CN114510006A - Remote testing method, device, equipment and storage medium of cockpit domain controller - Google Patents

Abstract

The present application discloses a remote testing method, device, device and storage medium for a cockpit domain controller. The method includes: displaying a target function display interface corresponding to the target function module in response to a simulated trigger operation for the target function module , wherein the target function display interface displays a plurality of function data information corresponding to the target function module in a preset format; in response to a trigger operation for the target function data information in the target function display interface, a control instruction corresponding to the target function data information is generated; Call the cockpit control interface to send the control command to the cockpit domain controller of the vehicle, and receive the control response information corresponding to the control command fed back by the cockpit domain controller; based on the control command and the control response information, generate the target corresponding to the target function data information Test data; display the target test data in the target function display interface; the present application can realize the simulated test of each functional module associated with the cockpit domain controller.

Description

Remote testing method, device, equipment and storage medium for cockpit domain controller

technical field

The present application relates to the technical field of simulation testing of vehicle functions, and in particular, to a remote testing method, device, device and storage medium of a cockpit domain controller.

Background technique

In the development process of cockpit software, as the main window for user interaction, many vehicle control and vehicle setting functions are realized through the large central control screen. Therefore, the cockpit software often needs to be debugged with many paired ECUs, such as Air conditioning controller, body controller (windows, lights and other functions), assisted driving controller, etc., each controller communicates with the cockpit controller through the CAN (Controller Area Network) protocol.

In the past development process of the cockpit domain controller, due to the lack of effective analog debugging methods, various signal mismatches and incorrect functional logic were prone to occur during the final vehicle function integration. Foreign simulation test equipment, such as CANoe, is very expensive, often requiring hundreds of thousands of RMB, which is difficult to popularize on a large scale. At the same time, since these equipments are designed for the whole vehicle, they are not very suitable for the simulation test scene of the cockpit controller.

SUMMARY OF THE INVENTION

In order to solve the above technical problems, the present application discloses a remote testing method for a cockpit domain controller, which can realize the simulation test of each functional module associated with the cockpit domain controller on the vehicle, and can visualize the test data of each functional module. display, and at a lower cost.

In order to achieve the above purpose of the invention, the present application provides a remote test method for a cockpit domain controller, which is applied to a remote control terminal, and the method includes:

In response to the simulated trigger operation for the target function module, a target function display interface corresponding to the target function module is displayed, wherein the target function display interface displays a plurality of function data corresponding to the target function module in a preset format information;

In response to a trigger operation for the target function data information in the target function display interface, a control instruction corresponding to the target function data information is generated;

calling the cockpit control interface to send the control command to the cockpit domain controller of the vehicle, and receive control response information corresponding to the control command fed back by the cockpit domain controller;

generating target test data corresponding to the target function data information based on the control instruction and the control response information;

The target test data is displayed in the target function display interface.

In some embodiments, before the displaying the target function display interface corresponding to the target function module in response to the simulated trigger operation for the target function module, the method further includes:

In response to the triggering operation for the plurality of vehicle function modules, acquiring the network database file corresponding to each vehicle function module;

Parsing each network database file to obtain node data information and message data information corresponding to each network database file, where the message data information includes the plurality of function data information;

Based on the data information of each node and the preset interface template, a module entry page document is generated, wherein the module entry interface corresponding to the module entry page document can display the module controls corresponding to each vehicle function module;

For each message data information, based on the corresponding relationship between the preset data signal type and the functional data information, determine the respective data display controls corresponding to each functional data information in the message data information from the preset display template , wherein the preset display template includes data display controls corresponding to each data signal type;

Acquiring respective data identifiers and initial display data corresponding to each of the functional data information;

For each function data information, load the data identification and the initial display data into the data display control corresponding to the function data information, and generate a function display page document of the corresponding function module;

The module entry page document and the function display page document corresponding to each function module are associated and stored.

In some embodiments, the displaying a target function display interface corresponding to the target function module in response to a simulated trigger operation for the target function module includes:

In response to the simulated triggering operation for the target module control in the module entry interface, determining a function display page document corresponding to the target function module, the target function module corresponding to the target module control;

Perform parsing and rendering processing on the function display page document, and display the target function display interface corresponding to the target function module.

In some embodiments, the invoking the cockpit control interface to send the control command to the cockpit domain controller of the vehicle, and receiving the control response information corresponding to the control command fed back by the cockpit domain controller, includes:

Encapsulating the control instruction to obtain a target signal group package corresponding to the target function data information;

calling the cockpit control interface to send the target signal group package to the cockpit domain controller, and receive a response information group package corresponding to the target signal group package fed back by the cockpit domain controller;

Parse the response information package to obtain control response information corresponding to the control instruction in the target signal package.

