that are larger than... Figure 1 The more or fewer components shown, or having the same Figure 1 The different configurations shown. Figure 1 The components shown can be implemented using hardware, software, or a combination thereof.

[0076] In some embodiments, the electronic device may be installed in a manned aircraft to control the flight of the manned aircraft and the display status of the cockpit display device in the manned aircraft, but its function is not limited thereto.

[0077] The following combination Figure 3 The pre-flight inspection method provided in the embodiments of the present invention will be described below. Figure 3 This is a flowchart of a pre-flight inspection method provided by an embodiment of the present invention, the pre-flight inspection method comprising:

[0078] In step S300, when the aircraft is in the pre-flight inspection phase of the control mechanism, the display device associated with the aircraft is controlled to display the inspection guidance interface of the control mechanism; the inspection guidance interface displays the control mechanism's operation guidance animation and corresponding prompts.

[0079] In step S400, when the response data fed back by the inspection of the control mechanism is received, it is determined whether the current inspection operation of the control mechanism is consistent with the inspection operation prompted by the current inspection guidance interface based on the response data.

[0080] In step S500, when the current inspection operation of the control mechanism is consistent with the inspection operation prompted by the current inspection guidance interface, and the current inspection guidance interface is not the last inspection guidance interface in the pre-flight inspection stage, the display device is controlled to display the next inspection guidance interface of the control mechanism;

[0081] In step S600, returning to the step of executing the received response data fed back by the control mechanism under inspection, it is determined whether the current inspection operation of the control mechanism is consistent with the inspection operation prompted by the current inspection guidance interface according to the response data until the current inspection guidance interface is the last inspection guidance interface.

[0082] Before the flight body takes off, in order to ensure the safe flight of the flight body, the flight body usually needs to be pre-flight checked. In order to at least simplify the complexity of the pre-flight inspection of the control mechanism, reduce the pre-flight inspection threshold of the control mechanism, and improve the pre-flight inspection efficiency of the control mechanism, the pre-flight inspection method provided by the embodiment of the application can be configured in the control system of the flight body in advance, so that the control system does not control the flight body to take off when receiving the instruction of the flight body taking off, but triggers the flight body to enter the pre-flight inspection process, and guides the user to perform the pre-flight inspection of the flight body through the pre-flight inspection method provided by the embodiment of the application. Based on this, the display device in the above step S300 can be a display device configured in the cockpit of the flight body.

[0083] In some embodiments, in order to be able to cover more inspection contents of the pre-flight inspection of the flight body, to provide more pre-flight inspection guidance of the inspection link for the user, to further reduce the pre-flight inspection threshold and to improve the overall efficiency of the pre-flight inspection, the pre-flight inspection method provided by the embodiment of the application further provides an inspection guidance scheme of a manual inspection work order in another inspection link before the pre-flight inspection stage of the control mechanism, that is, before the flight body enters the pre-flight inspection stage of the control mechanism, the pre-flight inspection method provided by the embodiment of the application can further include:

[0084] In step S100, when the take-off instruction is received, the display device is controlled to display a manual inspection order guidance interface; the manual inspection order guidance interface displays: a plurality of inspection items and their respective guidance controls, and a model display area; different inspection items are used to indicate different parts of the flight body that need to be inspected;

[0085] In step S200, when the instruction generated by the triggering of the guidance control is received, the target flight body part indicated by the inspection item corresponding to the currently triggered guidance control is acquired, and the model display area is controlled to display the target flight body part and the corresponding prompt information.

[0086] Please refer to Figure 3 and Figure 4, Figure 3 is a schematic diagram of an artificial inspection sheet guiding interface provided by an embodiment of the present application, Figure 4 is a schematic diagram of another artificial inspection sheet guiding interface provided by an embodiment of the present application, and the following Figure 3 and Figure 4 explain the pre-flight inspection guiding principle of the above steps S100-S200:

[0087] When the user controls the flight body to take off through the user interface on the flight body display device, or the user interface of the associated terminal device, or the remote controller or joystick, the take-off instruction recorded in step S100 is generated, and at this time, the execution subject of the pre-flight inspection provided by the embodiment of the present application, for example, the control system of the flight body, will receive the take-off instruction and execute step S100 to control the display device to display the artificial inspection sheet guiding interface, as shown in Figure 3 At this time, the artificial inspection sheet guiding interface displays a plurality of inspection items "arm", "rotor", "landing gear", "electric drive", "duct", "cabin", and "beeper inspection", Figure 3 The right side of each inspection item in Figure 3 is respectively configured with a guiding control, for example, the right side of "arm" is configured with a control similar to a play button figure, and for another example, the right side of "beeper inspection" is configured with a control surrounded by a rectangular frame, which is a volume figure control. These controls are all guiding controls. In addition, at this time, the artificial inspection sheet guiding interface also displays a model display area, as shown in Figure 3 At this time, the model display area displays the whole machine model of the flight body, which can indicate that the user has not started the pre-flight inspection according to the artificial inspection sheet, so the whole machine model of the flight body is displayed in the model display area.

