Pre-navigation inspection method, device and equipment and storage medium

Abstract

The embodiment of the invention provides a pre-flight inspection method, device and equipment and a storage medium, and the method comprises the steps: controlling display equipment associated with a flight body to display an inspection guide interface of a control mechanism when the flight body is in a pre-flight inspection stage 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 when the control mechanism is checked is received, whether the current check operation of the control mechanism is consistent with the check operation prompted by the current check guide interface or not is determined according to the response data; and 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-navigation inspection stage, controlling the display equipment to display the next inspection guide interface of the control mechanism.

Description

Technical Field

[0001] The present invention relates to the technical field of flying objects, and in particular to a pre-flight inspection method, device, equipment and storage medium. Background Art

[0002] Before a manned aircraft takes off, in order to ensure flight safety, it is usually necessary to conduct a pre-flight inspection of the manned aircraft, which includes external inspection of the aircraft, flight endurance status inspection, internal hardware inspection of the aircraft, and flight record sheet inspection. These pre-flight inspections are all completed by the crew according to standard operating documents such as the operating manual, maintenance manual, and flight checklist. The operating manual, maintenance manual, and flight checklist generally require personnel with relevant experience or relevant professional knowledge to understand. It is difficult for non-professionals to complete the pre-flight inspection based on these manuals, which shows that the threshold for pre-flight inspection is high; in addition, this method of requiring step-by-step reference to the manual and understanding before performing the inspection operation will not only bring a certain inspection burden to the inspectors, but also lead to low efficiency of pre-flight inspection. Summary of the invention

[0003] In view of this, an object of the present invention is to provide a pre-flight inspection method, device, equipment and storage medium to lower the threshold of pre-flight inspection and improve the efficiency of pre-flight inspection.

[0004] In order to achieve the above purpose, the technical solution adopted by the embodiment of the present invention is as follows:

[0005] A first aspect of an embodiment of the present invention provides a pre-flight inspection method, including:

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

[0007] When receiving response data fed back by the control mechanism being checked, 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;

[0008] 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, controlling the display device to display the next inspection guidance interface of the control mechanism;

[0009] 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 according to the response data when receiving the response data fed back by the operating mechanism being inspected, until the current inspection guidance interface is the last inspection guidance interface.

[0010] In an optional embodiment, upon receiving response data fed back by the control mechanism being inspected, the method further includes:

[0011] The manipulation mechanism model in the current inspection guidance interface is controlled in real time, and displayed in the state corresponding to the current response data.

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

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

[0014] 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:

[0015] Control the current inspection guide interface to display the inspection error prompt.

[0016] In an optional implementation, the current inspection guidance interface further displays multiple inspection progress bars, and different inspection progress bars correspond to different inspection operations;

[0017] When the current inspection operation of the operating mechanism is consistent with the inspection operation prompted by the current inspection guidance interface, the method further includes:

[0018] Among the multiple inspection progress bars, the progress bar corresponding to the inspection operation prompted by the current inspection guide interface is updated from an unfinished state to a completed state.

[0019] In an optional embodiment, the control mechanism includes a joystick, a throttle and an auxiliary button assembly, and the auxiliary button assembly includes a plurality of buttons;

[0020] There are multiple inspection guidance interfaces, including: an inspection guidance interface for guiding the operation of pushing the joystick forward and rotating it clockwise for one circle, an inspection guidance interface for guiding the operation of twisting the joystick left and right, an inspection guidance interface for guiding the operation of pushing the throttle up and down, and an inspection guidance interface for guiding the sequential operation of multiple buttons in the auxiliary button assembly.

[0021] In an optional embodiment, before the flying object enters the pre-flight inspection stage of the control mechanism, the method further includes:

[0022] When receiving a takeoff instruction, the display device is controlled to display a manual checklist guidance interface; the manual checklist guidance interface displays: multiple inspection items and their corresponding guidance controls, and a model display area; different inspection items are used to indicate different parts of the flying object that need to be inspected;

[0023] When receiving the instruction generated by the guidance control being triggered, 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 corresponding prompt information.

[0024] In an optional embodiment, after completing the inspection of the flying object in the pre-flight inspection stage of the control mechanism, the method further includes:

[0025] Controlling the display device to display a dynamic inspection guide interface; the dynamic inspection guide interface displays: a start control for starting a dynamic inspection, and a model display area;

[0026] When receiving the instruction generated by the triggering of the start control, the rotor of the flying object is controlled to rotate and the rotation data of the rotor is obtained in real time, and the flying object model displayed in the model display area is controlled to perform corresponding actions according to the rotation data.

[0027] In an optional embodiment, before controlling the rotor of the flying object to rotate, the method further includes:

[0028] Controlling the display device to display a three-dimensional map interface of the environment in which the flying object is located, wherein a safety confirmation control is displayed in the three-dimensional map interface;

[0029] Correspondingly, the step of controlling the rotation of the rotor of the flying body and acquiring the rotation data of the rotor in real time is executed when receiving the instruction generated by the triggering of the start control and the instruction generated by the triggering of the safety confirmation control.

[0030] A second aspect of an embodiment of the present invention provides a pre-flight inspection device, including:

[0031] The guidance module is configured to: when the flying object is in the pre-flight inspection stage of the control mechanism, control the display device associated with the flying object to display the inspection guidance interface of the control mechanism; the inspection guidance interface displays the control guidance animation of the control mechanism and corresponding prompt information;

[0032] A determination module is configured to: upon receiving response data fed back by the control mechanism being checked, determine 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;

[0033] a switching module 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 loop module is configured to: return to execute 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 according to the response data when the response data is received from the operating mechanism being inspected, until the current inspection guidance interface is the last inspection guidance interface.

[0035] According to a third aspect of an embodiment of the present invention, an electronic device is provided, including a processor and a memory, wherein the memory stores machine executable instructions that can be executed by the processor, and the processor can execute the machine executable instructions to implement the pre-flight inspection method provided in the first aspect above.