In some embodiments, the cockpit control interface and the cockpit domain controller perform data transmission based on a controller area network transmission channel or an Ethernet transmission channel.

In some embodiments, determining the target test data corresponding to the target function data information based on the control instruction and the control response information includes:

extracting configuration data corresponding to the target function data information from the control instruction;

Parsing the control response information to obtain response data corresponding to the target function data information;

The configuration data and the response data are determined as the target test data of the target function data information.

In some embodiments, after displaying the target test data in the target function display interface, the method further includes:

generating an update control instruction corresponding to the update configuration data based on the update configuration data corresponding to the configuration data obtained from the function display interface;

calling the cockpit control interface to send the update control instruction to the cockpit domain controller, and receive update control response information corresponding to the update control instruction fed back by the cockpit domain controller;

Parsing the update control response information to obtain update response data corresponding to the corresponding function data information;

The configuration data and the response data of the corresponding function data information in the target function display interface are respectively updated with the update configuration data and the update response data.

The application also provides a remote testing device for a cockpit domain controller, which is applied to a remote control terminal, and the device includes:

a first display module, configured to display a target function display interface corresponding to the target function module in response to a simulated trigger operation for the target function module, wherein the target function display interface displays the target function in a preset format Multiple functional data information corresponding to the module;

an instruction generation module, configured to generate a control instruction corresponding to the target function data information in response to a trigger operation for the target function data information in the target function display interface;

a first transceiver module, configured to call the cockpit control interface to send the control command to the cockpit domain controller of the vehicle, and receive control response information corresponding to the control command fed back by the cockpit domain controller;

a data generation module, configured to generate target test data corresponding to the target function data information based on the control instruction and the control response information;

The data display module is used to display the target test data in the target function display interface.

The present application also provides a remote testing device for a cockpit domain controller, the device includes a processor and a memory, and the memory stores at least one instruction or at least a piece of program, the at least one instruction or the at least one piece of program Loaded and executed by the processor to implement the remote testing method of the cockpit domain controller as described above.

The present application also provides a computer-readable storage medium, where the storage medium stores at least one instruction or at least one piece of program, and the at least one instruction or at least one piece of program is loaded and executed by a processor as described above Remote testing methods for cockpit domain controllers.

Implementing the embodiments of the present application has the following beneficial effects:

The remote testing method of the cockpit domain controller disclosed in the present application can realize the simulation test of each functional module associated with the cockpit domain controller on the vehicle, and can visualize the test data of each functional module, and the cost is low.

Description of drawings

In order to more clearly illustrate the remote testing method, device, device and storage medium of the cockpit domain controller described in the present application, the accompanying drawings required by the embodiments will be briefly introduced below. Obviously, the accompanying drawings in the following description These are just some embodiments of the present application. For those of ordinary skill in the art, other drawings can also be obtained based on these drawings without any creative effort.

1 is a schematic diagram of a remote testing system of a cockpit domain controller provided by an embodiment of the present application;

2 is a schematic flowchart of a configuration method of a test display interface provided by an embodiment of the present application;

3a is a schematic diagram of a display form of a display control provided by an embodiment of the present application;

3b is a schematic diagram of a module entry interface provided by an embodiment of the present application;

3c is a schematic diagram of a function display interface of an air conditioning module provided by an embodiment of the present application;

4 is a schematic flowchart of a method for determining a result of a first obstacle provided by an embodiment of the present application;

FIG. 5 is a schematic structural diagram of a remote testing device of a cockpit domain controller according to an embodiment of the present application;

FIG. 6 is a schematic structural diagram of an electronic device according to an embodiment of the present application.

Detailed ways

The technical solutions in the embodiments of the present application will be clearly and completely described below with reference to the drawings in the embodiments of the present application. Obviously, the described embodiments are only a part of the embodiments of the present application, but not all of the embodiments. Based on the embodiments in the present application, all other embodiments obtained by those of ordinary skill in the art without creative work shall fall within the protection scope of the present application.

It should be noted that the terms "first", "second", etc. in the description and claims of the present application and the above drawings are used to distinguish similar objects, and are not necessarily used to describe a specific sequence or sequence. It is to be understood that data so used may be interchanged under appropriate circumstances so that the embodiments of the application described herein can be practiced in sequences other than those illustrated or described herein. Furthermore, the terms "comprising" and "having" and any variations thereof, are intended to cover non-exclusive inclusion, for example, a process, method, system, product or server comprising a series of steps or units is not necessarily limited to those expressly listed Rather, those steps or units may include other steps or units not expressly listed or inherent to these processes, methods, products or devices.