[0088] After the artificial inspection sheet guiding interface is displayed through step S100, the user can gradually complete the inspection of the corresponding components in the flight body according to the inspection items guided by the artificial inspection sheet. During the inspection process, if the user is not clear about which part of the flight body a certain component refers to, the user can click the guiding control corresponding to the corresponding inspection item in the artificial inspection sheet guiding interface, for example, click the guiding control corresponding to "duct", at this time, the control system can receive the instruction generated by the triggering of the guiding control, and execute step S200 to obtain the target flight body part indicated by the inspection item corresponding to the currently triggered guiding control, for example, as shown in Figure 4 The "duct" part of the flight body is obtained, and the model display area is controlled to display the "duct" part and the prompt information "check the duct" and "duct connector connection fastener is complete". In this way, the user can check the corresponding part of the flight body according to the machine part displayed in the model display area, and the inspection content can also be obtained from the prompt information displayed in the model display area.

[0089] Therefore, through the manual inspection sheet guiding scheme in steps S100-S200, the ordinary user can quickly implement the pre-flight inspection of the manual inspection sheet stage of the flight body according to the guidance, which is conducive to reducing the threshold for the ordinary user to inspect the external structure of the flight body and is conducive to further improving the overall efficiency and user experience of the pre-flight inspection.

[0090] After the user completes the pre-flight inspection of the manual inspection sheet stage and confirms that the corresponding flight body components meet the pre-flight inspection requirements, as one of the examples, the "completion confirmation" control configured in the manual inspection sheet guiding interface can be used to trigger the control system to guide the next pre-flight inspection stage, at which time the pre-flight inspection stage of the control mechanism is entered. The triggering operation of the control system to guide the next pre-flight inspection stage can not depend on the "completion confirmation" control configured in the manual inspection sheet guiding interface, and in other examples, the corresponding instruction can also be input in the form of voice input or other bound terminal device, which is not limited in the embodiments of the present application.

[0091] When the flight body is in the pre-flight inspection stage of the control mechanism, the control system will execute step S300 to control the display device to display the inspection guiding interface of the control mechanism, and display the control guiding animation and the corresponding prompt information of the control mechanism in the inspection guiding interface. As one of the examples, the control mechanism of the flight body includes a control stick, a throttle, and an auxiliary key assembly. The auxiliary key assembly is used as a backup control mechanism of the control stick and can include the following keys for controlling the flight of the flight body: mode key, forward flight switch, backward flight switch, left turn switch, right turn switch, and lift switch. Based on this, in some embodiments, to achieve orderly inspection of the control mechanism and avoid confusion in the inspection operation caused by too much information being prompted at one time, the embodiments of the present application split the complex steps involved in the inspection into single simple steps and configure corresponding inspection guiding interfaces for this purpose, so that the whole pre-flight inspection process of the control mechanism is simple and clear, thereby further improving the pre-flight inspection efficiency. That is, the inspection guiding interface can be provided with multiple inspection guiding interfaces, including an inspection guiding interface for guiding the control of the control stick to be pushed forward and rotated clockwise for one turn, an inspection guiding interface for guiding the control of the control stick to be twisted left and right, an inspection guiding interface for guiding the control of the throttle to be pushed up and down, and an inspection guiding interface for guiding the control of the multiple keys in the auxiliary key assembly in sequence. Wherein, the related guiding interface of the control stick can refer to Figure 6a and Figure 6b , Figure 6a is a schematic view of an inspection guiding interface for guiding the control of the control stick to be twisted left, provided by the embodiments of the present application, Figure 6b is a schematic view of an inspection guiding interface for guiding the control of the control stick to be twisted right, provided by the embodiments of the present application. Similarly, the related guiding interface of the throttle can refer to Figure 7a and Figure 7b, Figure 7a is a schematic diagram of a check guide interface for guiding the manipulation of pushing up the throttle, Figure 7b is a schematic diagram of a check guide interface for guiding the manipulation of pushing down the throttle. Similarly, in the check guide interface for guiding the sequential manipulation of multiple keys in the auxiliary key assembly, there is a corresponding prompt interface for each key. Please refer to Figures 8a to 8f , Figure 8a is a schematic diagram of a check guide interface for guiding the manipulation of mode key switching, Figure 8b is a schematic diagram of a check guide interface for guiding the manipulation of the forward flight switch key, Figure 8c is a schematic diagram of a check guide interface for guiding the manipulation of the left turn switch key, Figure 8d is a schematic diagram of a check guide interface for guiding the manipulation of pulling up the lift switch, Figure 8e is a schematic diagram of a check guide interface for guiding the manipulation of pushing down the lift switch, Figure 8f is a schematic diagram of a check guide interface for guiding the manipulation of mode key switching back.

