CN115857859A - Debugging method and device of element module, electronic equipment and storage medium - Google Patents
Debugging method and device of element module, electronic equipment and storage medium Download PDFInfo
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Abstract
The embodiment of the application discloses a debugging method and device of an element module, electronic equipment and a storage medium, and is applicable to the fields of flight simulation, airplane control panel design technology and the like. The method comprises the following steps: acquiring first element information and first hardware driving data corresponding to each first element module installed on an aircraft panel base, wherein each first element module is installed on the aircraft panel base according to a preset debugging scheme; transmitting the information of each first element and the driving data of each first hardware to an upper computer; receiving first display data which are sent by an upper computer and correspond to at least one first display element module respectively; for each first display element module, corresponding first display data is sent to the first display element module. By adopting the embodiment of the application, the element module is arranged on the reusable airplane panel base according to the preset debugging scheme, so that the airplane panel base is quickly reconfigurable, the utilization rate of the airplane panel base is improved, and the cost is reduced.
Description
Technical Field
The present application relates to the field of flight simulation, aircraft control panel design technology, and the like, and in particular, to a method and an apparatus for debugging an element module, an electronic device, and a storage medium.
Background
At present, in the technical field of design of aircraft control panels, designers generally perform design evaluation on the aircraft control panels first and perform post-production test and use. In order to ensure reasonable layout of the control panel of the airplane and meet the actual use requirements of pilots, a large amount of comparison design and evaluation verification are required. In such a workflow, it is often necessary to modify the design of the control panel several times according to the use experience of the pilot. Since the modification process involves many steps such as redesign, production investment, etc., a lot of resources are consumed, and it is difficult to ensure the validity of the modification. For example, if the pilot makes a new feedback during the re-design of production, the existing modification work is to be performed again; or the safety and convenience of the pilot operation can not be met after the design is reproduced, and the design needs to be reproduced.
In order to avoid the situation of resource waste, at present, a digital airplane control panel design scheme is selected, a virtual airplane control panel human-computer interaction interface is displayed on a touch screen, and the virtual airplane control panel human-computer interaction interface can be modified at any time, so that the design and production cost is greatly reduced.
However, this method still has a great problem: firstly, a digital control panel lacks real physical feedback, the hand feeling of various elements during operation cannot be simulated, and a pilot hardly experiences real operation feeling; secondly, the digital control panel can only transmit some basic operation and display signals through programs, but the real control panel often involves many complex data protocols and physical signals, which still cannot be simulated by the digital control panel.
Therefore, how to improve the design efficiency of the aircraft control panel and reduce the waste of resources becomes a problem to be solved urgently.
Disclosure of Invention
The embodiment of the application provides a debugging method and device of an element module, electronic equipment and a storage medium.
In a first aspect, an embodiment of the present application provides a method for debugging a component module, which is applied to an aircraft panel base, and the method includes:
acquiring first element information and first hardware driving data corresponding to each first element module installed on the aircraft panel base, wherein each first element module is installed on the reusable aircraft panel base according to a preset debugging scheme;
transmitting the information of each first element and the drive data of each first hardware to an upper computer;
receiving first display data which are sent by the upper computer and correspond to at least one first display element module respectively, wherein any one first display element module is one element module in each first element module, and any one first display data is determined by the upper computer based on each first element information and each first hardware driving data;
and for each first display element module, sending the corresponding first display data to the first display element module so that the first display element module performs data display according to the first display data.
In some possible embodiments, the method further comprises:
acquiring second element information and second hardware driving data corresponding to each second element module installed on the aircraft panel base according to the adjusted debugging scheme under the condition that the debugging scheme is adjusted;
transmitting the information of each second element and the driving data of each second hardware to an upper computer;
receiving at least one piece of second display data which is sent by the upper computer and aims at least one second display element module, wherein any one second display element module is one element module in each second element module, and any one piece of second display data is determined by the upper computer based on each piece of second element information and each piece of second hardware driving data;
and for each second display element module, sending the corresponding second display data to the second display element module so that the second display element module performs data display according to the second display data.
In some possible embodiments, each of the first component modules includes at least one operating component module, and the method further includes:
for each operating element module, acquiring operating data of a target object aiming at the operating element module;
sending operation data corresponding to each operation element module to the upper computer;
and receiving third display data which is sent by the upper computer and determined based on the operation data, so that the first display element module corresponding to the third display data displays data according to the third display data.