The following describes the remote testing method of the cockpit domain controller of the present application with reference to FIG. 1, which can be applied to a remote control terminal. The remote control terminal includes but is not limited to a PC terminal, a mobile terminal, etc. Specifically, it can be a kind of remote control terminal. The application program, correspondingly, realizes the remote test of the cockpit domain controller through the information transmission between the remote control terminal and the cockpit domain controller, and can visualize the test data of each functional module, and the test cost is low.

Please refer to FIG. 1, which shows a schematic flowchart of a remote testing method for a cockpit domain controller provided by an embodiment of the present application. This specification provides the method operation steps as described in the embodiment or the flowchart, but is based on routines; Or non-creative work may involve more or fewer operational steps. The sequence of steps enumerated in the embodiment is only one of the execution sequences of many steps, and does not represent the only execution sequence. The remote testing method of the cockpit domain controller can be executed according to the method sequence shown in the embodiment or the accompanying drawings. Specifically, as shown in Figure 1, the method includes:

S101, in response to a simulated trigger operation for the target function module, display a target function display interface corresponding to the target function module, wherein the target function display interface displays a plurality of function data information corresponding to the target function module in a preset format.

It should be noted that, in this embodiment of the present application, the function module may be a function module corresponding to multiple functions in the vehicle on the trigger interface, and the target function module is a triggered function module among the multiple function modules.

Specifically, each function module corresponds to a function display interface; the function display interface can be pre-configured; correspondingly, each function module corresponds to a plurality of function data information; further, the function display interface can be used to display the corresponding Multiple function data information of the function module.

In an optional embodiment of the present application, if the functional module is an air conditioning module, its corresponding functional data information may include but not limited to air conditioning switch data information, air volume level data information, driver seat heating data information, circulation mode Data information and blowing mode data information, etc.

In the embodiment of the present application, the preset format may be a display format corresponding to the data type of each function data information in the function display interface and a display layout manner of the display format corresponding to each function data information.

In the embodiment of the present application, before displaying the target function display interface corresponding to the target function module in response to the simulated trigger operation for the target function module, it also includes the correlation of the test display interface of the application used for testing. configuration steps.

Specifically, as shown in FIG. 2 , which is a schematic flowchart of a configuration method for a test display interface provided by an embodiment of the present application; the specific steps are as follows:

S201 , in response to triggering operations for multiple vehicle function modules, acquire a network database file corresponding to each vehicle function module.

In this embodiment of the present application, the network database file may include, but is not limited to, a DBC file; specifically, the DBC file may represent a CAN database file.

Specifically, each vehicle function module corresponds to a DBC file; correspondingly, the application program used for testing in this application can identify the DBC file corresponding to each vehicle function.

In some embodiments of the present application, in response to a user's triggering operation on a plurality of vehicle function modules, respective DBC files corresponding to each vehicle function module are obtained respectively.

S202: Analyze each network database file to obtain node data information and message data information corresponding to each network database file, where the message data information includes the plurality of function data information.

In the embodiment of the present application, a preset algorithm is used to parse the DBC file to obtain node data information and message data information corresponding to the DBC file; wherein each message data information may include multiple functional data information.

The function data information may be the function data possessed by the corresponding vehicle function module.

S203, based on the data information of each node and a preset interface template, generate a module entry page document, wherein the module entry interface corresponding to the module entry page document can display module controls corresponding to each vehicle function module;

In this embodiment of the present application, the preset interface template may be a preset interface template capable of displaying multiple module controls.

In this embodiment of the present application, for each node data information, a module control corresponding to the node data information may be determined from a preset interface template.

Obtain the node identifier corresponding to each node data information; specifically, the node identifier may be the name of the node data information.

For each node data information, load the node identifier into the module control corresponding to the node data information, perform associated storage, and generate a module entry page document of the corresponding node data information.

S204, for each message data information, based on the preset corresponding relationship between the data signal type and the function data information, determine from the preset display template the respective data display controls corresponding to each function data information in the message data information, wherein , the preset display template includes data display controls corresponding to each data signal type.

In the embodiment of the present application, the data signal type corresponding to each function data information may be determined based on the corresponding relationship between the preset data signal type and the function data information corresponding to each packet data information.

Specifically, the preset data signal type may be predefined according to the function signal of the vehicle; exemplarily, may include but not limited to data type signal, option type signal, Boolean signal and wheel type signal;

Specifically, the data signal can be a data signal containing specific values, such as speed, air conditioner temperature and other information; the option signal can be a data signal with multiple selectable values, such as gear information, etc.; the Boolean signal can be a The data signal selected before the two states, such as the switch ON or OFF; the wheel type signal can be the data signal whose value can be increased or decreased, such as the temperature of the air conditioner.