[0092] It can be seen that, regardless of which check guide interface diagram, the corresponding virtual model of the currently checked component in the manipulation mechanism is used to construct the corresponding animation and prompt information of the virtual model according to the required check content, and is displayed, so that the user can clearly understand the check operation of the corresponding part according to the animation, and the content of the animation display can also be more clearly understood in combination with the prompt information, so that non-flight body professional technical ordinary users can also quickly understand the required manipulation check of the manipulation mechanism and the related check operation through the manipulation guide animation, effectively reducing the threshold of pre-flight check.

[0093] After the user performs the corresponding operation on the manipulation mechanism according to the manipulation guide animation and the corresponding prompt of the current check guide interface displayed by the display device, for example, assuming that the current check guide interface is the guide interface shown in Figure 5 , indicating that the user manipulates the joystick to push forward and rotate clockwise for one turn according to the animation and text prompt, after the user manipulates the joystick according to the prompt, if the joystick and related sensors are normal, the control system will receive the response data generated after the joystick is manipulated. The response data can include displacement data and rotation angle data of the joystick, which can be collected by corresponding sensors. For details, please refer to related technologies.

[0094] After receiving the response data, step S400 will be executed to determine whether the current inspection operation of the control mechanism is consistent with the inspection operation prompted by the current inspection guidance interface, based on the inherited... Figure 5 For example, if the inspection guidance interface prompts that the inspection operation is to push the joystick forward and rotate it clockwise one full turn, then the displacement threshold corresponding to pushing the joystick forward to its final position and the angle threshold corresponding to rotating the joystick clockwise one full turn can be pre-configured according to the required inspection data standards. Therefore, during the execution of step S400, the displacement and angle in the response data at the end of the operation can be checked. If both are satisfied, it indicates that the current inspection operation of the control mechanism is consistent with the inspection operation prompted by the current inspection guidance interface. If either is not satisfied, it indicates that the current inspection operation of the control mechanism is inconsistent with the inspection operation prompted by the current inspection guidance interface. This result may be due to improper user operation or a malfunction of the control mechanism. In either case, to facilitate timely understanding of the inspection results by the user, in some embodiments, the pre-flight inspection method provided by this invention also provides a feedback scheme for the inspection results. That is, the pre-flight inspection method provided by this invention may further include:

[0095] In step S410, when the current inspection operation of the operating mechanism is consistent with the inspection operation prompted by the current inspection guidance interface, the current inspection guidance interface is controlled to display an inspection success prompt.

[0096] And / or,

[0097] In step S420, when the current inspection operation of the control mechanism is inconsistent with the inspection operation prompted by the current inspection guidance interface, the current inspection guidance interface is controlled to display an inspection error prompt.

[0098] As can be seen from steps S410 and S420 above, when the current check operation of the control mechanism is consistent with the check operation prompted by the current check guidance interface, the current check guidance interface is controlled to display a check success indicator to indicate that the control mechanism is responding normally and meets the takeoff standards of the corresponding component. The check success indicator can be any form of label. To more intuitively represent success, in some examples, the check success indicator can be set to a pattern related to √. For example, please refer to... Figures 9 to 12a ,as well as Figures 12c to 12f , Figure 9 This is a schematic diagram of an inspection guidance interface provided by an embodiment of the present invention, used to indicate whether the control joystick has passed inspection after being pushed forward and rotated clockwise one full turn. Figure 10 This is a schematic diagram of an inspection guidance interface provided by an embodiment of the present invention, used to indicate whether the control joystick has passed the left and right turning check. Figure 11is a schematic diagram of an inspection guide interface for prompting that the throttle check is qualified, Figure 12a is a schematic diagram of an inspection guide interface for prompting that the mode button switching check is qualified, Figure 12c is a schematic diagram of an inspection guide interface for indicating that the forward flight switch and the backward flight switch checks are qualified, Figure 12d is a schematic diagram of an inspection guide interface for indicating that the left turn switch and the right turn switch checks are qualified, Figure 12e is a schematic diagram of an inspection guide interface for indicating that the lift switch check is qualified, Figure 12f is a schematic diagram of an inspection guide interface for indicating that the mode button back switching check is qualified. As can be seen, for each link of the pre-flight inspection of the control mechanism, when the current inspection operation of the control mechanism is consistent with the inspection operation prompted by the current inspection guide interface, the inspection success prompt symbol is displayed in the corresponding interface, such as Figure 9 the pattern formed by the white hook surrounded by the green square in the prompt information "push forward and rotate clockwise for one round" in Figures 10 to 12a , and Figures 12c to 12f Similarly.

[0099] On the contrary, when the current inspection operation of the control mechanism is inconsistent with the inspection operation prompted by the current inspection guide interface, the control current inspection guide interface displays the inspection error prompt symbol to indicate that the control mechanism is abnormal or the manual operation is incorrect, which does not meet the take-off standard. Similarly, the inspection error prompt symbol can be configured by referring to the examples of the inspection success prompt symbol, as long as it is inconsistent with the inspection success prompt symbol. However, in order to be more intuitive, in some examples, the inspection error prompt symbol can be set as a pattern related to ×.