[0036] According to a fourth aspect of an embodiment of the present invention, a computer-readable storage medium is provided, on which a computer program is stored. When the computer program is executed by a processor, the pre-flight inspection method provided in the first aspect is implemented.

[0037] The pre-flight inspection method, apparatus, equipment and storage medium provided in the embodiments of the present invention, on the one hand, control a display interface associated with the flying body to display the control guidance animation and corresponding prompt information of the control mechanism when the flying body is in the pre-flight inspection stage of the control mechanism. This method of using animation combined with prompt information to guide the user on the pre-flight inspection content of the control mechanism is more intuitive and clear. Even ordinary users who do not have professional flying skills can quickly understand the current required control inspection of the control mechanism and related inspection operations through the control guidance animation, which effectively lowers the threshold for pre-flight inspection. On the other hand, when receiving the response data fed back by the user when checking the control mechanism, it is automatically 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 it is determined that the result is consistent, as long as the current is not the last inspection process of the control mechanism, it will automatically jump to the next inspection guidance interface to guide the user to perform the next inspection of the control mechanism. This method of linking the response data generated by the user's operation inspection of the control mechanism with the switching of the inspection process and the inspection guidance interface does not need to rely on manual judgment whether the current inspection process is completed and whether the control mechanism is faulty, and can avoid the problem of low pre-flight inspection efficiency caused by the user having to query the relevant manual for the next inspection after completing the current inspection process. It is conducive to ensuring the smooth progress of the inspection process and improving the efficiency of pre-flight inspection.

[0038] In order to make the above-mentioned objects, features and advantages of the present invention more obvious and easy to understand, preferred embodiments are given below and described in detail with reference to the accompanying drawings. BRIEF DESCRIPTION OF THE DRAWINGS

[0039] In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the drawings required for use in the embodiments are briefly introduced below. It should be understood that the following drawings only show certain embodiments of the present invention and therefore should not be regarded as limiting the scope. For ordinary technicians in this field, other related drawings can be obtained based on these drawings without creative work.

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

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

[0042] Figure 3 A schematic diagram of a manual checklist guidance interface provided by an embodiment of the present invention is shown;

[0043] Figure 4 A schematic diagram showing another manual checklist guidance interface provided by an embodiment of the present invention is shown;

[0044] Figure 5 A schematic diagram of an inspection guidance interface for guiding a joystick to be pushed forward and rotated clockwise for one circle provided by an embodiment of the present invention is shown;

[0045] Figure 6a A schematic diagram of an inspection guidance interface for guiding the left twisting of a joystick provided by an embodiment of the present invention is shown;

[0046] Figure 6b A schematic diagram of an inspection guidance interface for guiding the right twisting of a joystick provided by an embodiment of the present invention is shown;

[0047] Figure 7a A schematic diagram of a check guidance interface for guiding throttle push-up operation provided by an embodiment of the present invention is shown;

[0048] Figure 7b A schematic diagram of a check guidance interface for guiding throttle push-down operation provided by an embodiment of the present invention is shown;

[0049] Figure 8a A schematic diagram of an inspection guidance interface for guiding key switching of operation modes provided by an embodiment of the present invention is shown;

[0050] Figure 8bA schematic diagram of a check guidance interface for guiding the operation of a forward flight switch button provided by an embodiment of the present invention is shown;

[0051] Figure 8c A schematic diagram of a check guidance interface for guiding the operation of a left turn switch button provided by an embodiment of the present invention is shown;

[0052] Figure 8d A schematic diagram of an inspection guide interface for guiding the operation of pulling up a lifting switch provided by an embodiment of the present invention is shown;

[0053] Figure 8e A schematic diagram of an inspection guide interface for guiding the pressing of a lifting switch provided by an embodiment of the present invention is shown;

[0054] Figure 8f A schematic diagram of a check guide interface for guiding key switching back of an operation mode provided by an embodiment of the present invention is shown;

[0055] Fig. 9 A schematic diagram of an inspection guide interface for prompting a joystick to be pushed forward and rotated clockwise for one circle to pass the inspection provided by an embodiment of the present invention is shown;

[0056] Fig.10 A schematic diagram of an inspection guide interface for prompting that a left twist and a right twist of a joystick are qualified provided by an embodiment of the present invention is shown;

[0057] Fig.11 A schematic diagram of an inspection guidance interface for prompting that a throttle inspection is qualified provided by an embodiment of the present invention is shown;

[0058] Fig.12a A schematic diagram of an inspection guide interface for prompting a mode key switch inspection to be qualified provided by an embodiment of the present invention is shown;

[0059] Figure 12b A schematic diagram of a state for indicating that a forward flight switch is pressed during inspection provided by an embodiment of the present invention is shown;

[0060] Fig.12c A schematic diagram of an inspection guide interface for indicating that a forward flight switch and a backward flight switch have passed inspection provided by an embodiment of the present invention is shown;

[0061] Fig.12d A schematic diagram of an inspection guidance interface for indicating that a left-turn switch and a right-turn switch have passed inspection provided by an embodiment of the present invention is shown;

[0062] Fig.12e A schematic diagram of an inspection guidance interface for indicating that a lift switch has passed inspection provided by an embodiment of the present invention is shown;

[0063] Fig.12f A schematic diagram of an inspection guide interface for indicating that a mode button switchback inspection is qualified provided by an embodiment of the present invention is shown;

[0064] Fig.13 It is a schematic diagram of a flight log filling interface provided by an embodiment of the present invention;

[0065] Fig.14 is a schematic diagram of a dynamic inspection guidance interface provided by an embodiment of the present invention;

[0066] Fig.15 A functional module diagram of a pre-flight inspection device provided by an embodiment of the present invention is shown. DETAILED DESCRIPTION

[0067] The following will be combined with the accompanying drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of the embodiments. Generally, the components of the embodiments of the present invention described and shown in the drawings here can be arranged and designed in various different configurations.