In this embodiment of the present application, each of the defined data signal types may also be displayed in different display controls on the UI interface, and stored in the interface.

In some optional embodiments of the present application, the display form of the display controls of each data signal type on the UI interface may be as shown in FIG. 3a.

For each message data information, a data display control corresponding to each function data information in the message data information is determined from a preset display template, wherein the preset display template includes data display corresponding to each data signal type controls.

In this embodiment of the present application, the preset display template may be a preset template for displaying the data information of each function. Specifically, the data information of each function is displayed in the form of a data display control in the preset template; Correspondingly, in the preset template, the number of data display controls may be increased or deleted according to the amount of functional data information corresponding to each functional module.

Specifically, the preset display template includes data display controls corresponding to each data signal type; correspondingly, the data display control corresponding to the function data information can be determined from the preset interface according to the data signal type corresponding to the function data information.

S205, acquiring respective data identifiers and initial display data corresponding to each functional data information;

In this embodiment of the present application, the data identifier may be the name of the function data information; the initial display data may be user-defined default display data.

S206, for each function data information, load the data identification and the initial display data into the data display control corresponding to the function data information, and generate a function display page document of the corresponding function module;

In the embodiment of the present application, the data identification and initial display data of each function data information are loaded into the data display control corresponding to the function data information, and are stored in association, and the function display page document of the corresponding function module has been obtained.

S207, associate and store the module entry page document and the function display page document corresponding to each function module.

In the embodiment of the present application, the module controls corresponding to each function module in the module entry page document are associated and stored with the function display page document corresponding to each function module; so that subsequent responses to the module controls corresponding to the function modules can be performed. , find the function display page document corresponding to the function module.

In this embodiment of the present application, the module entry page document can be parsed in response to a triggering operation on the application, and the module entry interface can be displayed.

Specifically, the triggering operation may be a user's click operation.

In some optional embodiments of the present application, as shown in FIG. 3 b , it is a schematic diagram of a module entry interface provided by an embodiment of the present application.

In some optional embodiments of the present application, as shown in FIG. 3c, it is a schematic diagram of a function display interface of an air conditioner module provided by an embodiment of the present application; correspondingly, in this embodiment, the air conditioner module includes an air conditioner switch , Refrigeration switch, front defrost, equivalent level, blower mode, circulation mode and driver seat heating and other functional data information.

S102, in response to a trigger operation for the target function data information in the target function display interface, generate a control instruction corresponding to the target function data information;

In this embodiment of the present application, the trigger operation may include, but is not limited to, a user's click operation, an editing operation, and the like.

Specifically, a corresponding control instruction is generated according to the operation result of the click operation and the operation result of the editing operation.

S103, call the cockpit control interface to send the control command to the cockpit domain controller of the vehicle, and receive the control response information corresponding to the control command fed back by the cockpit domain controller;

In the embodiment of the present application, the cockpit control interface may be a transmission interface for data communication between the application program used for the simulation test and the cockpit domain controller; correspondingly, the control instruction is sent to the cockpit domain controller through the cockpit control interface, So that the cockpit domain controller executes the response according to the received control instruction, and feeds back the execution response result to the application that issued the control instruction.

In this embodiment of the present application, the control response information may be an execution response result made by the cockpit domain controller based on the control instruction.

In some embodiments of the present application, calling the cockpit control interface to send a control command to the cockpit domain controller of the vehicle, and receiving control response information corresponding to the control command fed back by the cockpit domain controller, may specifically include the following steps:

The control instruction is encapsulated to obtain a target signal package corresponding to the target function data information.

In the embodiment of the present application, the sent control command can be encapsulated to obtain the target signal package corresponding to the control command; correspondingly, the target signal package is sent to the cockpit domain controller through the cockpit control interface.

calling the cockpit control interface to send the target signal group package to the cockpit domain controller, and receive a response information group package corresponding to the target signal group package fed back by the cockpit domain controller;

In this embodiment of the present application, the response information package may be an execution response result made by the cockpit domain controller based on the control instruction, and the packaged information package; correspondingly, when the cockpit domain controller receives the target signal package Afterwards, the target signal packet is parsed and processed to obtain the relevant information of the control command, such as the address and other information; and the response is made according to the relevant information of the control information, and the response structure is fed back to the address where the control command is sent.

Parse the response information package to obtain control response information corresponding to the control instruction in the target signal package.

In the embodiment of the present application, after receiving the response information packet, the response information packet is parsed to obtain the execution response result corresponding to the response information packet and information such as the terminal that issued the response execution result; correspondingly, The execution response result obtained by the analysis may be determined as control response information corresponding to the control instruction.