In some possible embodiments, the sending, to the upper computer, operation data corresponding to each operating element module includes:
and sending the operation data corresponding to each operation element module to the upper computer according to a preset data transmission protocol between the aircraft panel base and the upper computer.
In some possible embodiments, the aircraft panel base includes a housing, a standardized interface slot, a data bus and a power bus corresponding to the standardized interface slot, a chip, a power bus, a data transmission unit, and a network communication unit.
In some possible embodiments, for each of the first component modules, the first component module is connected to the standardized interface slot of the aircraft panel base by a standardized plug at the bottom of the first component module.
In a second aspect, an embodiment of the present application provides a debugging apparatus for a component module, including:
the first acquisition module is used for acquiring first element information and first hardware driving data which correspond to each first element module installed on the aircraft panel base, wherein each first element module is installed on the reusable aircraft panel base according to a preset debugging scheme;
the first transmission module is used for transmitting the information of each first element and the drive data of each first hardware to the upper computer;
a first receiving module, configured to receive first display data, which is sent by the upper computer and corresponds to at least one first display element module, where any one of the first display element modules is one of the first element modules, and any one of the first display data is determined by the upper computer based on the first element information and the first hardware driving data;
and a first sending module, configured to send, for each first display element module, the corresponding first display data to the first display element module, so that the first display element module performs data display according to the first display data.
In a third aspect, an embodiment of the present application provides an electronic device, including a processor and a memory, where the processor and the memory are connected to each other;
the memory is used for storing computer programs;
the processor is configured to perform the method provided by the first aspect when the computer program is called.
In a fourth aspect, the present application provides a computer-readable storage medium, where a computer program is stored, where the computer program is executed by a processor to implement the method provided in the first aspect.
In a fifth aspect, embodiments of the present application provide a computer program product or a computer program comprising computer instructions stored in a computer-readable storage medium. The processor of the electronic 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 method provided by the first aspect.
In the embodiment of the application, each first element module is installed on a reusable airplane panel base according to a preset debugging scheme, then, first element information and first hardware driving data corresponding to each first element module are obtained through the airplane panel base, the first element information and the first hardware driving data are transmitted to an upper computer, the upper computer determines first display data corresponding to at least one first display element module based on the first element information and the first hardware driving data, and after the airplane panel base receives the first display data corresponding to each first display element module sent by the upper computer, the airplane panel base sends the corresponding first display data to each first display element module, so that each first display element module performs data display according to the first display data. By adopting the mode, each element module is arranged on the reusable airplane panel base according to the preset debugging scheme, so that the airplane panel base realizes the quick reconfigurable function, the utilization rate of the airplane panel base is improved, the resource waste is reduced, the cost is reduced, and the physical element module has real physical feedback and improves the operation experience of pilots compared with the traditional digital control panel.
Drawings
In order to more clearly illustrate the technical solutions in the embodiments of the present application, the drawings needed to be used in the embodiments will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments of the present application, and it is obvious for those skilled in the art to obtain other drawings without creative efforts.
Fig. 1 is a schematic flowchart of a debugging method for a component module according to an embodiment of the present application;
fig. 2 is a schematic flowchart of another debugging method for a component module according to an embodiment of the present disclosure;
FIG. 3 is a schematic diagram illustrating a connection relationship between a component module and a panel base according to an embodiment of the present disclosure;
fig. 4 is a schematic diagram of a connection relationship between an element module, a panel base and an upper computer according to an embodiment of the present disclosure;
fig. 5 is a schematic structural diagram of a debugging apparatus of an element module according to an embodiment of the present application;
fig. 6 is a schematic structural diagram of an electronic device provided in an embodiment of the present application.
Detailed Description
The technical solutions in the embodiments of the present application will be described clearly and completely with reference to the drawings in the embodiments of the present application, and it is obvious that the described embodiments are only some embodiments of the present application, and not all embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present application.
Referring to fig. 1, fig. 1 is a schematic flowchart of a debugging method of an element module according to an embodiment of the present disclosure. As shown in fig. 1, a debugging method of an element module provided in an embodiment of the present application may include the following steps:
step S101, acquiring first element information and first hardware driving data corresponding to each first element module installed on the aircraft panel base, wherein each first element module is installed on the reusable aircraft panel base according to a preset debugging scheme;
step S102, transmitting the information of each first element and the drive data of each first hardware to an upper computer;
step S103, receiving first display data which is sent by the upper computer and corresponds to at least one first display element module respectively, wherein any one first display element module is one element module in each first element module, and any one first display data is determined by the upper computer based on each first element information and each first hardware driving data;
step S104, for each of the first display element modules, sending the corresponding first display data to the first display element module, so that the first display element module performs data display according to the first display data.