[0100] In addition to the feedback of the inspection result realized by the schemes in steps S410 and S420, in other variant embodiments, the inspection result can also be output in the form of voice broadcast, so that the user can also know the inspection result in time. In addition, the output of the inspection result can be further enhanced by combining the voice broadcast mode on the basis of the schemes in steps S410 and S420, so as to better attract the attention of the user. Based on this, in other embodiments, the prompt information recorded above can also be played in the form of voice broadcast in addition to the interface display.

[0101] As described above, if the current inspection operation of the control mechanism is consistent with the inspection operation prompted by the current inspection guidance interface, it indicates that the control mechanism is responding normally and meets the takeoff standards of the corresponding component. Therefore, it can be considered that a certain inspection of the corresponding component has been completed. If there are still uninspected items, i.e., the current inspection guidance interface is not the last inspection guidance interface in the pre-flight inspection phase, then step S500 will be executed to control the display device to show the next inspection guidance interface for the control mechanism, for example, completing... Figure 5 After the check shown, you can switch to Figure 6a The inspection guidance interface shown will continue in this manner. If each subsequent inspection passes, it will start from... Figure 6a Gradually switch to Figure 8f This completes the pre-flight checks of all items related to the control mechanism.

[0102] It should be noted that if, during the inspection of a certain item, the control system determines that the current inspection operation of the control mechanism is inconsistent with the inspection operation prompted by the current inspection guidance interface, the user can first operate the control mechanism again according to the guidance of the current inspection guidance interface. If the cumulative number of operations reaches the set threshold, the control mechanism can be considered abnormal. Since the pre-flight inspection of the aircraft is to ensure flight safety, as long as an abnormality is detected, the aircraft can be considered not to meet the takeoff standards. There is no need to continue the inspection of other items, that is, there is no need to switch from the current inspection guidance interface to the next inspection guidance interface. Instead, the current pre-flight inspection can be ended, and an alarm message can be sent to the relevant user terminal to prompt relevant personnel to troubleshoot and maintain the aircraft.

[0103] As can be seen from the above, although a success or error message can be used to inform the user of the inspection status of the control mechanism, the user cannot obtain relevant data during the operation inspection process, nor can they intuitively understand which operations in the operation inspection have problems. Therefore, to solve this technical problem, in some embodiments, the pre-flight inspection method provided by the present invention may further include a scheme to display the status of the control mechanism model in the inspection guidance interface in real time based on response data. That is, the pre-flight inspection method provided by the present invention may further include:

[0104] In step S401, the operating mechanism model in the current inspection guidance interface is controlled in real time and displayed according to the status corresponding to the current response data.

[0105] The following example, using the response data of the forward flight switch, illustrates the principle behind dynamically displaying the corresponding control mechanism model through step S401:

[0106] The three-dimensional model of the control mechanism can be pre-built in a three-dimensional world, that is, the control mechanism model mentioned in step S401. If the current inspection guidance interface is an inspection guidance interface of the auxiliary key assembly, as shown in Figure 8b , when the user presses the forward flight switch according to Figure 8b , the forward flight switch will generate corresponding response data in real time during the process from being just pressed to passing through the key stroke and reaching the lowest position due to the existence of a certain key stroke. Therefore, the control system can collect these response data in real time and process the real-time position of the forward flight switch in this process according to the response data collected in real time, and further can continuously link the three-dimensional model of the forward flight key according to the real-time position, so that the dynamic change of the three-dimensional model of the forward flight key is consistent with the movement trajectory of the actual pressing of the forward flight key, as shown in Figure 12b , Figure 12b is a state diagram provided by an embodiment of the application for indicating that the forward flight switch is pressed in the inspection. It should be understood that Figure 12b is a state diagram of the three-dimensional model corresponding to the pressing of the forward flight key to the position in the dynamic display process of the three-dimensional model of the forward flight key. The state diagram is only one frame of image in the dynamic display process.

[0107] Therefore, according to the scheme shown in step S401, the pre-flight inspection method provided by the embodiment of the application can control the three-dimensional model of the control mechanism to display the corresponding state according to the response data collected in real time, realize the linkage control of the action of the control mechanism model by the actual control of the control mechanism by the user, and thus correctly and intuitively display the actual operation process of the control mechanism in the inspection guidance interface, so that the actual operation process can be intuitively understood.

[0108] As known from the above, the pre-flight inspection of the control mechanism involves multiple links. In order to facilitate the user to understand the pre-flight inspection progress of the control mechanism, in some embodiments, the pre-flight inspection method provided by the embodiment of the application further provides a progress prompting scheme of the pre-flight inspection, that is, the current inspection guidance interface further displays a plurality of inspection progress bars, and different inspection progress bars correspond to different inspection operations. Correspondingly, when the current inspection operation of the control mechanism is consistent with the inspection operation prompted by the current inspection guidance interface, the pre-flight inspection method provided by the embodiment of the application can further include:

[0109] In step S430, the progress bar corresponding to the inspection operation prompted by the current inspection guidance interface among the plurality of inspection progress bars is updated from the uncompleted state to the completed state.

