CN113704882A - Full-machine standard view construction method based on standard data structuralization - Google Patents

Full-machine standard view construction method based on standard data structuralization Download PDF

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CN113704882A
CN113704882A CN202110905170.4A CN202110905170A CN113704882A CN 113704882 A CN113704882 A CN 113704882A CN 202110905170 A CN202110905170 A CN 202110905170A CN 113704882 A CN113704882 A CN 113704882A
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full
specifications
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何俊伟
苗壮
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Shenyang Aircraft Design and Research Institute Aviation Industry of China AVIC
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Shenyang Aircraft Design and Research Institute Aviation Industry of China AVIC
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Abstract

The application relates to the technical management field, in particular to a full-machine standard view construction method based on standard data structuring, which comprises the steps of S1, forming independent standard items based on various standards, and importing the independent standard items into a management system; step S2, carrying out deduplication processing on the standard items in the management system; step S3, according to the incidence relation between each standard item and each airplane design requirement, a verification matrix for standard implementation is constructed, wherein the incidence relation refers to that each airplane design corresponds to one or more standard items. The method and the device can assist designers in selecting and implementing the standard correctly, ensure that the designers select and apply the standard specification correctly, and improve the development quality.

Description

Full-machine standard view construction method based on standard data structuralization
Technical Field
The application relates to the technical management field, in particular to a full-machine standard view construction method based on standard data structuring.
Background
The standard implementation is a basic requirement of military parties on the standard work of models, the traditional standard implementation method is characterized in that a standard professional provides a standard selection catalogue, a designer uses a standard in a project development process, the problems of over-catalogue selection, wrong selection, non-selection of the standard and the like exist, particularly, the designer does not know specific standard terms, the design requirement is divorced from the standard requirement, the phenomenon of two layers of leather is serious, a plurality of normative problems of project development are caused, and the design is difficult and the quality is improved.
Disclosure of Invention
The patent provides a set of brand-new standard implementation method and means, and the full-machine standard view is constructed to assist designers in correctly selecting and implementing the standard, so that the correct selection and application of the standard specification of the designers are ensured, and the development quality is improved.
The application provides a full-machine standard view construction method based on standard data structuring, which mainly comprises the following steps:
step S1, importing the independent standard items formed based on various standards into a management system;
step S2, carrying out deduplication processing on the standard items in the management system;
step S3, according to the incidence relation between each standard item and each airplane design requirement, a verification matrix for standard implementation is constructed, wherein the incidence relation refers to that each airplane design corresponds to one or more standard items.
Preferably, the step S1 further includes:
step S11, determining various standards for model development and selection;
and step S12, standard elements in various standards are obtained, independent standard items are formed, and the standard items are imported into the management system.
Preferably, before step S11, the method further includes the step of collecting the heading information of the combing item.
Preferably, the management system comprises a DOORS.
Preferably, step S3 further includes determining the demand item lacking the existing standard support, and forming a standard prediction model.
Preferably, the method further comprises forming a model-specific standard set according to the standard prediction model, wherein the model-specific standard set comprises system specifications, development specifications, product specifications, software specifications, process specifications, material specifications, design specifications and test specifications.
Preferably, step S3 is followed by performing multi-dimensional statistical analysis on the adopted standard information in the verification matrix, wherein the statistical analysis includes standard type, standard age, standard technical level and civil and military commonality.
Another aspect of the present application provides an electronic device, which includes a memory, a processor, and a computer program stored in the memory and capable of running on the processor, and the processor executes the computer program to implement the above full-computer standard view building method based on standard data structuring.
Another aspect of the present application provides a computer-readable storage medium, which stores a computer program, and when the computer program is executed by a processor, the computer program can implement the above method for constructing a full-machine standard view based on standard data structuring.
The beneficial effects of adopting the above scheme are as follows:
1) because the standard text is structured into the standard data and is combed into the standard data modules which are in one-to-one correspondence with the design requirements, the implementation degree of the standard specification is improved by 85 percent compared with the prior art.
2) The design requirements can be deeply analyzed by each system of the project, the relevant standards on which various requirement indexes can be realized are determined, the standard items are refined, and the association link matrix of the design requirement items and the standard items is established.
3) And analyzing the missing standard in the matrix for the technical requirement index lacking the standard support, and developing special standard prediction and compilation to form a project special standard set.
4) And carrying out multi-dimensional statistical analysis on the standard type, standard age, standard technical level, civil and military universality and the like on the collected standard information in the matrix, and further optimizing and executing a standard system according to an analysis result.
5) The project development has national military standards as bases, the design is more reasonable, the design quality is improved, the development period is shortened, and the development cost is saved.