In some embodiments of the present application, the cockpit control interface and the cockpit domain controller may perform data transmission through a controller network transmission channel or perform data transmission based on an Ethernet transmission channel.

Specifically, the controller network transmission channel may be CAN communication; exemplarily, it may be a signal transmission channel based on a CAN box.

Specifically, the Ethernet transmission channel may be an Ethernet socket signal transmission channel.

S104, based on the control instruction and the control response information, generate target test data corresponding to the target function data information;

In some embodiments of the present application, the configuration data corresponding to the control instruction and the response data corresponding to the control response information may be determined as target test data; correspondingly, the target test data may be when the application program tests the cockpit domain controller , the configuration data received and the response data fed back by the cockpit domain controller.

Specifically, the configuration data corresponding to the target function data information is extracted from the control instruction.

In the embodiment of the present application, each control instruction corresponds to a piece of configuration data; preferably, the control instruction may be generated based on the configuration data corresponding to the function data information.

Parsing the control response information to obtain response data corresponding to the target function data information;

In this embodiment of the present application, the response data may be result data corresponding to an execution response result made by the cockpit domain controller based on the control instruction; correspondingly, the response data in the information may be extracted from the control response information.

The configuration data and the response data are determined as the target test data of the target function data information.

S105, display the target test data in the target function display interface;

In this embodiment of the present application, the target function display interface may display test data corresponding to each function data information in the target function module.

In a preferred embodiment of the present application, take a function data information in the air conditioning function module as an example, for example, the temperature adjustment data information for the main driver side; the function display page can be configured for the main driver side heating temperature and main driver side. The actual response temperature is displayed; so that the user can obtain the feasibility of the application for testing based on the target test data.

In some embodiments of the present application, during the testing process, if the test data displayed in the target function display interface needs to be updated or processed, the method in FIG. 4 can be used to update.

Specifically, as shown in FIG. 4 , it is a schematic flowchart of a data update method provided by an embodiment of the present application, which specifically includes the following steps.

S401, based on the update configuration data corresponding to the configuration data obtained on the function display interface, generate an update control instruction corresponding to the update configuration data;

In this embodiment of the present application, the updated configuration data may be changed actively by the user, or may be changed automatically according to a preset rule; correspondingly, the updated configuration data corresponds to the configuration data.

S402, calling the cockpit control interface to send the update control instruction to the cockpit domain controller, and receive the update control response information corresponding to the update control instruction fed back by the cockpit domain controller;

In the embodiment of the present application, the update control instruction is sent to the cockpit domain controller through the cockpit control interface, so that the cockpit domain controller responds and executes according to the received update control instruction, and feeds back the execution response result made to the cockpit domain controller. An application that issues update control instructions.

In this embodiment of the present application, the update control response information may be an execution response result made by the cockpit domain controller based on the update control instruction.

Specifically, in the present application, the control instruction may be encapsulated and then sent to the cockpit domain controller through the cockpit control interface.

S403, parse the update control response information to obtain update response data corresponding to the corresponding function data information;

In this embodiment of the present application, the update response data may be extracted from the update control response information.

S404, the configuration data and the response data of the corresponding function data information in the target function display interface are respectively updated by updating the configuration data and updating the response data.

In this embodiment of the present application, the configuration data of the corresponding function data information is updated with the update configuration data; the response data corresponding to the function data information is updated with the update response data.

It can be seen from the above-mentioned embodiments of the remote testing method, device, device, and storage medium for a cockpit domain controller provided by the present application that, in response to a simulated trigger operation for a target functional module, the embodiment of the present application displays a display corresponding to the target functional module. A target function display interface, wherein the target function display interface displays a plurality of function data information corresponding to the target function module in a preset format; in response to a trigger operation for the target function data information in the target function display interface , generate the control command corresponding to the target function data information; call the cockpit control interface to send the control command to the cockpit domain controller of the vehicle, and receive the control command corresponding to the control command fed back by the cockpit domain controller response information; generate target test data corresponding to the target function data information based on the control instruction and the control response information; display the target test data in the target function display interface; use the The technical solution can realize the simulation test of each functional module associated with the cockpit domain controller on the vehicle, and can visualize the test data of each functional module, and the cost is low.