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

[0069] It should be noted that relational terms such as "first" and "second" are used only to distinguish one entity or operation from another entity or operation, and do not necessarily require or imply any such actual relationship or order between these entities or operations. Moreover, the terms "include", "comprise" or any other variants thereof are intended to cover non-exclusive inclusion, so that a process, method, article or device including a series of elements includes not only those elements, but also other elements not explicitly listed, or also includes elements inherent to such process, method, article or device. In the absence of further restrictions, the elements defined by the sentence "comprise a ..." do not exclude the existence of other identical elements in the process, method, article or device including the elements.

[0070] In order to solve the technical problems of high threshold and low efficiency of pre-flight inspection in traditional technology due to the need to rely on professionals to complete the pre-flight inspection of the flying object according to standard operating documents such as operating manuals, maintenance manuals and flight checklists, the present invention provides a pre-flight inspection method. On the one hand, when the flying object is in the pre-flight inspection stage of the control mechanism, the display interface associated with the flying object is controlled to display the control guidance animation and corresponding prompt information of the control mechanism. This method of using animation combined with prompt information to guide the user on the pre-flight inspection content of the control mechanism is more intuitive and clear. Even ordinary users who do not have professional skills in flying objects can quickly understand the current required control inspection of the control mechanism and related inspection operations through the control guidance animation. It can be seen that the threshold of pre-flight inspection is effectively lowered. On the other hand, when receiving the response data fed back by the user when checking the control mechanism, it is automatically 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 it is determined that the result is consistent, as long as the current is not the last inspection process of the control mechanism, it will automatically jump to the next inspection guidance interface to guide the user to perform the next inspection of the control mechanism. This method of linking the response data generated by the user's operation inspection of the control mechanism with the switching of the inspection process and the inspection guidance interface does not need to rely on manual judgment whether the current inspection process is completed and whether the control mechanism is faulty, and can avoid the problem of low pre-flight inspection efficiency caused by the user having to query the relevant manual for the next inspection after completing the current inspection process. It is conducive to ensuring the smooth progress of the inspection process and improving the efficiency of pre-flight inspection.

[0071] The pre-flight inspection method provided by the present invention can be applied to electronic equipment. Figure 1 , is a block diagram of the structure 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 electrically connected to each other directly or indirectly to achieve data transmission or interaction. For example, these components 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, a random access memory (RAM), a read only memory (ROM), a programmable read-only memory (PROM), an erasable programmable read-only memory (EPROM), an electrically erasable programmable read-only memory (EEPROM), etc.

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

[0074] The communication module is used to establish a communication connection between the electronic device and other communication terminals through a network, and is used to send and receive data through the network.

[0075] It should be understood that Figure 1 The structure shown is only a schematic diagram of the structure of the electronic device, and the electronic device may also include Figure 1 More or fewer components as shown, or with Figure 1 Different configurations are shown. Figure 1 Each component shown in the figure can be implemented by 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 a 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 by the embodiment of the present invention is described. Figure 3 1 is a flow chart of a pre-flight inspection method provided by an embodiment of the present invention, wherein the pre-flight inspection method comprises:

[0078] In step S300, when the flying object is in the pre-flight inspection stage of the control mechanism, the display device associated with the flying object is controlled to display the inspection guidance interface of the control mechanism; the inspection guidance interface displays the control guidance animation of the control mechanism and corresponding prompt information;

[0079] In step S400, when receiving the response data fed back by the control mechanism being checked, 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;

[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, controlling the display device to display the next inspection guidance interface of the control mechanism;

[0081] In step S600, the step of returning 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 according to the response data received when the operating mechanism is inspected is received, until the current inspection guidance interface is the last inspection guidance interface.

[0082] Before an aircraft takes off, in order to ensure the safe flight of the aircraft, it is usually necessary to conduct a pre-flight inspection of the aircraft. Among them, in order to at least simplify the tediousness of the inspection of the control mechanism in the pre-flight inspection, 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 present invention can be pre-configured in the control system of the aircraft, so that when the control system receives the take-off instruction of the aircraft, it does not control the take-off of the aircraft first, but triggers the aircraft to enter the pre-flight inspection process, and guides the user to perform a pre-flight inspection of the aircraft through the pre-flight inspection method provided by the embodiment of the present invention. Based on this, the display device in the above step S300 can be a display device configured in the cockpit of the aircraft.

[0083] In some embodiments, in order to cover more inspection contents of the pre-flight inspection of the flying object, to provide users with pre-flight inspection guidance for more inspection links, to further lower the threshold of pre-flight inspection and to improve the overall efficiency of pre-flight inspection, the pre-flight inspection method provided by the embodiment of the present invention further provides another inspection link before the pre-flight inspection stage of the control mechanism - an inspection guidance scheme for manual inspection work orders, that is, before the flying object enters the pre-flight inspection stage of the control mechanism, the pre-flight inspection method provided by the embodiment of the present invention may also include:

[0084] In step S100, upon receiving a takeoff instruction, the display device is controlled to display a manual checklist guidance interface; the manual checklist guidance interface displays: a plurality of check items and their corresponding guidance controls, and a model display area; different check items are used to indicate different parts of the flying object that need to be checked;

[0085] In step S200, when an instruction generated by triggering a guidance control is received, 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 corresponding prompt information.

[0086] See also Figure 3 and Figure 4, Figure 3 is a schematic diagram of a manual checklist guidance interface provided by an embodiment of the present invention. Figure 4 This is a schematic diagram of another manual inspection list guidance interface provided by an embodiment of the present invention. Figure 3 and Figure 4 The following describes the pre-flight inspection guidance principle of the above steps S100 to S200:

[0087] When the user controls the flight object to take off through the user interface on the flight object display device, the user interface of the associated terminal device, or the remote control or the joystick, the take-off instruction recorded in step S100 is generated. At this time, the execution subject of the pre-flight check provided by the embodiment of the present invention, for example, the control system of the flight object, will receive the take-off instruction and execute step S100 to control the display device to display the manual checklist guidance interface, such as Figure 3 As shown, the manual checklist guidance interface at this time displays multiple inspection items: "Arm", "Rotor", "Landing Gear", "Electric Drive", "Duct", "Inside the Cabin" and "Buzzer Inspection". Figure 3 There is a guide control on the right side of each inspection item. For example, there is a control with a play button graphic on the right side of "arm", and there is a control with a volume graphic surrounded by a rectangular frame on the right side of "buzzer inspection". These controls are guide controls. In addition, the manual inspection list guide interface also displays a model display area, such as Figure 3 As shown, the model display area at this time displays the whole aircraft model of the aircraft, which may indicate that the user has not yet started the pre-flight check for the manual checklist, so the whole aircraft model of the aircraft is first displayed in the model display area.