[0110] For the above progress prompting scheme, the following related descriptions are made in combination with Figure 5 , Figure 9 and Figure 12f .

[0111] Referring to Figure 5 , Figure 5 The area indicated by reference sign A is the plurality of inspection progress bars. As can be seen, each inspection progress bar is in the form of an arc, and the plurality of inspection progress bars form a circular ring. However, it should be understood that the plurality of inspection progress bars provided by the embodiments of the present application are not limited to the form shown in the drawings. For example, the progress bars can also be in the form of line segments or dots, and the arrangement of the plurality of progress bars can not be limited. For example, the plurality of progress bars can be arranged in the form of regular figures such as circles or polygons, or can be arranged randomly. Figure 5

[0112] In the inspection guidance interface shown in Figure 5 , it can be seen that the corresponding progress bar is in an incomplete state and is in gray. When the user correctly completes the manipulation of the control stick according to the inspection guidance interface shown in Figure 5 , and the response data of the control stick indicates that the control stick is in place and there is no abnormality, it is considered that the inspection link shown in Figure 5 has been completed. At this time, the inspection guidance interface will be updated to the interface shown in Figure 9 . As can be seen, the progress bar at this time has been updated to a completed state and is in black. The gray and black colors are only used as examples for illustration and should not be understood as limiting the embodiments of the present application. In addition, in addition to using colors to distinguish the progress bars in the incomplete state and the completed state, a marking method can also be used to distinguish them. For example, a corresponding word or letter is marked on the progress bar in the incomplete state, and a word or letter different from that in the incomplete state is marked on the progress bar in the completed state.

[0113] In addition, if the inspection of all links of the control mechanism has been completed and the inspection results of all links are normal, at this time, all progress bars will be displayed in the completed state, or all progress bars can not be displayed, but a word prompt can be used to indicate that the control mechanism has passed the inspection, as shown in Figure 12f .

[0114] After the pre-flight inspection of the control mechanism is passed, it is usually necessary to fill in the flight logbook. Therefore, in order to facilitate the user to complete the above inspection operation, the next pre-flight inspection process can be continued directly in the display device. That is, in some embodiments, the pre-flight inspection method provided by the embodiments of the present application can further include:

[0115] In step S700, when an instruction indicating that the pre-flight inspection of the control mechanism has passed is received, the display device is controlled to display a flight logbook filling interface.

[0116] ​In the above, the flight log form filling interface can include a flight information input box to be filled, wherein the flight information includes but is not limited to pilot information, load information, and route information. In this interface, in order to enable the user to view the shape and state of the flight body, a three-dimensional model of the flight body can also be displayed, as shown in Figure 13 Figure 13 is a schematic diagram of a flight log form filling interface provided by an embodiment of the present application.

[0117] Similarly, after the pre-flight inspection of the control mechanism is passed or after the flight log is filled, a dynamic inspection of the rotor of the flight body is usually required. Therefore, in order to facilitate the user to complete the inspection operation of the control mechanism or the filling of the flight log, the next pre-flight inspection process can be directly continued in the display device. In some embodiments, the pre-flight inspection method provided by the embodiment of the present application can further include:

[0118] In step S800, the display device is controlled to display a dynamic inspection guidance interface; the dynamic inspection guidance interface displays a start control for starting the dynamic inspection and a model display area;

[0119] In step S920, when receiving an instruction generated by the start control being triggered, the rotor of the flight body is controlled to rotate and real-time rotor rotation data is acquired, and the flight body model displayed in the model display area is controlled to perform a corresponding action according to the rotation data.

[0120] It can be understood that, after the pre-flight inspection of the control mechanism is passed or after the flight log is filled, the control system can control the display device to switch from the current interface to the dynamic inspection guidance interface in step S800. In order to facilitate the user to start the dynamic inspection of the rotor of the flight body and enable the user to intuitively understand the running state of the rotor of the flight body in the dynamic inspection process, the dynamic inspection guidance interface is configured with a start control and a model display area, wherein the model display area is used to display a three-dimensional model of the flight body, as shown in Figure 14 Figure 14 is a schematic diagram of a dynamic inspection guidance interface provided by an embodiment of the present application, Figure 14 In the above, the control at the "start inspection" is the start control in step S800.

[0121] ​​After the user clicks the start control in the dynamic inspection guidance interface, the control system will receive the instruction generated by the triggering of the start control, and step S920 will be executed to control the rotor of the flight body to rotate and acquire the rotation data of the rotor in real time, and control the flight body model displayed in the model display area to perform corresponding actions according to the rotation data. The acquisition of the rotor rotation data and the linkage control of the actions of the flight body model based on the rotation data can refer to the related description above or related technologies.