Drawings
FIG. 1 is a flow chart of a method for constructing a full-machine standard view based on standard data structuring according to the present application.
Fig. 2 is a schematic view of a preferred embodiment of the electronic device of the present application.
Detailed Description
In order to make the implementation objects, technical solutions and advantages of the present application clearer, the technical solutions in the embodiments of the present application will be described in more detail below with reference to the accompanying drawings in the embodiments of the present application. In the drawings, the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The described embodiments are some, but not all embodiments of the present application. The embodiments described below with reference to the drawings are exemplary and intended to be used for explaining the present application, and should not be construed as limiting the present application. All other embodiments obtained by a person of ordinary skill in the art without any inventive work based on the embodiments in the present application are within the scope of protection of the present application. Embodiments of the present application will be described in detail below with reference to the drawings.
The application provides a full-machine standard view construction method based on standard data structuring, as shown in fig. 1, which mainly comprises the following steps:
step S1, importing the independent standard items formed based on various standards into a management system;
step S2, carrying out deduplication processing on the standard items in the management system;
step S3, according to the incidence relation between each standard item and each airplane design requirement, a verification matrix for standard implementation is constructed, wherein the incidence relation refers to that each airplane design corresponds to one or more standard items.
In some alternative embodiments, step S1 further includes:
step S11, determining various standards for model development and selection;
and step S12, standard elements in various standards are obtained, independent standard items are formed, and the standard items are imported into the management system.
In some optional embodiments, before step S11, further comprising the step of collecting the heading information of the combed item.
In some alternative embodiments, the management system comprises a DOORS.
In the above embodiment, the standard text is split in step S1, the standard elements are structured to form a standard module, which mainly includes item tagging information, various standards developed and selected by model are comprehensively combed based on design requirements and standard view angles, after the standard items are determined, the standard elements in the standard text are structured and split into independent standard items, and the standard items are imported into a data management system (e.g., DOORS) for management.
In step S2, the standard data imported into the data management system is relatively scattered and has high repeatability, and the standard data must be subjected to deduplication, error correction, and other processing, and then sorted and analyzed according to the use requirements to form usable standard data, which is a basis for constructing standard matrix identification.
In some alternative embodiments, step S3 further includes determining a demand item that lacks an existing standard support, forming a standard predictive model.
In some alternative embodiments, further comprising forming a model specific set of standards from the standard predictive model, the model specific set of standards including system specifications, development specifications, product specifications, software specifications, process specifications, material specifications, design specifications, and test specifications.
As shown in fig. 1, in step S3, based on the module, the design requirement items of the equipment-plane level and the standard items are established for correlation tracing, a standard implementation verification matrix is formed, and the standard implementation effect is enhanced by implementing visual display on the designer in response to standard multi-dimensional statistical analysis.
In some optional embodiments, step S3 is followed by performing multi-dimensional statistical analysis on the mining target information in the verification matrix, wherein the statistical analysis includes standard type, standard age, standard skill level, and civil and military commonality.
The application also provides an electronic device, which comprises a memory, a processor and a computer program stored in the memory and capable of running on the processor, wherein the processor implements the above full-machine standard view construction method based on standard data structuring when executing the computer program.
The application also provides a computer readable storage medium, which stores a computer program, and the computer program can realize the above full-machine standard view construction method based on standard data structuring when being executed by a processor.
FIG. 2 is an exemplary block diagram of an electronic device capable of implementing functionality provided in accordance with one embodiment of the present application. As shown in fig. 2, the electronic device includes an input device 501, an input interface 502, a central processor 503, a memory 504, an output interface 505, and an output device 506. The input interface 502, the central processing unit 503, the memory 504 and the output interface 505 are connected to each other through a bus 507, and the input device 501 and the output device 506 are connected to the bus 507 through the input interface 502 and the output interface 505, respectively, and further connected to other components of the electronic device. Specifically, the input device 504 receives input information from the outside and transmits the input information to the central processor 503 through the input interface 502; the central processor 503 processes input information based on computer-executable instructions stored in the memory 504 to generate output information, temporarily or permanently stores the output information in the memory 504, and then transmits the output information to the output device 506 through the output interface 505; the output device 506 outputs the output information to the outside of the electronic device for use by the user.
That is, the electronic device shown in fig. 2 may also be implemented to include: a memory storing computer-executable instructions; and one or more processors that when executing computer executable instructions may implement the unmanned aerial vehicle autonomous homing model training method described in connection with fig. 1.