In an optional embodiment, the aircraft panel base comprises a shell, a standardized interface slot, a data bus and a power bus corresponding to the standardized interface slot, a chip, a power bus, a data transmission unit and a network communication unit.
Optionally, the aircraft panel base may also be referred to as an aircraft control panel, a panel base, and the like, and the embodiment of the present application is not limited in any way, and the aircraft panel base is composed of a shell, a standardized interface slot (may also be referred to as a standardized slot) distributed in a matrix form in an indefinite number, a chip, a power bus, a data transmission unit, a network communication unit, data and a power bus required by the standardized interface slot, and the like. The standardized interface slot may be an existing standard interface, for example, a Universal Serial Bus (USB) or a Type-C (USB interface profile standard) interface, or a customized standardized interface slot. The aircraft panel base can be connected with each component module through a standardized interface slot, supplies power for the component module and performs data interaction with the component module.
For any one aircraft panel base, according to the difference of the number of the standardized interface slots fixed on the aircraft panel base, a plurality of different types of element modules (no more than the number of the interface slots) can be installed, including various operation element modules and display element modules. Meanwhile, the number, the types, the positions and the like of the element modules can be rapidly adjusted according to modification requirements (namely debugging schemes), due to the rapid characteristic of the airplane panel base, the airplane panel base has the characteristic of repeated use, and finally, the mask module without the functional elements is used for filling blank areas on the panel base, so that a set of rapid and reconfigurable operation panel is formed. That is to say, use this aircraft panel base, need not to carry out die sinking production and complicated circuit wiring work, only need according to the plug component module at will of debugging scheme on panel base, great improvement aircraft panel base's design development efficiency.
For any one component module (also referred to as a component), each component module has a standardized plug corresponding to the base of the aircraft panel at the bottom end and a functional area at the top end. According to different element function types, the device can be divided into an operation element module (also referred to as an operation element) and a display element module (also referred to as a display element), wherein the operation element module can include element modules such as buttons and knobs, and the display element module can include element modules such as a nixie tube or a liquid crystal display.
The component module is a rectangular cube with fixed height, and the area of the front surface is equal to the area of one or a plurality of standardized interface slots. The main circuit comprises a chip, a power bus, a data storage module, a data transmission unit, a data transmission interface bus and the like. The standardized plug of component module bottom corresponds with the standardized interface slot of aircraft panel base for standardized plug and standardized interface slot can be connected fixedly, make the component module can install in aircraft panel base. The data storage module of the component module is responsible for storing information (i.e. component information) such as component module type, module identification code, etc. The program recorded in the chip of the component module is responsible for reading the information of the data storage module, optionally, if the component module is an acquisition function module, the chip is responsible for the signal acquisition function of the component module; after the component module is installed, the program driving data transmission unit burned in the chip of the component module transmits data to the aircraft panel base and receives data returned by the aircraft panel base, and optionally, if the component module is a display component module, the program driving the display component module to display data according to the data returned by the aircraft panel base.
The aircraft panel base and the element module are described in detail above, and the debugging process of the element module is described in detail below, and the specific steps are as follows:
installing each first element module on the plane panel base according to a preset debugging scheme, wherein the preset debugging scheme comprises the specific number of the first element modules, the function types of the first element modules, the specific positions of the first element modules on the plane panel base and the like.
After each first element module is installed according to the debugging scheme, a program recorded in a chip of the aircraft panel base can drive a data transmission unit of the aircraft panel base to perform data transmission with each first element module, and first element information and first hardware driving data corresponding to each first element module are obtained, wherein the first element information comprises the number of the first element modules installed on the aircraft panel base and the function types of the first element modules, and the first hardware driving data is related hardware information corresponding to each first element module.
Optionally, each first element module includes at least one first display element module, that is, each first element module includes at least one first display element module having a display function. The airplane panel base transmits the acquired first element information and the acquired first hardware driving data to the upper computer. And after receiving the first element information and the first hardware driving data, the upper computer performs data processing based on the received first element information and the first hardware driving data to determine first display data corresponding to each first display element module.