[0088] After the manual checklist guidance interface is displayed in step S100, the user can gradually complete the inspection of the corresponding components in the flying object according to the inspection items indicated in the manual checklist. During the inspection process, if the user is not sure which part of the flying object a certain component refers to, the user can click the guidance control corresponding to the corresponding inspection item in the manual checklist guidance interface, for example, click the guidance control corresponding to "duct". At this time, the control system can receive the instruction generated by the guidance control being triggered, and execute step S200 to obtain the target flying object part indicated by the inspection item corresponding to the currently triggered guidance control. For example, Figure 4 As shown, the "duct" part of the flying body is obtained, and the model display area is controlled to display the "duct" part and the prompt information: "Check the duct", "The fasteners at the connection of the duct connector are intact". In this way, the user can check the corresponding part of the flying body according to the body part displayed in the model display area, and the inspection content can also be learned from the prompt information displayed in the model display area.

[0089] Therefore, through the manual checklist guidance scheme in the above-mentioned steps S100 to S200, ordinary users can quickly complete the pre-flight inspection of the manual checklist stage of the flying object according to the guidance, which is conducive to lowering the threshold for ordinary users to inspect the external structure of the flying object, and is conducive to further improving the overall efficiency of the pre-flight inspection and user experience.

[0090] After the user completes the pre-flight inspection of the manual checklist stage and confirms that the corresponding flight body parts meet the pre-flight inspection requirements, as one example, the "Complete Confirmation" control configured in the manual checklist guidance interface can be used to trigger the control system to perform guidance for the next pre-flight inspection stage, and the pre-flight inspection stage of the control mechanism will be entered. Among them, the triggering operation of the control system to perform guidance for the next pre-flight inspection stage may not rely on the "Complete Confirmation" control configured in the manual checklist guidance interface. In other examples, it can also be implemented by voice input or other binding terminal devices inputting corresponding instructions, which is not limited in the embodiments of the present invention.

[0091] When the flying object is in the pre-flight inspection stage of the control mechanism, the control system will execute step S300 to control the above-mentioned display device to display the inspection guidance interface of the control mechanism, and display the control guidance animation of the control mechanism and the corresponding prompt information in the inspection guidance interface. As an example, the control mechanism of the flying object includes a joystick, a throttle and an auxiliary button assembly; the auxiliary button assembly is used as a backup control mechanism for the joystick, and may include the following buttons for controlling the flight of the flying object: mode button, forward flight switch, backward flight switch, left turn switch, right turn switch and lifting switch. Based on this, in some embodiments, in order to realize the orderly inspection of the control mechanism and avoid prompting too much information at one time to cause confusion in the inspection operation, the embodiment of the present invention splits the complex steps involved in the inspection into single simple steps, and configures a corresponding inspection guidance interface for this purpose, so that the entire pre-flight inspection process of the control mechanism is simple and clear, thereby further improving the efficiency of the pre-flight inspection. That is, there may be multiple inspection guide interfaces, including: an inspection guide interface for guiding the joystick to push forward and rotate clockwise for one circle, an inspection guide interface for guiding the joystick to twist left and right, an inspection guide interface for guiding the throttle to push up and push down, and an inspection guide interface for guiding the sequential manipulation of multiple buttons in the auxiliary button assembly. Figure 6a and Figure 6b , Figure 6a is a schematic diagram of an inspection guidance interface for guiding the left twisting of a joystick provided by an embodiment of the present invention, Figure 6b is a schematic diagram of a check guide interface for guiding the right twist of the joystick provided by an embodiment of the present invention. Similarly, the relevant guide interface for the throttle can be found in Figure 7a and Figure 7b, Figure 7a is a schematic diagram of a check guidance interface for guiding the throttle push-up operation provided by an embodiment of the present invention, Figure 7b is a schematic diagram of a check guide interface for guiding the operation of throttle push-down provided by an embodiment of the present invention. Similarly, in the check guide interface for guiding the sequential operation of multiple buttons in the auxiliary button assembly, there will be a corresponding prompt interface for each button, please refer to Figure 8a to Figure 8f , Figure 8a is a schematic diagram of an inspection guidance interface for guiding key switching of operation modes provided by an embodiment of the present invention, Figure 8b is a schematic diagram of an inspection guidance interface for guiding the operation of a forward flight switch button provided by an embodiment of the present invention, Figure 8c is a schematic diagram of an inspection guidance interface for guiding the operation of a left turn switch button provided by an embodiment of the present invention, Figure 8d is a schematic diagram of an inspection guide interface for guiding the operation of pulling up a lifting switch provided by an embodiment of the present invention, Figure 8e is a schematic diagram of an inspection guide interface for guiding the operation of pressing a lifting switch provided by an embodiment of the present invention, Figure 8f It is a schematic diagram of a check guidance interface for guiding key switching back of an operation mode provided by an embodiment of the present invention.

[0092] It can be seen that no matter which inspection guidance interface diagram, the virtual model corresponding to the component currently being inspected in the control mechanism will be used to construct the corresponding animation and prompt information of the virtual model according to the content to be inspected, and then display it, so that the user can clearly understand the inspection operation of the corresponding components according to the animation, and can also combine the prompt information to have a clearer understanding of the content of the animation display. Therefore, ordinary users who do not have professional flight skills can also quickly understand the current required control inspection and related inspection operations of the control mechanism through the control guidance animation, effectively lowering the threshold for pre-flight inspection.