[0122] From the above embodiment, it can be known that the rotor is constantly rotating in the process of dynamically inspecting the rotor of the flight body, and therefore it is necessary to pay attention to the safety of the environment around the flight body to avoid obstacles, human bodies or animals from entering the safety inspection range of the flight body. Based on this, in some embodiments, before controlling the rotor of the flight body to rotate, the pre-flight inspection method provided by the embodiments of the application can further include:

[0123] In step S910, the display device is controlled to display a three-dimensional map interface of the environment in which the flight body is located, and the three-dimensional map interface displays a safety confirmation control;

[0124] Correspondingly, in step S920, the rotor of the flight body is controlled to rotate and the rotation data of the rotor is acquired in real time, which is executed when the instruction generated by the triggering of the start control and the instruction generated by the triggering of the safety confirmation control are received.

[0125] It can be understood that when the instruction generated by the triggering of the start control is received and before the rotor of the flight body is controlled to rotate, step S910 is executed first to control the display device to display a three-dimensional map interface of the environment in which the flight body is located. The three-dimensional map in the three-dimensional map interface can be constructed from the environment images collected by the image collection device arranged on the shell of the flight body or the image collection device arranged in the environment in which the flight body is located, and the construction principle can refer to related technologies. After the three-dimensional map of the environment in which the flight body is located is constructed, it can be displayed in the display device, so that the user can determine whether there are obstacles, human bodies or animals in the safety inspection range of the flight body through the three-dimensional map, so as to avoid safety accidents.

[0126] When the user determines through the above three-dimensional map that there are no dangerous factors in the safety inspection range of the flight body, the user can click the safety confirmation control in the three-dimensional map interface to feed back the instruction indicating that the environment in which the flight body is located is safe to the control system, and the control system can execute step S920 to dynamically inspect the rotor of the flight body.

[0127] It is worth noting that the technical features or technical solutions in any of the above embodiments of the application can be combined with each other as long as there is no contradiction in combination.

[0128] To perform the corresponding steps in the above-mentioned embodiments and various possible manners, an implementation of a pre-flight inspection device is given below, which can optionally adopt the device structure of the electronic device shown in Figure 1 Further, please refer to Figure 15 , Figure 15 A functional module diagram of a pre-flight inspection device provided by an embodiment of the present application. It should be noted that the pre-flight inspection device provided by the present embodiment has the same basic principles and technical effects as the above-mentioned embodiments. For brief description, the part not mentioned in the present embodiment can refer to the corresponding content in the above-mentioned embodiments. The pre-flight inspection device 200 includes:

[0129] The guiding module 210 is configured to control the display device associated with the flight body to display the inspection guiding interface of the control mechanism when the flight body is in the pre-flight inspection stage of the control mechanism; the inspection guiding interface displays the control guiding animation of the control mechanism and the corresponding prompt information;

[0130] The determining module 220 is configured to, when receiving the response data fed back by the control mechanism being inspected, determine whether the current inspection operation of the control mechanism is consistent with the inspection operation prompted by the current inspection guiding interface according to the response data;

[0131] The switching module 230 is configured to, when the current inspection operation of the control mechanism is consistent with the inspection operation prompted by the current inspection guiding interface, and the current inspection guiding interface is not the last inspection guiding interface in the pre-flight inspection stage, control the display device to display the next inspection guiding interface of the control mechanism;

[0132] The cycling module 240 is configured to return to perform the step of determining whether the current inspection operation of the control mechanism is consistent with the inspection operation prompted by the current inspection guiding interface according to the response data when receiving the response data fed back by the control mechanism being inspected, until the current inspection guiding interface is the last inspection guiding interface.

[0133] In some embodiments, the pre-flight inspection device 200 can further include:

[0134] The dynamic control module is configured to, when receiving the response data fed back by the control mechanism being inspected, control the control mechanism model in the current inspection guiding interface to be displayed in the state corresponding to the current response data in real time.

[0135] In some embodiments, the pre-flight inspection device 200 can further include:

[0136] The state prompting module is configured to: when the current inspection operation of the steering mechanism is consistent with the inspection operation prompted by the current inspection guidance interface, control the current inspection guidance interface to display an inspection success prompt; and / or when the current inspection operation of the steering mechanism is inconsistent with the inspection operation prompted by the current inspection guidance interface, control the current inspection guidance interface to display an inspection error prompt.

[0137] In some embodiments, the state prompting module is further configured to: when the current inspection operation of the steering mechanism is consistent with the inspection operation prompted by the current inspection guidance interface, update the progress bar corresponding to the inspection operation prompted by the current inspection guidance interface from an uncompleted state to a completed state in the plurality of inspection progress bars.

[0138] In some embodiments, the steering mechanism includes a joystick, a throttle, and an auxiliary key assembly, and the auxiliary key assembly includes a plurality of keys.