In one embodiment, the electronic device shown in fig. 2 may be implemented to include: a memory 504 configured to store executable program code; one or more processors 503 configured to execute the executable program code stored in the memory 504 to perform the full-machine standard view construction method based on standard data structuring in the above embodiments.
In a typical configuration, a computing device includes one or more processors (CPUs), input/output interfaces, network interfaces, and memory.
The memory may include forms of volatile memory in a computer readable medium, Random Access Memory (RAM) and/or non-volatile memory, such as Read Only Memory (ROM) or flash memory (flash RAM). Memory is an example of a computer-readable medium.
Computer-readable media include both non-transitory and non-transitory, removable and non-removable media that implement information storage by any method or technology. The information may be computer readable instructions, data structures, modules of a program, or other data. Examples of computer storage media include, but are not limited to, phase change memory (PRAM), Static Random Access Memory (SRAM), Dynamic Random Access Memory (DRAM), other types of Random Access Memory (RAM), Read Only Memory (ROM), Electrically Erasable Programmable Read Only Memory (EEPROM), flash memory or other memory technology, compact disc read only memory (CD-ROM), Digital Versatile Discs (DVD) or other optical storage, magnetic cassettes, magnetic tape, magnetic disk storage or other magnetic storage devices, or any other non-transmission medium that can be used to store information that can be accessed by a computing device.
As will be appreciated by one skilled in the art, embodiments of the present application may be provided as a method, system, or computer program product. Accordingly, the present application may take the form of an entirely hardware embodiment, an entirely software embodiment or an embodiment combining software and hardware aspects. Furthermore, the present application may take the form of a computer program product embodied on one or more computer-usable storage media (including, but not limited to, disk storage, CD-ROM, optical storage, and the like) having computer-usable program code embodied therein.
Furthermore, it will be obvious that the term "comprising" does not exclude other elements or steps. A plurality of units, modules or devices recited in the device claims may also be implemented by one unit or overall device by software or hardware. The terms first, second, etc. are used to identify names, but not any particular order.
The flowchart and block diagrams in the figures illustrate the architecture, functionality, and operation of possible implementations of systems, methods and computer program products according to various embodiments of the present application. In this regard, each block in the flowchart or block diagrams may represent a module, segment, or portion of code, which comprises one or more executable instructions for implementing the specified logical function(s). It should also be noted that, in some alternative implementations, the functions noted in the block may occur out of the order noted in the figures. For example, two blocks identified in succession may, in fact, be executed substantially concurrently, or the blocks may sometimes be executed in the reverse order, depending upon the functionality involved. It will also be noted that each block of the block diagrams and/or flowchart illustration, and combinations of blocks in the block diagrams and/or flowchart illustration, can be implemented by special purpose hardware-based systems which perform the specified functions or acts, or combinations of special purpose hardware and computer instructions.
The Processor in this embodiment may be a Central Processing Unit (CPU), other general purpose Processor, a Digital Signal Processor (DSP), an Application Specific Integrated Circuit (ASIC), an off-the-shelf Programmable Gate Array (FPGA) or other Programmable logic device, a discrete Gate or transistor logic device, a discrete hardware component, and so on. A general purpose processor may be a microprocessor or the processor may be any conventional processor or the like.
The memory may be used to store computer programs and/or modules, and the processor may implement various functions of the apparatus/terminal device by running or executing the computer programs and/or modules stored in the memory, as well as by invoking data stored in the memory. The memory may mainly include a storage program area and a storage data area, wherein the storage program area may store an operating system, an application program required by at least one function (such as a sound playing function, an image playing function, etc.), and the like; the storage data area may store data (such as audio data, a phonebook, etc.) created according to the use of the cellular phone, and the like. In addition, the memory may include high speed random access memory, and may also include non-volatile memory, such as a hard disk, a memory, a plug-in hard disk, a Smart Media Card (SMC), a Secure Digital (SD) Card, a Flash memory Card (Flash Card), at least one magnetic disk storage device, a Flash memory device, or other volatile solid state storage device.
In this embodiment, the module/unit integrated with the apparatus/terminal device may be stored in a computer-readable storage medium if it is implemented in the form of a software functional unit and sold or used as a separate product. Based on such understanding, all or part of the flow in the method according to the embodiments of the present invention may also be implemented by a computer program, which may be stored in a computer-readable storage medium and used by a processor to implement the steps of the above-described embodiments of the method. Wherein the computer program comprises computer program code, which may be in the form of source code, object code, an executable file or some intermediate form, etc. The computer readable medium may include: any entity or device capable of carrying computer program code, recording medium, U.S. disk, removable hard disk, magnetic disk, optical disk, computer Memory, Read-Only Memory (ROM), Random Access Memory (RAM), electrical carrier wave signals, telecommunications signals, software distribution media, and the like.
It should be noted that the computer readable medium may contain content that is appropriately increased or decreased as required by legislation and patent practice in the jurisdiction. Although the present application has been described with reference to the preferred embodiments, it is not intended to limit the present application, and those skilled in the art can make variations and modifications without departing from the spirit and scope of the present application.
Although the invention has been described in detail hereinabove with respect to a general description and specific embodiments thereof, it will be apparent to those skilled in the art that modifications or improvements may be made thereto based on the invention. Accordingly, such modifications and improvements are intended to be within the scope of the invention as claimed.