And then, the upper computer transmits the determined first display data corresponding to each first display element module back to the plane panel base. After receiving the first display data corresponding to each first display element module, the aircraft panel base sends the corresponding first display data to each first display element module, and for each first display element module, the first display data is used for the first display element module to perform data display according to the first display data, for example, if the first display element module is a nixie tube used for displaying a target height, when the nixie tube receives the first display data (for example, 10000), the nixie tube displays 10000 according to the first display data.
Through this application embodiment, through using standardized component module, can reconstruct aircraft panel base fast, need not to carry out die sinking production and complicated circuit wiring work, only need according to the plug component module of debugging scheme at will on aircraft panel base, can modify according to the debugging scheme, great improvement aircraft panel base's design development efficiency, greatly reduced the wasting of resources, development cost is reduced, and, compare in digital control panel design method, because the component module is specific in kind, can provide real physical feedback, it is more true on the sense organ, user's operation experience has been improved.
In an optional embodiment, the method further includes:
acquiring second element information and second hardware driving data corresponding to each second element module installed on the aircraft panel base according to the adjusted debugging scheme under the condition that the debugging scheme is adjusted;
transmitting the information of each second element and the drive data of each second hardware to an upper computer;
receiving at least one piece of second display data which is sent by the upper computer and aims at least one second display element module, wherein any one second display element module is one element module in each second element module, and any one piece of second display data is determined by the upper computer based on each piece of second element information and each piece of second hardware driving data;
and for each second display element module, sending the corresponding second display data to the second display element module so that the second display element module performs data display according to the second display data.
Optionally, in practical applications, the debugging scheme often needs to be modified many times to design an aircraft panel base meeting requirements, and each second element module is installed on the aircraft panel base according to the adjusted debugging scheme under the condition that the debugging scheme is adjusted, where the adjusted debugging scheme includes the specific number of the second element modules, the functional types of the second element modules, the specific positions of the second element modules on the aircraft panel base, and the like.
After each second element module is installed according to the adjusted debugging scheme, the program recorded in the chip of the aircraft panel base can drive the data transmission unit of the aircraft panel base to perform data transmission with each second element module, and second element information and second hardware driving data corresponding to each second element module are obtained, wherein the second element information comprises the number of the second element modules installed on the aircraft panel base and the function types of the second element modules, and the second hardware driving data are related hardware information corresponding to each second element module.
Optionally, each second element module includes at least one second display element module, that is, each second element module includes at least one second display element module having a display function. And the aircraft panel base transmits the acquired second element information and second hardware driving data to the upper computer. And after receiving the second element information and the second hardware driving data, the upper computer performs data processing based on the received second element information and the second hardware driving data to determine second display data corresponding to each second display element module.
And then, the upper computer transmits the determined second display data corresponding to each second display element module back to the plane panel base. And after receiving the second display data corresponding to each second display element module, the aircraft panel base sends the corresponding second display data to each second display element module, and for each second display element module, the second display data is used for the second display element module to perform data display according to the second display data.
Through this application embodiment, through the aircraft panel base of quick reconsitution, need not to carry out die sinking production and complicated circuit wiring work, only need according to the plug component module at will of debugging scheme on aircraft panel base, can debug the component module according to the debugging scheme after the adjustment and change, great improvement aircraft panel base's design and development efficiency, greatly reduced the wasting of resources, reduced development cost.
In an alternative embodiment, each of the first component modules includes at least one operating component module, and the method further includes:
for each operating element module, acquiring operating data of a target object aiming at the operating element module;
sending operation data corresponding to each operation element module to the upper computer;
and receiving third display data which is sent by the upper computer and determined based on the operation data, so that the first display element module corresponding to the third display data performs data display according to the third display data.
Optionally, each first element module includes at least one operating element module, such as a button-type operating element module and a knob-type operating element module, after a commissioning worker (i.e., a target object) performs a corresponding operation on at least one operating element module on the aircraft panel base, for each operating element module, the inside of the element module collects operating data of the operating element module through data collection, and transmits the operating data to the aircraft panel base through a data transmission interface, and at this time, the aircraft panel base may acquire operating data of the target object for the operating element module.