[0139] The inspection guidance interface is provided with a plurality of inspection guidance interfaces, including an inspection guidance interface for guiding the forward pushing and clockwise rotation of the joystick, an inspection guidance interface for guiding the left and right twisting of the joystick, an inspection guidance interface for guiding the upward and downward pushing of the throttle, and an inspection guidance interface for guiding the sequential operation of the plurality of keys in the auxiliary key assembly.

[0140] In some embodiments, the guidance module 210 is further configured to:

[0141] Before the flight body enters the pre-flight inspection stage of the steering mechanism, when a take-off instruction is received, the display device is controlled to display a manual inspection list guidance interface; the manual inspection list guidance interface displays a plurality of inspection items and their respective corresponding guidance controls, and a model display area; different inspection items are used to indicate different parts of the flight body that need to be inspected;

[0142] When an instruction generated by the triggering of the guidance control is received, the target flight body part indicated by the inspection item corresponding to the currently triggered guidance control is obtained, and the model display area is controlled to display the target flight body part and the corresponding prompt information.

[0143] In some embodiments, the guidance module 210 is further configured to:

[0144] After the inspection of the flight body in the pre-flight inspection stage of the steering mechanism is completed, the display device is controlled to display a dynamic inspection guidance interface; the dynamic inspection guidance interface displays a start control for starting dynamic inspection, and a model display area.

[0145] Correspondingly, the pre-flight inspection device 200 can further include:

[0146] The rotor control module is configured to: when receiving an instruction generated by the activation control, control the rotor of the aircraft to rotate and acquire the rotation data of the rotor in real time, and control the aircraft model displayed in the model display area to perform corresponding actions based on the rotation data.

[0147] In some embodiments, the pre-flight inspection device 200 may further include:

[0148] The environment detection module is configured to: before the rotor control module controls the rotor of the aircraft to rotate, control the display device to display a three-dimensional map interface of the environment in which the aircraft is located, and the three-dimensional map interface displays safety confirmation controls.

[0149] Accordingly, the rotor control module only controls the rotor of the aircraft to rotate and acquires the rotor rotation data in real time when it receives the command generated by the start control and the command generated by the safety confirmation control.

[0150] Optionally, the above modules can be stored in the form of software or firmware. Figure 1 The memory shown is either stored in or embedded in the operating system (OS) of the electronic device, and can be... Figure 1 The processor executes the commands. Meanwhile, the data and program code required to execute these modules can be stored in memory.

[0151] In the several embodiments provided in this application, it should be understood that the disclosed apparatus and methods can also be implemented in other ways. The apparatus embodiments described above are merely illustrative; for example, the flowcharts and block diagrams in the accompanying drawings illustrate the architecture, functionality, and operation of possible implementations of apparatus, methods, and computer program products according to various embodiments of the present invention. In this regard, each block in a flowchart or block diagram may represent a module, segment, or portion of code containing one or more executable instructions for implementing a specified logical function. It should also be noted that in some alternative implementations, the functions marked in the blocks may occur in a different order than those marked in the drawings. For example, two consecutive blocks may actually be executed substantially in parallel, and they may sometimes be executed in reverse order, depending on the functions involved. It should also be noted that each block in a block diagram and / or flowchart, and combinations of blocks in block diagrams and / or flowcharts, can be implemented using a dedicated hardware-based system that performs the specified function or action, or using a combination of dedicated hardware and computer instructions.

[0152] In addition, each functional module in various embodiments of the present application can be integrated together to form an independent part, or each module can exist independently, or two or more modules can be integrated to form an independent part.

[0153] If the functions are realized in the form of software functional modules and sold or used as independent products, the functions can be stored in a computer readable storage medium. Based on this understanding, the technical solutions of the present application or the parts of the technical solutions that essentially contribute to the prior art can be embodied in the form of a software product. The computer software product is stored in a storage medium and includes a plurality of instructions for causing a computer device (which can be a personal computer, a server, or a network device, etc.) to execute all or part of the steps of the method described in various embodiments of the present application. The aforementioned storage medium includes a U disk, a mobile hard disk, a read-only memory (ROM), a random access memory (RAM), a magnetic disk or an optical disk, and various media that can store program codes.

[0154] The above only describes the preferred embodiments of the present application and is not intended to limit the present application. For those skilled in the art, the present application can have various modifications and changes. Any modification, equivalent replacement, improvement, etc. made within the spirit and principles of the present application shall be included in the protection scope of the present application.

Claims

1. A pre-flight inspection method, characterized in that, include: When the aircraft is in the pre-flight inspection phase of the control mechanism, the display device associated with the aircraft displays the inspection guidance interface of the control mechanism. The inspection guidance interface displays an animation guiding the operation of the control mechanism and corresponding prompts. When the response data is received from the inspection of the control mechanism, it is determined whether the current inspection operation of the control mechanism is consistent with the inspection operation prompted by the current inspection guidance interface based on the response data. When the current inspection operation of the control mechanism is consistent with the inspection operation prompted by the current inspection guidance interface, and the current inspection guidance interface is not the last inspection guidance interface in the pre-flight inspection phase, the display device is controlled to display the next inspection guidance interface of the control mechanism. When returning to the step of receiving response data from the inspection of the control mechanism, determining whether the current inspection operation of the control mechanism is consistent with the inspection operation prompted by the current inspection guidance interface based on the response data, until the current inspection guidance interface is the last inspection guidance interface.