An embodiment of the present application further provides a remote testing device for a cockpit domain controller, as shown in FIG. 5 , which is a schematic structural diagram of a remote testing device for a cockpit domain controller provided in an embodiment of the present application; , the device includes:

The display module 510 is configured to display a target function display interface corresponding to the target function module in response to a simulated trigger operation for the target function module, wherein the target function display interface displays the target function module in a preset format Corresponding multiple functional data information;

an instruction generation module 520, configured to generate a control instruction corresponding to the target function data information in response to a trigger operation for the target function data information in the target function display interface;

a first transceiver module 530, configured to call the cockpit control interface to send the control command to the cockpit domain controller of the vehicle, and receive control response information corresponding to the control command fed back by the cockpit domain controller;

a data generation module 540, configured to generate target test data corresponding to the target function data information based on the control instruction and the control response information;

The data display module 550 is configured to display the target test data in the target function display interface.

In the embodiment of this application, it also includes:

a first obtaining module, configured to obtain the network database file corresponding to each vehicle function module in response to a trigger operation for a plurality of vehicle function modules;

a first parsing module, configured to parse each network database file to obtain node data information and message data information corresponding to each network database file, where the message data information includes the plurality of function data information;

a first generation module, configured to generate a module entry page document based on the data information of each node and a preset interface template, wherein the module entry interface corresponding to the module entry page document can display module controls corresponding to each vehicle function module;

The determining module is configured to, for each message data information, determine the respective function data information in the message data information from the preset display template based on the corresponding relationship between the preset data signal type and the functional data information A corresponding data display control, wherein the preset display template includes a data display control corresponding to each data signal type;

a second acquisition module, configured to acquire the respective data identifiers and initial display data corresponding to the respective functional data information;

The second generation module is configured to, for each function data information, load the data identification and the initial display data into the data display control corresponding to the function data information, and generate a function display page document of the corresponding function module;

The storage module is configured to associate and store the module entry page document and the function display page document corresponding to each function module.

In this embodiment of the present application, the display module 510 includes:

a determining unit, configured to determine a function display page document corresponding to the target function module in response to a simulated trigger operation for the target module control in the module entry interface, the target function module corresponding to the target module control;

A display unit, configured to perform parsing and rendering processing on the function display page document, and display a target function display interface corresponding to the target function module.

In this embodiment of the present application, the first transceiver module 530 includes:

an encapsulation processing unit, configured to encapsulate the control instruction to obtain a target signal package corresponding to the target function data information;

an information transceiver unit, configured to call the cockpit control interface to send the target signal group package to the cockpit domain controller, and receive a response information group corresponding to the target signal group package fed back by the cockpit domain controller Bag;

A first parsing unit, configured to parse the response information packet to obtain control response information corresponding to the control instruction in the target signal packet.

In this embodiment of the present application, the data generation module 540 includes:

an extraction unit, configured to extract configuration data corresponding to the target function data information from the control instruction;

a second parsing unit, configured to parse the control response information to obtain response data corresponding to the target function data information;

A determination unit, configured to determine the configuration data and the response data as target test data of the target function data information.

In the embodiment of this application, it also includes:

an update instruction generation module, configured to generate an update control instruction corresponding to the update configuration data based on the update configuration data corresponding to the configuration data obtained from the function display interface;

a second transceiver module, configured to call the cockpit control interface to send the update control instruction to the cockpit domain controller, and receive update control response information corresponding to the update control instruction fed back by the cockpit domain controller ;

a second parsing module, configured to parse the update control response information to obtain update response data corresponding to the corresponding function data information;

A data update module, configured to update the configuration data and the response data of the corresponding function data information in the target function display interface with the update configuration data and the update response data, respectively.

It should be noted that the apparatus and method embodiments in the apparatus embodiments are based on the same inventive concept.

An embodiment of the present application provides a remote testing device for a cockpit domain controller. The device includes a processor and a memory. The memory stores at least one instruction or at least one program, and the at least one instruction or at least one program is loaded and executed by the processor to The remote testing method of the cockpit domain controller according to the above method embodiment is implemented.

Further, FIG. 6 shows a schematic diagram of the hardware structure of an electronic device for implementing the remote testing method for the cockpit domain controller provided by the embodiment of the present application, and the electronic device may participate in forming or include all the methods in the embodiment of the present application. Provides a remote test setup for the cockpit domain controller. As shown in FIG. 6, the electronic device 60 may include one or more (shown as 602a, 602b, . processing means of a logic device FPGA or the like), a memory 604 for storing data, and a transmission means 606 for communication functions. In addition, may also include: display, input/output interface (I/O interface), universal serial bus (USB) port (may be included as one of the ports of the I/O interface), network interface, power supply and/or camera. Those of ordinary skill in the art can understand that the structure shown in FIG. 6 is only a schematic diagram, which does not limit the structure of the above electronic device. For example, electronic device 60 may also include more or fewer components than shown in FIG. 6 , or have a different configuration than that shown in FIG. 6 .