And then, the plane panel base sends the operation data corresponding to each operation element module to the upper computer. In an optional embodiment, the sending the operation data corresponding to each operation element module to the upper computer includes:
and sending the operation data corresponding to each operation element module to the upper computer according to a preset data transmission protocol between the aircraft panel base and the upper computer.
Optionally, the program recorded in the chip of the aircraft panel base may automatically generate a standard data protocol (that is, the data transmission protocol) according to a protocol rule set in advance, and transmit operation data corresponding to each operating element module on the aircraft panel base to the upper computer through the network communication unit of the aircraft panel base, where it is to be noted that the network communication unit of the aircraft panel base also needs to transmit element information and hardware driving data corresponding to each operating element module to the upper computer at the same time.
After the upper computer receives the operation data, the element information and the hardware driving data corresponding to each operation element module, third display data corresponding to each first display element module contained in each first element module is determined based on the data, and the determined third display data corresponding to each first display element module is transmitted back to the aircraft panel base. And after receiving the third display data corresponding to each first display element module, the aircraft panel base sends the corresponding third display data to each first display element module, and for each first display element module, the third display data are used for the first display element module to perform data display according to the third display data.
Optionally, an embodiment of the present application provides a data transmission protocol, as shown in table 1:
TABLE 1
For example, suppose that it is necessary to turn an altitude knob (an operating element module) on an aircraft panel base, the element module of the altitude knob transmits the turning data to the aircraft panel base through a data transmission unit.
After the aircraft panel base integrates operation data (including height knobs) of all element modules installed on the aircraft panel base, a data transmission protocol is generated according to rules established between the aircraft panel base and an upper computer, and related data (including element information, hardware driving data and operation data) of all the element modules are sent to the upper computer according to the data transmission protocol.
And after receiving the relevant data of each element module, the upper computer sends target altitude display data (third display data) back to the airplane panel base through logic processing, and the airplane panel base distributes the display data (third display data) to the target altitude nixie tube. Through the above process, assuming that the target height nixie tube is displayed as 10000 before being rotated, when the debugger rotates the target height knob right, the display of the target height nixie tube is changed from 10000 to 10100.
According to the embodiment of the application, the data transmission protocol of the panel device and the upper computer is automatically generated according to the established rule, and the development cost of a software layer is reduced.
A debugging scheme of an element module in the embodiment of the present application is described in detail below with reference to an example, referring to fig. 2, fig. 2 is a schematic flow chart of another debugging method of an element module provided in the embodiment of the present application, as shown in fig. 2, and the specific steps are as follows:
in step S201, the panel base identifies the type of each component module.
Each component module is installed on the panel base in advance according to a preset debugging scheme, see fig. 3, and fig. 3 is a schematic diagram of a connection relationship between a component module and the panel base according to an embodiment of the present application. As shown in fig. 3, the panel base supplies power to the component module through the standardized interface, the component module includes an operation component and a display component, the program recorded in the chip of the operation component performs a data acquisition function, that is, acquires operation data, and transmits the acquired operation data to the panel base through the standardized plug/socket and the data transmission unit of the component module. The panel base issues display data to the display element through the data transmission unit of the element module through the standardized plug/socket.
Fig. 4 is a schematic diagram of a connection relationship between an element module, a panel base, and an upper computer according to an embodiment of the present disclosure. As shown in fig. 4, an external power supply supplies power to the panel base through a power bus, and the panel base supplies power to the component module through a standardized interface slot/plug. The panel base comprises a data transmission unit, the element module performs data transmission (such as transmission of operation data of the element module to the panel base) with the data transmission unit of the panel base through a standardized interface/slot at the bottom, the panel base uploads the operation data of the element module to the upper computer through the network communication unit, and the upper computer transmits display data back to the panel base.
Optionally, the panel base can identify the types of all component modules mounted on the panel base, which is described in detail in the foregoing and is not described herein again.
Step S202, generating a data transmission protocol according to an agreed rule.
Step S203, collecting element information and hardware driving data of each element module, and collecting operation data of the operation type element module.
In step S204, the panel base receives the component information and the hardware driving data of all the component modules, and the operation data of the operation component module.
In step S205, the panel base uploads the component information and the hardware driving data of all the component modules, and the operation data of the operation component module.
And S206, uploading the element information and hardware driving data of all the element modules and operating data of the operating element modules to the upper computer by the panel base.
And step S207, the upper computer determines display data based on the received data and transmits the display data back to the panel base.
In step S208, the panel base distributes display data to each display element module.