[0093] After the user performs corresponding operations on the operating mechanism according to the operation guidance animation and corresponding prompts of the current inspection guidance interface currently displayed by the display device, for example, assuming that the current inspection guidance interface is Figure 5 The guidance interface shown instructs the user to push the joystick forward and rotate it clockwise for one circle according to the animation and text prompts. After the user operates the joystick according to the prompt, if the joystick and related sensors are normal, the control system will receive response data generated after the joystick is operated. The response data may include displacement data and rotation angle data of the joystick. These data can be collected by corresponding sensors. For details, please refer to the relevant technology.

[0094] After receiving the response data, step S400 is executed to determine whether the current inspection operation of the operating mechanism is consistent with the inspection operation prompted by the current inspection guidance interface according to the response data. Figure 5 For example, the inspection operation prompted by the inspection guidance interface is to push the joystick forward and rotate it clockwise for one circle. Then, the displacement threshold corresponding to the joystick being pushed forward to the desired position and the angle threshold corresponding to the joystick being rotated clockwise for one circle can be configured in advance according to the data standard to be inspected. Thus, in the process of executing step S400, it can be determined whether the displacement in the response data at the end of the operation satisfies the above displacement threshold and whether the angle satisfies the above angle threshold. If both are satisfied, it means that the current inspection operation of the operating mechanism is consistent with the inspection operation prompted by the current inspection guidance interface. If one of them is not satisfied, it means that the current inspection operation of the operating mechanism is inconsistent with the inspection operation prompted by the current inspection guidance interface. This result may be caused by the user's inadequate operation or by a malfunction of the operating mechanism. In either case, in order to facilitate users to understand the inspection results in a timely manner, in some embodiments, the pre-flight inspection method provided in an embodiment of the present invention also provides a feedback scheme for the inspection results, that is, the pre-flight inspection method provided in an embodiment of the present invention may also 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 operating 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] From the above steps S410 and S420, it can be seen that when the current inspection operation of the control mechanism is consistent with the inspection operation prompted by the current inspection guidance interface, the current inspection guidance interface is controlled to display the inspection success prompt to indicate that the control mechanism responds normally and meets the takeoff standard of the corresponding component. The inspection success prompt can be any form of number. In order to more intuitively indicate success, in some examples, the inspection success prompt can be set to a pattern related to √, for example, see Figure 9 to Figure 12a ,as well as Figure 12c to Figure 12f , Fig. 9 is a schematic diagram of an inspection guide interface for prompting a joystick to be pushed forward and rotated clockwise for one circle to pass the inspection, provided by an embodiment of the present invention. Fig.10 is a schematic diagram of an inspection guide interface for prompting that a joystick left twist and right twist inspection is qualified, provided by an embodiment of the present invention. Fig.11is a schematic diagram of an inspection guidance interface for prompting that a throttle inspection is qualified, provided by an embodiment of the present invention. Fig.12a is a schematic diagram of an inspection guide interface for prompting mode key switching inspection to be qualified provided by an embodiment of the present invention, Fig.12c is a schematic diagram of an inspection guide interface for indicating that a forward flight switch and a backward flight switch have passed the inspection provided by an embodiment of the present invention. Fig.12d is a schematic diagram of an inspection guidance interface for indicating that a left-turn switch and a right-turn switch have passed inspection, provided by an embodiment of the present invention. Fig.12e is a schematic diagram of an inspection guide interface for indicating that a lift switch has passed the inspection provided by an embodiment of the present invention. Fig.12f is a schematic diagram of an inspection guidance interface for indicating a qualified inspection of a mode key switch back provided by an embodiment of the present invention. It can be seen that for each link of the pre-flight inspection performed by the control mechanism, when the current inspection operation of the control mechanism is consistent with the inspection operation prompted by the current inspection guidance interface, an inspection success prompt will be displayed in the corresponding interface, such as Fig. 9 The pattern formed by a white tick surrounded by a green square before the prompt "Push forward and rotate clockwise one circle" Figure 10 to Figure 12a ,as well as Figure 12c to Figure 12f The same goes for this.

[0099] On the contrary, 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 the inspection error prompt to indicate that the control mechanism is abnormal or the manual operation is incorrect and does not meet the takeoff standard. Similarly, the inspection error prompt can refer to the example of the inspection success prompt and be configured as long as it is inconsistent with the inspection success prompt. However, in order to more intuitively indicate success, in some examples, the inspection error prompt can be set to a pattern related to ×.

[0100] In addition to implementing the feedback of the inspection results through the schemes in step S410 and step S420, in other variant embodiments, the inspection results can also be output by voice broadcast, so that the user can also know the inspection results in time. In addition, based on the schemes in step S410 and step S420, the output of the inspection results can be further enhanced by combining the voice playback method to better attract the user's attention. Based on this, in other embodiments, the prompt information recorded above can be played by voice playback in addition to being displayed through the interface.

[0101] From the above, it can be seen that the current inspection operation of the control mechanism is consistent with the inspection operation prompted by the current inspection guidance interface, indicating that the control mechanism responds normally and meets the takeoff standard of the corresponding component. In this way, it can be considered that a certain inspection of the corresponding component has been completed. If there are still items that have not been inspected, that is, the current inspection guidance interface is not the last inspection guidance interface in the pre-flight inspection stage, step S500 will be executed to control the display device to display the next inspection guidance interface of the control mechanism, for example, the completion Figure 5 After checking as shown, you can switch to Figure 6a The inspection guide interface shown in the figure is as follows. If each subsequent inspection is qualified, Figure 6a Gradually switch to Figure 8f , thus completing the pre-flight inspection of all items of 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 instructions of the current inspection guidance interface. If the cumulative number of operations reaches the set number threshold, the control mechanism can be considered to be abnormal. Since the pre-flight inspection of the flight body is to ensure flight safety, as long as an abnormality is detected, it can be considered that the flight body does not meet the take-off standards, and there is no need to continue to inspect other items, that is, there is no need to switch from the current inspection guidance interface to the next inspection guidance interface. Instead, the 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 flight body.