2. The method according to claim 1, characterized in that, Upon receiving response data from the inspection of the control mechanism, the method further includes: The system provides real-time control over the operating mechanism model in the current inspection guidance interface, displaying the status corresponding to the current response data.

3. The method according to claim 1, characterized in that, When the current inspection operation of the control mechanism is consistent with the inspection operation prompted by the current inspection guidance interface, the method further includes: Controls the display of a successful inspection message on the current inspection guidance interface; And / or, when the current inspection operation of the operating mechanism is inconsistent with the inspection operation prompted by the current inspection guidance interface, the method further includes: Controls the display of error messages in the current inspection guide interface.

4. The method according to claim 1, characterized in that, The current inspection guide interface also displays multiple inspection progress bars, with different progress bars corresponding to different inspection operations; When the current inspection operation of the control mechanism is consistent with the inspection operation prompted by the current inspection guidance interface, the method further includes: Update the progress bar corresponding to the inspection operation prompted by the current inspection guidance interface from an incomplete state to a completed state.

5. The method according to claim 1, characterized in that, The control mechanism includes a joystick, a throttle, and an auxiliary button assembly, wherein the auxiliary button assembly includes multiple buttons; The inspection guidance interface includes multiple interfaces, including: an inspection guidance interface for guiding the joystick to be pushed forward and rotated clockwise one full turn; an inspection guidance interface for guiding the joystick to be turned left and right; an inspection guidance interface for guiding the throttle to be pushed up and down; and an inspection guidance interface for guiding the sequential operation of multiple buttons in the auxiliary button assembly.

6. The method according to claim 1, characterized in that, Before the aircraft enters the pre-flight inspection phase of the control mechanism, the method further includes: Upon receiving a takeoff command, the display device is controlled to show a manual inspection checklist guidance interface; the manual inspection checklist guidance interface displays: multiple inspection items and their corresponding guidance controls, as well as a model display area; different inspection items are used to indicate different parts of the aircraft that need to be inspected; When an instruction is received from the triggering of the guidance control, the target flying body part indicated by the inspection item corresponding to the currently triggered guidance control is obtained, and the model display area is controlled to display the target flying body part and the corresponding prompt information.

7. The method according to claim 1, characterized in that, After completing the pre-flight inspection phase of the flight vehicle's control mechanisms, the method further includes: The display device is controlled to display a dynamic inspection guidance interface; the dynamic inspection guidance interface displays: a start control for initiating dynamic inspection, and a model display area; When a command is received from the start control, the rotor of the aircraft is controlled to rotate and the rotation data of the rotor is acquired in real time. Based on the rotation data, the aircraft model displayed in the model display area is controlled to perform corresponding actions.

8. The method according to claim 7, characterized in that, Before controlling the rotor rotation of the flying body, the method further includes: The display device is controlled to display a three-dimensional map interface of the environment in which the flying object is located, and the three-dimensional map interface displays safety confirmation controls; Accordingly, the step of controlling the rotor rotation of the flight body and acquiring the rotor rotation data in real time is executed when an instruction generated by the activation control and an instruction generated by the safety confirmation control are received.

9. A pre-flight inspection device, characterized in that, include: The guidance module is configured to: when the aircraft is in the pre-flight inspection phase of the control mechanism, control the display device associated with the aircraft to display the inspection guidance interface of the control mechanism; the inspection guidance interface displays the control mechanism's operation guidance animation and corresponding prompt information. The determination module is configured to: upon receiving response data from the inspection of the control mechanism, determine whether the current inspection operation of the control mechanism is consistent with the inspection operation prompted by the current inspection guidance interface based on the response data; The switching module is configured to: when the current inspection operation of the control mechanism is consistent with the inspection operation prompted by the current inspection guidance interface, and the current inspection guidance interface is not the last inspection guidance interface in the pre-flight inspection phase, control the display device to display the next inspection guidance interface of the control mechanism. The loop module is configured to: return to the step of determining whether the current inspection operation of the operating mechanism is consistent with the inspection operation prompted by the current inspection guidance interface when the response data fed back by the inspection of the operating mechanism is received, until the current inspection guidance interface is the last inspection guidance interface.

10. An electronic device, characterized in that, It includes a processor and a memory, the memory storing machine-executable instructions that can be executed by the processor to implement the method of any one of claims 1 to 8.

11. A computer-readable storage medium having a computer program stored thereon, characterized in that, When the computer program is executed by a processor, it implements the method as described in any one of claims 1 to 8.

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