In step S209, each display element module displays data according to the corresponding display data.
For the above steps S201 to S209, reference may be made to the foregoing description, which is not repeated herein.
Through this application embodiment, use standardized component module can reconstruct aircraft panel base fast, need not to carry out die sinking production and complicated circuit wiring work, only need according to design at will plug component module on panel base, great improvement panel base's design development efficiency.
Referring to fig. 4, fig. 4 is a schematic structural diagram of a debugging apparatus of an element module according to an embodiment of the present application.
The debugging device 1 of the element module provided by the embodiment of the application comprises:
a first obtaining module 11, configured to obtain first element information and first hardware driving data corresponding to each first element module installed on the aircraft panel base, where each first element module is installed on the reusable aircraft panel base according to a preset debugging scheme;
the first transmission module 12 is used for transmitting the information of each first element and the drive data of each first hardware to the upper computer;
a first receiving module 13, configured to receive first display data, which is sent by the upper computer and corresponds to at least one first display element module, where any one of the first display element modules is one of the first element modules, and any one of the first display data is determined by the upper computer based on the first element information and the first hardware driving data;
a first sending module 14, configured to send, for each first display element module, the corresponding first display data to the first display element module, so that the first display element module performs data display according to the first display data.
In an optional embodiment, the apparatus further comprises:
the second obtaining module is used for obtaining second element information and second hardware driving data which correspond to each second element module installed on the plane panel base according to the adjusted debugging scheme under the condition that the debugging scheme is adjusted;
the second transmission module is used for transmitting the information of each second element and the drive data of each second hardware to the upper computer;
a second receiving module, configured to receive at least one piece of second display data, which is sent by the upper computer and is specific to at least one second display element module, where any one of the second display element modules is one of the second element modules, and any one of the second display data is determined by the upper computer based on the second element information and the second hardware driving data;
and a second sending module, configured to send, to each second display element module, corresponding second display data to the second display element module, where each second display data is used for the corresponding second display element module to perform data display according to the second display data.
In an alternative embodiment, each of the first component modules includes at least one operating component module, and the apparatus further includes:
the third acquisition module is used for acquiring the operation data of the target object aiming at each operation element module;
the third sending module is used for sending the operation data corresponding to each operation element module to the upper computer;
and a third receiving module, configured to receive third display data that is sent by the upper computer and is determined based on each piece of operation data, so that the first display element module corresponding to the third display data performs data display according to the third display data.
In an optional embodiment, the third sending module is specifically configured to:
and sending the operation data corresponding to each operation element module to the upper computer according to a preset data transmission protocol between the aircraft panel base and the upper computer.
In an optional embodiment, the aircraft panel base includes a housing, a standardized interface slot, a data bus and a power bus corresponding to the standardized interface slot, a chip, a power bus, a data transmission unit, and a network communication unit.
In an alternative embodiment, for each of the first component modules, the first component module is connected to the standardized interface slot of the aircraft panel base via a standardized plug at the bottom of the first component module.
In the embodiment of the application, each first element module is installed on a reusable airplane panel base according to a preset debugging scheme, then, first element information and first hardware driving data corresponding to each first element module are obtained through the airplane panel base, the first element information and the first hardware driving data are transmitted to an upper computer, the upper computer determines first display data corresponding to at least one first display element module based on the first element information and the first hardware driving data, and after the airplane panel base receives the first display data corresponding to each first display element module sent by the upper computer, the airplane panel base sends the corresponding first display data to each first display element module, so that each first display element module performs data display according to the first display data. By adopting the mode, each element module is arranged on the reusable airplane panel base according to the preset debugging scheme, so that the airplane panel base realizes the quick reconfigurable function, the utilization rate of the airplane panel base is improved, the resource waste is reduced, the cost is reduced, and the physical element module has real physical feedback and improves the operation experience of pilots compared with the traditional digital control panel.
In a specific implementation, the debugging apparatus 1 of the component module may execute the implementation manners provided in the steps in fig. 1 through the built-in function modules, which may specifically refer to the implementation manners provided in the steps, and will not be described herein again.