[0103] As can be seen from the above, although the user can be informed of the inspection status of the control mechanism in a timely manner through the inspection success prompt or the inspection error prompt, the user cannot obtain the relevant data in the process of the control mechanism operation inspection, nor can the user intuitively understand which operations in the operation inspection have problems. Therefore, in order to solve this technical problem, in some embodiments, the pre-flight inspection method provided by the embodiment of the present invention may also include a scheme for linking and displaying the status of the control mechanism model in the inspection guide interface in real time according to the response data, that is, the pre-flight inspection method provided by the embodiment of the present invention may also include:

[0104] In step S401, the manipulation mechanism model in the current inspection guidance interface is controlled in real time to display the state corresponding to the current response data.

[0105] The following uses the response data of the previous flight switch as an example to explain the principle of implementing the dynamic display of the corresponding control mechanism model through step S401:

[0106] A three-dimensional model of the operating mechanism can be pre-constructed in the three-dimensional world, that is, the operating mechanism model mentioned in step S401. If the current inspection guide interface is the inspection guide interface of the auxiliary button component, such as Figure 8b As shown, when the user follows Figure 8b In the process of pressing the forward flight switch as shown in the inspection guide, the forward flight switch has a certain key travel, so the corresponding response data will be generated in real time during the process from when the forward flight switch is just pressed to when it passes through the above key travel and reaches the lowest position. 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 then the three-dimensional model of the forward flight button can be continuously linked according to the real-time position, so that the dynamic changes presented by the three-dimensional model of the forward flight button are consistent with the motion trajectory of the forward flight button when it is actually pressed, such as Figure 12b As shown, Figure 12b is a schematic diagram of a state for indicating that the forward flight switch is pressed during inspection provided by an embodiment of the present invention. It should be understood that Figure 12b It is a state diagram of the corresponding three-dimensional model when the forward flight button is pressed into place during the dynamic display process of the forward flight button three-dimensional model. The state diagram is only one frame of image in the dynamic display process.

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

[0108] As can be seen from the above, the pre-flight inspection involved in the control mechanism has multiple links. Because, in order to facilitate users to understand the progress of the pre-flight inspection of the control mechanism, in some embodiments, the pre-flight inspection method provided by the embodiment of the present invention also provides a progress prompt scheme for the pre-flight inspection, that is, the current inspection guide interface also displays multiple inspection progress bars, and different inspection progress bars correspond to different inspection operations. Accordingly, when the current inspection operation of the control mechanism is consistent with the inspection operation prompted by the current inspection guide interface, the pre-flight inspection method provided by the embodiment of the present invention may also include:

[0109] In step S430, the progress bar corresponding to the inspection operation prompted by the current inspection guide interface among the multiple inspection progress bars is updated from an unfinished state to a completed state.

[0110] For the above progress prompt scheme, the following combination Figure 5 , Fig. 9 and Fig.12f For relevant instructions:

[0111] See also Figure 5 , Figure 5 The area indicated by the label A is a plurality of inspection progress bars. It can be seen that each inspection progress bar is in an arc shape, and the plurality of inspection progress bars surround a ring. However, it should be understood that the plurality of inspection progress bars provided in the embodiment of the present invention are not limited to Figure 5 As shown in the presentation method, for example, the progress bar can also be presented in a line segment shape or a dot shape, and the arrangement of multiple progress bars can be unlimited. For example, they can be arranged in regular shapes such as circles, polygons, etc., but they can also be arranged randomly.

[0112] exist Figure 5 In the inspection guide interface shown, the corresponding progress bar is in an unfinished state and is grayed out. Figure 5 When the joystick operation is completed correctly on the inspection guide interface shown in the figure, and the joystick response data also indicates that the joystick inspection is in place and there is no abnormality, it is considered Figure 5 The inspection steps shown have been completed, and the inspection guide interface will be updated to Fig. 9 In the interface shown, it can be seen that the progress bar has been updated to the completed state and is black. The gray and black colors are only used as examples and should not be understood as limitations on the embodiments of the present invention. In addition, in addition to using colors to distinguish the progress bars in the unfinished state and the completed state, marking can also be used to distinguish them. For example, the corresponding text or letters are marked on the progress bar in the unfinished state, and the text or letters different from the unfinished state are 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, all progress bars will be displayed in a completed state. Alternatively, all progress bars may not be displayed, but text prompts may be used to indicate that the control mechanism has passed the inspection, such as Fig.12f shown.

[0114] After the pre-flight inspection of the control mechanism is passed, generally speaking, a flight record sheet needs to be filled out. 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 embodiment of the present invention may also include:

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

[0116] In the above, the flight log filling interface may include a flight information input box that needs to be filled in, where the flight information includes but is not limited to: pilot information, load information, and route information. In this interface, in order to allow users to view the shape and status of the flying object, a three-dimensional model of the flying object can also be displayed, such as Fig.13 As shown, Fig.13 It is a schematic diagram of a flight log filling interface provided by an embodiment of the present invention.

[0117] Similarly, after the pre-flight inspection of the control mechanism is passed, or after the flight log is completed, it is usually necessary to perform a dynamic inspection on the rotor of the flying object. Therefore, in order to facilitate the user to complete the inspection operation of the control mechanism or fill in the flight log, the next pre-flight inspection process can be directly continued in the display device. That is, in some embodiments, the pre-flight inspection method provided by the embodiment of the present invention may also include:

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

[0119] In step S920, when an instruction generated by the start control being triggered is received, the rotor of the flying object is controlled to rotate and the rotation data of the rotor is obtained in real time, and the flying object model displayed in the model display area is controlled to perform corresponding actions according to the rotation data.