Claims (9)

1. A full-machine standard view construction method based on standard data structuring is characterized by comprising the following steps:
step S1, importing the independent standard items formed based on various standards into a management system;
step S2, carrying out deduplication processing on the standard items in the management system;
step S3, according to the incidence relation between each standard item and each airplane design requirement, a verification matrix for standard implementation is constructed, wherein the incidence relation refers to that each airplane design corresponds to one or more standard items.
2. The method for building a full-machine standard view based on standard data structuring according to claim 1, wherein the step S1 further comprises:
step S11, determining various standards for model development and selection;
and step S12, standard elements in various standards are obtained, independent standard items are formed, and the standard items are imported into the management system.
3. The method for constructing full-machine standard view based on standard data structuring according to claim 2, wherein before step S11, further comprising combing item target information.
4. The method for building a full-machine standard view based on standard data structuring according to claim 1, wherein the management system comprises DOORS.
5. The method for constructing a full-machine standard view based on standard data structuring as claimed in claim 1, wherein step S3 further comprises determining the requirement items lacking the existing standard support, and forming a standard prediction model.
6. The method of claim 5, further comprising forming a model specific set of standards from the standard predictive model, the model specific set of standards including system specifications, development specifications, product specifications, software specifications, process specifications, material specifications, design specifications, and test specifications.
7. The method for constructing a full-machine standard view based on standard data structuring according to claim 1, wherein step S3 is followed by performing multi-dimensional statistical analysis of standard type, standard age, standard skill level and civil and military commonality on the adopted standard information in the verification matrix.
8. An electronic device, comprising a memory, a processor and a computer program stored in the memory and capable of running on the processor, wherein the processor executes the computer program to implement the above full computer standard view construction method based on standard data structuring.
9. A computer-readable storage medium, characterized in that the computer-readable storage medium stores a computer program, which when executed by a processor is capable of implementing the above standard data structuring-based all-computer standard view construction method.
CN202110905170.4A 2021-08-08 2021-08-08 Full-machine standard view construction method based on standard data structuralization Pending CN113704882A (en)

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Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104850711A (en) * 2015-05-26 2015-08-19 重庆大学 Mechanical and electrical product design standard selecting method
CN107194029A (en) * 2017-04-19 2017-09-22 中国航空综合技术研究所 A kind of normal view modeling method based on architecture frame
CN111367499A (en) * 2019-12-10 2020-07-03 中国航空综合技术研究所 Product demand definition and tracing method based on standard index library
CN111680029A (en) * 2020-06-12 2020-09-18 普元信息技术股份有限公司 Optimization management method based on data standard system label falling

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104850711A (en) * 2015-05-26 2015-08-19 重庆大学 Mechanical and electrical product design standard selecting method
CN107194029A (en) * 2017-04-19 2017-09-22 中国航空综合技术研究所 A kind of normal view modeling method based on architecture frame
CN111367499A (en) * 2019-12-10 2020-07-03 中国航空综合技术研究所 Product demand definition and tracing method based on standard index library
CN111680029A (en) * 2020-06-12 2020-09-18 普元信息技术股份有限公司 Optimization management method based on data standard system label falling

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