Referring to fig. 6, fig. 6 is a schematic structural diagram of an electronic device provided in an embodiment of the present application. As shown in fig. 6, the electronic device 1000 in the present embodiment may include: the processor 1001, the network interface 1004, and the memory 1005, and the electronic device 1000 may further include: a user interface 1003, and at least one communication bus 1002. Wherein a communication bus 1002 is used to enable connective communication between these components. The user interface 1003 may include a Display screen (Display) and a Keyboard (Keyboard), and the optional user interface 1003 may also include a standard wired interface and a standard wireless interface. The network interface 1004 may optionally include a standard wired interface, a wireless interface (e.g., WI-FI interface). The memory 1004 may be a high-speed RAM memory or a non-volatile memory (e.g., at least one disk memory). The memory 1005 may optionally be at least one memory device located remotely from the processor 1001. As shown in fig. 6, a memory 1005, which is a kind of computer-readable storage medium, may include therein an operating system, a network communication module, a user interface module, and a device control application program.
In the electronic device 1000 shown in fig. 6, the network interface 1004 may provide a network communication function; the user interface 1003 is an interface for providing a user with input; and the processor 1001 may be used to invoke a device control application stored in the memory 1005.
It should be understood that, in some possible embodiments, the processor 1001 may be a Central Processing Unit (CPU), and the processor may be other general-purpose processors, digital Signal Processors (DSPs), application Specific Integrated Circuits (ASICs), field-programmable gate arrays (FPGAs) or other programmable logic devices, discrete gate or transistor logic devices, discrete hardware components, or the like. A general purpose processor may be a microprocessor or the processor may be any conventional processor or the like. The memory may include both read-only memory and random access memory, and provides instructions and data to the processor. A portion of the memory may also include non-volatile random access memory. For example, the memory may also store device type information.
In a specific implementation, the electronic device 1000 may execute the implementation manners provided in the steps in fig. 1 through the built-in functional modules, which may specifically refer to the implementation manners provided in the steps, and are not described herein again.
An embodiment of the present application further provides a computer-readable storage medium, where a computer program is stored in the computer-readable storage medium, and is executed by a processor to implement the method provided in each step in fig. 1, which may specifically refer to the implementation manner provided in each step, and is not described herein again.
The computer-readable storage medium may be an internal storage unit of the debugging apparatus of the component module provided in any of the foregoing embodiments, for example, a hard disk or a memory of an electronic device. The computer readable storage medium may also be an external storage device of the electronic device, such as a plug-in hard disk, a Smart Memory Card (SMC), a Secure Digital (SD) card, a flash card (flash card), and the like, which are provided on the electronic device. The computer readable storage medium may further include a magnetic disk, an optical disk, a read-only memory (ROM), a Random Access Memory (RAM), and the like. Further, the computer readable storage medium may also include both an internal storage unit and an external storage device of the electronic device. The computer-readable storage medium is used for storing the computer program and other programs and data required by the electronic device. The computer readable storage medium may also be used to temporarily store data that has been output or is to be output.
Embodiments of the present application provide a computer program product or computer program comprising computer instructions stored in a computer readable storage medium. The computer instructions are read by a processor of the electronic device from the computer-readable storage medium, and the processor executes the computer instructions, so that the computer device executes the method provided by the steps in fig. 1.
The terms "first", "second", and the like in the claims and in the description and drawings of the present application are used for distinguishing between different objects and not for describing a particular order. Furthermore, the terms "include" and "have," as well as any variations thereof, are intended to cover non-exclusive inclusions. For example, a process, method, system, article, or electronic device that comprises a list of steps or elements is not limited to only those steps or elements listed, but may alternatively include other steps or elements not listed, or inherent to such process, method, article, or electronic device. Reference herein to "an embodiment" means that a particular feature, structure, or characteristic described in connection with the embodiment can be included in at least one embodiment of the application. The appearances of the phrase in various places in the specification are not necessarily all referring to the same embodiment, nor are separate or alternative embodiments mutually exclusive of other embodiments. It is explicitly and implicitly understood by one skilled in the art that the embodiments described herein can be combined with other embodiments. The term "and/or" as used in this specification and the appended claims refers to and includes any and all possible combinations of one or more of the associated listed items.
Those of ordinary skill in the art will appreciate that the elements and algorithm steps of the examples described in connection with the embodiments disclosed herein may be embodied in electronic hardware, computer software, or combinations of both, and that the components and steps of the examples have been described in a functional general in the foregoing description for the purpose of illustrating clearly the interchangeability of hardware and software. Skilled artisans may implement the described functionality in varying ways for each particular application, but such implementation decisions should not be interpreted as causing a departure from the scope of the present application.