[0120] It is understandable that after the pre-flight inspection of the control mechanism is passed, or after the flight log is completed, the control system can control the display device to switch from the current interface to the dynamic inspection guidance interface in step S800, wherein, in order to facilitate the user to start the dynamic inspection of the rotor of the flying object and facilitate the user to intuitively understand the rotor operation status of the flying object during 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 flying object, such as Fig.14 As shown, Fig.14 is a schematic diagram of a dynamic inspection guidance interface provided by an embodiment of the present invention. Fig.14 In the example, the control at "Start Checking" 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 will execute step S920 to control the rotation of the rotor of the flying object and obtain the rotation data of the rotor in real time, and control the flying object model displayed in the model display area to perform corresponding actions according to the rotation data. Among them, the acquisition of the rotor rotation data and the corresponding principle of controlling the action of the flying object model based on the rotation data can refer to the relevant records above, and can also refer to the relevant technology.

[0122] As can be seen from the previous embodiment, during the dynamic inspection of the rotor of the flying object, the rotor is constantly rotating, so it is necessary to pay attention to the safety of the environment around the flying object to prevent obstacles or human beings or animals from entering the safety inspection range of the flying object. Based on this, in some embodiments, before controlling the rotation of the rotor of the flying object, the pre-flight inspection method provided by the embodiment of the present invention may also include:

[0123] In step S910, the display device is controlled to display a three-dimensional map interface of the environment in which the flying object is located, wherein a safety confirmation control is displayed in the three-dimensional map interface;

[0124] Correspondingly, in step S920, the step of controlling the rotation of the rotor of the flying body and acquiring the rotation data of the rotor in real time is executed when receiving the instruction generated by the start control being triggered and the instruction generated by the safety confirmation control being triggered.

[0125] It is understandable that when the instruction generated by the triggering of the start control is received, and before the rotor of the flying body is controlled to rotate, step S910 is first executed to control the display device to display a three-dimensional map interface of the flying body's environment. The three-dimensional map in the three-dimensional map interface can be constructed by an image acquisition device arranged at the outer shell of the flying body, or an image acquisition device arranged in the flying body's environment. The construction principle can be found in the relevant technology. After the three-dimensional map of the flying body's environment is constructed, it can be displayed on the display device, so that the user can determine whether there are obstacles, human bodies or animals within the safety inspection range of the flying body through the three-dimensional map, thereby avoiding safety accidents.

[0126] When the user determines through the above-mentioned three-dimensional map that there are no dangerous factors in the safety inspection range of the flying object, he can click the safety confirmation control in the three-dimensional map interface to feedback instructions indicating that the environment in which the flying object is located is safe to the control system. The control system can then execute step S920 to perform a dynamic inspection of the rotor of the flying object.

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

[0128] In order to execute the corresponding steps in the above embodiments and various possible methods, a method for implementing a pre-flight inspection device is given below. Optionally, the pre-flight inspection device can adopt the above Figure 1 For further information, please refer to Fig.15 , Fig.15 This is a functional module diagram of a pre-flight inspection device provided by an embodiment of the present invention. It should be noted that the basic principle and technical effects of the pre-flight inspection device provided by this embodiment are the same as those of the above embodiments. For the sake of brief description, for parts not mentioned in this embodiment, reference can be made to the corresponding contents in the above embodiments. The pre-flight inspection device 200 includes:

[0129] The guidance module 210 is configured to: when the aircraft is in the pre-flight inspection stage 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 guidance animation of the control mechanism and corresponding prompt information;

[0130] The determination module 220 is configured to: upon receiving response data fed back by the control mechanism being checked, determine 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;

[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 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;

[0132] The loop module 240 is configured to: return to execute 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 based on the response data received when the operating mechanism is inspected, until the current inspection guidance interface is the last inspection guidance interface.

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

[0134] The dynamic control module is configured to: upon receiving the response data fed back by the control mechanism being inspected, control the control mechanism model in the current inspection guidance interface in real time to display the state corresponding to the current response data.

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

[0136] The status prompt module is configured to: when the current inspection operation of the operating 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 operating 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 above-mentioned status prompt module is also configured to: when the current inspection operation of the operating 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 among the multiple inspection progress bars from an unfinished state to a completed state.

[0138] In some embodiments, the control mechanism includes a joystick, a throttle, and an auxiliary button assembly, and the auxiliary button assembly includes a plurality of buttons;

[0139] There are multiple inspection guidance interfaces, including: an inspection guidance interface for guiding the operation of pushing the joystick forward and rotating it clockwise for one circle, an inspection guidance interface for guiding the operation of twisting the joystick left and right, an inspection guidance interface for guiding the operation of pushing the throttle up and down, and an inspection guidance interface for guiding the sequential operation of multiple buttons in the auxiliary button assembly.

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

[0141] Before the flying object enters the pre-flight inspection stage of the control mechanism, upon receiving a take-off instruction, the display device is controlled to display a manual checklist guidance interface; the manual checklist guidance interface displays: multiple inspection items and their corresponding guidance controls, and a model display area; different inspection items are used to indicate different parts of the flying object that need to be inspected;

[0142] When receiving the instruction generated by the guidance control being triggered, 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 corresponding prompt information.

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

[0144] After completing the pre-flight inspection of the control mechanism of the flying object, 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.

[0145] Accordingly, the pre-flight inspection device 200 may further include:

[0146] The rotor control module is configured to: when receiving the instruction generated by the start control being triggered, control the rotation of the rotor of the flying body and obtain the rotation data of the rotor in real time, and control the flying body model displayed in the model display area to perform corresponding actions according to 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 flying object to rotate, control the display device to display a three-dimensional map interface of the environment in which the flying object is located, wherein a safety confirmation control is displayed in the three-dimensional map interface.

[0149] Correspondingly, the rotor control module controls the rotation of the rotor of the flying body and obtains the rotation data of the rotor in real time only when receiving the instruction generated by the triggering of the start control and the instruction generated by the triggering of the safety confirmation control.

[0150] Optionally, the above modules can be stored in the form of software or firmware. Figure 1 The memory shown in the figure or solidified in the operating system (OS) of the electronic device, and can be Figure 1 Meanwhile, the data and program codes required for executing the above modules can be stored in the memory.