It should be noted that the one or more processors 602 and/or other data processing circuits described above may generally be referred to herein as "data processing circuits." The data processing circuit may be embodied in whole or in part as software, hardware, firmware or any other combination. Furthermore, the data processing circuitry may be a single, stand-alone processing module, or incorporated in whole or in part into any of the other elements in the electronic device 60 (or mobile device). As referred to in the embodiments of the present application, the data processing circuit acts as a kind of processor control (eg, selection of a variable resistance termination path connected to an interface).

The memory 604 can be used to store software programs and modules of the application software, such as the program instruction/data storage device corresponding to the remote testing method of the cockpit domain controller described in the embodiments of the present application, the processor 602 executes the program stored in the memory 604 by running The software programs and modules are used to perform various functional applications and data processing, that is, to implement the above-mentioned remote testing method for a cockpit domain controller. Memory 604 may include high-speed random access memory, and may also include non-volatile memory, such as one or more magnetic storage devices, flash memory, or other non-volatile solid-state memory. In some examples, memory 604 may further include memory located remotely from processor 602, which may be connected to electronic device 60 through a network. Examples of such networks include, but are not limited to, the Internet, an intranet, a local area network, a mobile communication network, and combinations thereof.

Transmission means 606 is used to receive or transmit data via a network. The specific example of the above-mentioned network may include a wireless network provided by the communication provider of the electronic device 60 . In one example, the transmission device 606 includes a network adapter (Network Interface Controller, NIC), which can be connected to other network devices through the base station so as to communicate with the Internet. In one embodiment, the transmission device 606 may be a radio frequency (Radio Frequency, RF) module, which is used to communicate with the Internet in a wireless manner.

The display may be, for example, a touch screen-style liquid crystal display (LCD) that enables a user to interact with the user interface of the electronic device 60 (or mobile device).

Embodiments of the present application further provide a computer-readable storage medium, which can be set in an electronic device to store at least one item related to a remote testing method for implementing a cockpit domain controller in the method embodiment An instruction or at least one piece of program, the at least one instruction or at least one piece of program is loaded and executed by the processor to implement the remote testing method for a cockpit domain controller provided by the above method embodiments.

Optionally, in this embodiment, the above-mentioned storage medium may be located in at least one network server among multiple network servers of a computer network. Optionally, in this embodiment, the above-mentioned storage medium may include but is not limited to: a U disk, a read-only memory (ROM, Read-Only Memory), a random access memory (RAM, Random Access Memory), a mobile hard disk, a magnetic Various media that can store program codes, such as discs or optical discs.

It should be noted that: the above-mentioned order of the embodiments of the present application is only for description, and does not represent the advantages and disadvantages of the embodiments. And the above describes specific embodiments of the present application. Other embodiments are within the scope of the appended claims. In some cases, the actions or steps recited in the claims can be performed in an order different from that in the embodiments and still achieve desirable results. Additionally, the processes depicted in the figures do not necessarily require the particular order shown, or sequential order, to achieve desirable results. In some embodiments, multitasking and parallel processing are also possible or may be advantageous.

According to one aspect of the present application, there is provided a computer program product or computer program comprising computer instructions stored in a computer readable storage medium. The processor of the computer device reads the computer instructions from the computer-readable storage medium, and the processor executes the computer instructions to cause the computer device to perform the methods provided in the various optional implementations described above.

Each embodiment in this application is described in a progressive manner, and the same and similar parts between the various embodiments may be referred to each other, and each embodiment focuses on the differences from other embodiments. In particular, for the apparatus and electronic device embodiments, since they are basically similar to the method embodiments, the description is relatively simple, and for related parts, refer to the partial descriptions of the method embodiments.

Those of ordinary skill in the art can understand that all or part of the steps of implementing the above embodiments can be completed by hardware, or can be completed by instructing relevant hardware through a program, and the program can be stored in a computer-readable storage medium. The storage medium mentioned may be a read-only memory, a magnetic disk or an optical disk, etc.

The above are only preferred embodiments of the present application, and are not intended to limit the present application. Any modifications, equivalent replacements, improvements, etc. made within the spirit and principles of the present application shall be included in the protection of the present application. within the range.

Claims (10)

1. A remote testing method of a cockpit area controller is applied to a remote control terminal, and is characterized by comprising the following steps:

responding to a simulation trigger operation aiming at a target function module, and displaying a target function display interface corresponding to the target function module, wherein a plurality of pieces of function data information corresponding to the target function module are displayed in a preset format in the target function display interface;

responding to a trigger operation aiming at target function data information in the target function display interface, and generating a control instruction corresponding to the target function data information;

calling a cabin control interface to send the control instruction to a cabin domain controller of the vehicle and receive control response information corresponding to the control instruction fed back by the cabin domain controller;

generating target test data corresponding to the target function data information based on the control instruction and the control response information;

and displaying the target test data in the target function display interface.