The above disclosure is only for the purpose of illustrating the preferred embodiments of the present application and is not to be construed as limiting the scope of the present application, which is therefore intended to be covered by the present application with all equivalent modifications made to the claims of the present application.
Claims (10)
1. A method of commissioning a component module for application to an aircraft panel base, the method comprising:
acquiring first element information and first hardware driving data corresponding to each first element module installed on the aircraft panel base, wherein each first element module is installed on the reusable aircraft panel base according to a preset debugging scheme;
transmitting the information of each first element and the driving data of each first hardware to an upper computer;
receiving first display data which are sent by the upper computer and correspond to at least one first display element module respectively, wherein any one first display element module is one element module in each first element module, and any one first display data is determined by the upper computer based on each first element information and each first hardware driving data;
for each first display element module, sending the corresponding first display data to the first display element module, so that the first display element module performs data display according to the first display data.
2. The method of claim 1, further comprising:
acquiring second element information and second hardware driving data corresponding to each second element module installed on the aircraft panel base according to the adjusted debugging scheme under the condition that the debugging scheme is adjusted;
transmitting the information of each second element and the driving data of each second hardware to the upper computer;
receiving at least one piece of second display data which is sent by the upper computer and aims at least one second display element module, wherein any one second display element module is one element module in each second element module, and any one piece of second display data is determined by the upper computer based on each piece of second element information and each piece of second hardware driving data;
and for each second display element module, sending the corresponding second display data to the second display element module, so that the second display element module performs data display according to the second display data.
3. The method of claim 1, wherein each first element module comprises at least one operational element module, the method further comprising:
for each operating element module, acquiring operating data of a target object aiming at the operating element module;
sending operation data corresponding to each operation element module to the upper computer;
and receiving third display data which are sent by the upper computer and determined based on the operation data, so that the first display element module corresponding to the third display data displays data according to the third display data.
4. The method according to claim 3, wherein the sending the operation data corresponding to each operation element module to the upper computer comprises:
and sending the operation data corresponding to each operation element module to the upper computer according to a preset data transmission protocol between the aircraft panel base and the upper computer.
5. The method of claim 1, wherein the aircraft panel base comprises a housing, a standardized interface slot, a data bus and a power bus corresponding to the standardized interface slot, a chip, a power bus, a data transmission unit, and a network communication unit.
6. The method of claim 1, wherein for each of the first component modules, the first component module connects with a standardized interface socket of the aircraft panel base via a standardized plug at a bottom of the first component module.
7. An apparatus for debugging a component module, the apparatus comprising:
the system comprises a first acquisition module, a second acquisition module and a control module, wherein the first acquisition module is used for acquiring first element information and first hardware driving data which correspond to each first element module arranged on an aircraft panel base, and each first element module is arranged on the reusable aircraft panel base according to a preset debugging scheme;
the first transmission module is used for transmitting the information of each first element and the drive data of each first hardware to the upper computer;
the first receiving module is used for receiving first display data which are sent by the upper computer and correspond to at least one first display element module respectively, wherein any one first display element module is one element module in each first element module, and any one first display data is determined by the upper computer based on each first element information and each first hardware driving data;
the first sending module is configured to send, to each first display element module, corresponding first display data to the first display element module, so that the first display element module performs data display according to the first display data.
8. The apparatus of claim 7, further comprising:
the second acquisition module is used for acquiring second element information and second hardware driving data which correspond to each second element module installed on the aircraft panel base according to the adjusted debugging scheme under the condition that the debugging scheme is adjusted;
the second transmission module is used for transmitting the information of each second element and the drive data of each second hardware to the upper computer;
the second receiving module is used for receiving at least one piece of second display data which is sent by the upper computer and aims at least one second display element module, wherein any one second display element module is one element module in each second element module, and any one piece of second display data is determined by the upper computer based on each piece of second element information and each piece of second hardware driving data;
and a second sending module, configured to send, to each second display element module, the corresponding second display data to the second display element module, so that the second display element module performs data display according to the second display data.
9. An electronic device comprising a processor and a memory, the processor and the memory being interconnected;
the memory is used for storing a computer program;
the processor is configured to perform the method of any of claims 1 to 6 when the computer program is invoked.
10. A computer-readable storage medium, characterized in that the computer-readable storage medium stores a computer program which is executed by a processor to implement the method of any one of claims 1 to 6.
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