[0151] In several embodiments provided in the present application, it should be understood that the disclosed devices and methods can also be implemented in other ways. The device embodiments described above are merely schematic. For example, the flowcharts and block diagrams in the accompanying drawings show the possible architecture, functions and operations of the devices, methods and computer program products according to multiple embodiments of the present invention. In this regard, each box in the flowchart or block diagram can represent a module, a program segment or a part of a code, and the module, a program segment or a part of a code contains one or more executable instructions for implementing the specified logical function. It should also be noted that in some alternative implementations, the functions marked in the box can also occur in a different order from the order marked in the accompanying drawings. For example, two consecutive boxes can actually be executed substantially in parallel, and they can sometimes be executed in the opposite order, depending on the functions involved. It should also be noted that each box in the block diagram and / or flowchart, and the combination of boxes in the block diagram and / or flowchart can be implemented with a dedicated hardware-based system that performs a specified function or action, or can be implemented with a combination of dedicated hardware and computer instructions.

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

[0153] If the functions are implemented in the form of software function modules and sold or used as independent products, they can be stored in a computer-readable storage medium. Based on this understanding, the technical solution of the present invention, or the part that contributes to the prior art or the part of the technical solution, can be embodied in the form of a software product. The computer software product is stored in a storage medium, including several instructions for enabling a computer device (which can be a personal computer, a server, or a network device, etc.) to perform all or part of the steps of the methods described in each embodiment of the present invention. The aforementioned storage medium includes: various media that can store program codes, such as a USB flash drive, a mobile hard disk, a read-only memory (ROM), a random access memory (RAM), a magnetic disk or an optical disk.

[0154] The above description is only a preferred embodiment of the present invention and is not intended to limit the present invention. For those skilled in the art, the present invention may have various modifications and variations. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present invention shall be included in the protection scope of the present invention.

Claims

1. A pre-flight inspection method, characterized in that: include: When the flying object is in the pre-flight inspection stage of the control mechanism, controlling a display device associated with the flying object to display an inspection guidance interface of the control mechanism; The inspection guidance interface displays the operation guidance animation of the operating mechanism and corresponding prompt information; When receiving response data fed back by the control mechanism being checked, 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; 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, controlling the display device to display the next inspection guidance interface of the control mechanism; 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 according to the response data when receiving the response data fed back by the operating mechanism being inspected, until the current inspection guidance interface is the last inspection guidance interface.

2. The method according to claim 1, characterized in that When receiving the response data fed back by the control mechanism being checked, the method further includes: The operating mechanism model in the current inspection guidance interface is controlled in real time, and displayed in the state corresponding to the current response data.

3. The method according to claim 1, characterized in that When the current inspection operation of the operating mechanism is consistent with the inspection operation prompted by the current inspection guidance interface, the method further includes: Control the current inspection guidance interface to display the inspection success prompt; 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: Control the current inspection guide interface to display the inspection error prompt.

4. The method according to claim 1, characterized in that: The current inspection guidance interface also displays multiple inspection progress bars, and different inspection progress bars correspond to different inspection operations; When the current inspection operation of the operating mechanism is consistent with the inspection operation prompted by the current inspection guidance interface, the method further includes: Among the multiple inspection progress bars, the progress bar corresponding to the inspection operation prompted by the current inspection guide interface is updated from an unfinished 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, and the auxiliary button assembly includes a plurality of buttons; There are multiple inspection guidance interfaces, including: an inspection guidance interface for guiding the operation of pushing the joystick forward and rotating it clockwise for one circle, an inspection guidance interface for guiding the operation of twisting the joystick left and right, an inspection guidance interface for guiding the operation of pushing the throttle 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 flying object enters the pre-flight inspection phase of the control mechanism, the method further includes: When receiving a takeoff instruction, the display device is controlled to display a manual checklist guidance interface; the manual checklist guidance interface displays: multiple inspection items and their corresponding guidance controls, and a model display area; different inspection items are used to indicate different parts of the flying object that need to be inspected; When receiving the instruction generated by the guidance control being triggered, 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 corresponding prompt information.

7. The method according to claim 1, characterized in that After completing the inspection of the flying object in the pre-flight inspection stage of the control mechanism, the method further includes: Controlling the display device to display a dynamic inspection guide interface; the dynamic inspection guide interface displays: a start control for starting a dynamic inspection, and a model display area; When receiving the instruction generated by the triggering of the start control, the rotor of the flying object is controlled to rotate and the rotation data of the rotor is obtained in real time, and the flying object model displayed in the model display area is controlled to perform corresponding actions according to the rotation data.

8. The method according to claim 7, characterized in that Before controlling the rotor of the flying object to rotate, the method further includes: Controlling the display device to display a three-dimensional map interface of the environment in which the flying object is located, wherein a safety confirmation control is displayed in the three-dimensional map interface; Correspondingly, the step of controlling the rotation of the rotor of the flying body and acquiring the rotation data of the rotor in real time is executed when receiving the instruction generated by the triggering of the start control and the instruction generated by the triggering of the safety confirmation control.

9. A pre-flight inspection device, characterized in that: include: The guidance module is configured to: when the flying object is in the pre-flight inspection stage of the control mechanism, control the display device associated with the flying object to display the inspection guidance interface of the control mechanism; the inspection guidance interface displays the control guidance animation of the control mechanism and corresponding prompt information; A determination module is configured to: upon receiving response data fed back by the control mechanism being checked, determine 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; a switching module 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; The loop module is configured to: return to execute 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 according to the response data when the response data is received from the operating mechanism being inspected, until the current inspection guidance interface is the last inspection guidance interface.

10. An electronic device, characterized in that: The invention comprises a processor and a memory, wherein the memory stores machine executable instructions that can be executed by the processor, and the processor can execute the machine executable instructions to implement the method according to 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, the method according to any one of claims 1 to 8 is implemented.

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