2. The remote testing method of a cockpit domain controller of claim 1, wherein prior to said displaying a target function presentation interface corresponding to a target function module in response to a simulated triggering operation for said target function module, further comprising:

responding to the triggering operation aiming at the plurality of vehicle function modules, and acquiring network database files corresponding to the vehicle function modules;

analyzing each network database file to obtain node data information and message data information corresponding to each network database file, wherein the message data information comprises the plurality of functional data information;

generating a module entry page document based on the data information of each node and a preset interface template, wherein the module entry interface corresponding to the module entry page document can display the module control corresponding to each vehicle function module;

for each message data information, determining a data display control corresponding to each functional data information in the message data information from a preset display template based on a corresponding relation between a preset data signal type and the functional data information, wherein the preset display template comprises the data display control corresponding to each data signal type;

acquiring data identification and initial display data corresponding to each piece of functional data information;

for each piece of functional data information, loading the data identifier and the initial display data into a data display control corresponding to the functional data information, and generating a functional display page document of a corresponding functional module;

and performing associated storage on the module entry page document and the function display page documents corresponding to the function modules respectively.

3. The remote testing method of a cockpit domain controller of claim 2 wherein said displaying a target function presentation interface corresponding to a target function module in response to a simulated triggering operation for said target function module comprises:

responding to a simulation trigger operation aiming at a target module control in the module inlet interface, and determining a function display page document corresponding to the target function module, wherein the target function module corresponds to the target module control;

and analyzing and rendering the function display page document, and displaying a target function display interface corresponding to the target function module.

4. The remote testing method of the cockpit domain controller of claim 1, wherein said invoking a cockpit control interface to send the control command to a cockpit domain controller of a vehicle and receive control response information corresponding to the control command fed back by the cockpit domain controller comprises:

packaging the control instruction to obtain a target signal package corresponding to the target function data information;

calling a cockpit control interface to send the target signal package to the cockpit area controller and receive a response information package corresponding to the target signal package fed back by the cockpit area controller;

and analyzing the response information packet to obtain control response information corresponding to the control instruction in the target signal packet.

5. The remote testing method of a cockpit domain controller of claim 1 where said cockpit control interface and said cockpit domain controller are data-transmitting based on a controller area network transmission channel or an ethernet transmission channel.

6. The remote testing method of the cockpit domain controller of claim 1, wherein said generating target test data corresponding to said target function data information based on said control command and control response information comprises:

extracting configuration data corresponding to the target function data information from the control instruction;

analyzing the control response information to obtain response data corresponding to the target function data information;

and determining the configuration data and the response data as target test data of the target function data information.

7. The remote testing method of a cockpit domain controller of claim 6, further comprising, after presenting said target test data in said target function presentation interface:

generating an update control instruction corresponding to the update configuration data based on the update configuration data corresponding to the configuration data acquired by the function display interface;

calling the cockpit control interface to send the updated control instruction to a cockpit area controller, and receiving updated control response information corresponding to the updated control instruction and fed back by the cockpit area controller;

analyzing the updating control response information to obtain updating response data corresponding to the corresponding functional data information;

and respectively updating the configuration data and the response data of the corresponding function data information in the target function display interface according to the updated configuration data and the updated response data.

8. A remote testing device of a cockpit area controller is applied to a remote control terminal, and is characterized by comprising:

the display module is used for responding to the simulation trigger operation aiming at the target function module and displaying a target function display interface corresponding to the target function module, wherein a plurality of pieces of function data information corresponding to the target function module are displayed in the target function display interface in a preset format;

the instruction generating module is used for responding to the trigger operation aiming at the target function data information in the target function display interface and generating a control instruction corresponding to the target function data information;

the first transceiving module is used for calling a cabin control interface so as to send the control instruction to a cabin domain controller of a vehicle and receive control response information corresponding to the control instruction fed back by the cabin domain controller;

the data generation module is used for generating target test data corresponding to the target function data information based on the control instruction and the control response information;

and the data display module is used for displaying the target test data in the target function display interface.

9. A remote test apparatus for a cockpit domain controller, the apparatus comprising a processor and a memory, the memory having stored therein at least one instruction or at least one program, the at least one instruction or the at least one program being loaded and executed by the processor to implement the remote test method for a cockpit domain controller according to any of claims 1 to 7.

10. A computer-readable storage medium, characterized in that said storage medium has stored therein at least one instruction or at least one program, which is loaded by a processor and executes a method of remote testing of a cockpit domain controller according to any of claims 1 to 7.

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