CN116611235A - Multi-level componentization model system architecture method, assembly system and method - Google Patents
Multi-level componentization model system architecture method, assembly system and method Download PDFInfo
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Abstract
The invention discloses a multi-level componentization model system architecture method, an assembly system and a method, wherein the architecture method comprises the following steps: defining and storing model basic data, model performance parameters, model expected parameters and model interaction information of a model component, and constructing a multi-level simulation model architecture to obtain a basic model component database; and assembling the model components in the basic model component database through assembly simulation model assembly combinations to obtain a simulation application model, and storing the simulation application model in the simulation application model database. The multi-level model system architecture provided by the invention enables mapping of models among different levels to be achieved, so that a user can endow the model with different forms and simulation granularities according to the attention points of the model in different simulation application scenes, the confidence of the model is improved, and meanwhile, the efficiency of constructing and operating the model is improved.
Description
Technical Field
The invention relates to the field of simulation deduction systems. And more particularly to a multi-level componentized model architecture method, assembly system and method.
Background
The confidence of the model in the simulation deduction system is an important index for evaluating the simulation supporting capability, and the accuracy of the simulation deduction system is directly affected. Simulation models built to fully match the operational mechanisms of the operational entity typically exhibit a careful simulation process with high confidence. However, the attention points of different simulation application scenes to the simulation model are different, for example, the combined combat deduction research does not need a simulation system to finely simulate the operation mechanism of a device subsystem or a component, and only needs to accurately express the device capability parameters in the combat process. Therefore, the realistic requirements of different simulation application scenes on different forms and simulation granularities of the simulation model are generated.
Currently, the mainstream simulation systems all support the assembly of models, so that more complex and higher-level simulation models are built. However, the organization structure of the model in most simulation systems is flattened, the description granularity of the assembly parts is approximately the same, and the model cannot be expressed according to the attention points of specific simulation application scenes, so that the confidence of the constructed model is low. In addition, some simulation assembly processes still need to be realized through codes, the coupling degree between models is extremely high, the whole simulation deduction process and even large-scale integration joint test are difficult, and the usability of the system is greatly reduced.
Disclosure of Invention
The invention aims to provide a multi-level componentization model system architecture method, an assembly system and a method, wherein a model assembly process is established by constructing a multi-level model system structure and an extensible parameter inheritance combination mode and taking components as minimum assembly units, a mapping mechanism among different-level models is opened, iterative check and verification of the models among different levels are promoted, the model confidence is improved, and meanwhile, the model construction and application efficiency is improved.
In order to achieve the above purpose, the invention adopts the following technical scheme:
the first aspect of the present invention provides a multi-level componentized model architecture method, the method comprising:
defining and storing model basic data, model performance parameters, model expected parameters and model interaction information of a model component, and constructing a multi-level simulation model architecture to obtain a basic model component database;
and assembling the model components in the basic model component database through assembly simulation model assembly combinations to obtain a simulation application model, and storing the simulation application model in the simulation application model database.
Preferably, the multi-level simulation model architecture defines assembly combination rules;
the assembly and combination of the componentized simulation models are that models with repeatability, cross-field and heterogeneous characteristics in model components are combined through an assembly mechanism and a style;
the simulation application model comprises a simulation application model assembled by a basic model component and a simulation application model directly serving application system construction.
Preferably, the multi-level simulation model architecture comprises
The first layer is a solid-level model component of a base class in the multi-level simulation model architecture;
the second layer is a platform-level model component and a component-level model component which inherit the base class in the multi-level simulation model architecture;
the third hierarchy includes a platform level subdivision model assembly inheriting the platform level model assembly, and a component level subdivision model assembly inheriting the component level model assembly.
Preferably, the multi-level simulation model architecture comprises at least one of:
parameters of the entity-level model component include the size, weight and country of the model;
parameters of the platform-level model component include platform customization parameters, average travel speed, and maximum travel speed;
parameters of the component level model assembly include size, weight and country of the model;
the platform level subdivision model includes
An aircraft solid model, a ship solid model, a vehicle solid model, a weapon solid model, a satellite solid model, and a ground facility solid model;
the component level subdivision model includes
Sensor models, communication models, interference models, ammunition library models, rack models, and resource center models.
Preferably, the assembly rule is that,
the entity-level model component, the platform-level model component, and the model component subdivided by the platform-level model component are capable of assembling the component-level model component;
the component-level model assembly and the model assembly of the component-level model assembly subdivision cannot be assembled with each other.
The second aspect of the present invention provides a multi-level componentized model assembly system, based on a multi-level componentized model system obtained by the architecture method, the system comprising:
the scheme management unit is used for configuring schemes by users;
the model component management unit is used for managing the basic model components in the basic model component database;
the model assembly module is used for providing all the model assembly information capable of being assembled in the scheme for a user to select according to the assembly combination rule of the multi-level componentization model system architecture;
the model test module is used for testing the suitability of all model components and simulation engine versions on the assembled simulation application model through the iterative check verification of models among different levels, and initializing and rationality of model interfaces;
the basic model component database is used for storing basic model components, can also automatically create a table structure of the model components according to a multi-level componentization model system architecture when a user performs scheme design, and responds to the operations of adding, deleting, modifying and inquiring the records of the basic model component database by the user;
and the simulation application model database is used for storing the simulation application models tested by the model test module.
Preferably, the configuration includes model components, models, parts, and assembly information.
Preferably, the management of the model component includes constructing parameters of the model component, creating, modifying or deleting model components and importing and exporting model component model data.
Preferably, the model component management unit includes
The parameter construction module is used for supporting a user to add, modify or delete performance parameters of the model component;
the performance parameters include basic information of the model component including name, unit, default, and data type.
The third aspect of the invention provides an assembling method based on a multi-level componentized model assembling system, the method comprising:
s1: publishing the basic component database outwards;
s2: managing basic model components in a basic model component database, and configuring a scheme;
s3: according to the information of all the model components which can be assembled in the scheme provided by the assembly system, selecting the model components for combined assembly to obtain a simulation model with a complex model;
s4: testing the suitability of the simulation model and the version of the simulation engine, initialization and rationality of a model interface;
s5: and storing the simulation model subjected to the test into the simulation application model database, and analyzing the information of the simulation model by a simulation engine.
The beneficial effects of the invention are as follows:
the multi-level model system architecture provided by the invention enables mapping of models among different levels to be achieved, so that a user can endow the model with different forms and simulation granularities according to the attention points of the model in different simulation application scenes, and the confidence of the model is improved. The invention can expand model inheritance combination parameters, and a user can not only construct different parts by configuring model assembly parameters, but also expand new parameters for the model assembly, and support the combination of various parts to assemble a model with more complicated and higher level.
Drawings
The following describes the embodiments of the present invention in further detail with reference to the drawings.
FIG. 1 is a flow diagram that illustrates a method of building a componentized model architecture in one embodiment.
FIG. 2 illustrates a database management system data flow diagram in one particular embodiment.
FIG. 3 illustrates a block diagram of a multi-level scalable componentized assembly system in one embodiment.
FIG. 4 is a flow diagram illustrating a multi-level extensible assembly allocation method in one embodiment.
Detailed Description
In order to more clearly illustrate the present invention, the present invention will be further described with reference to the preferred embodiments and the accompanying fig. 1 to 4. Like parts in the drawings are denoted by the same reference numerals. It is to be understood by persons skilled in the art that the following detailed description is illustrative and not restrictive, and that this invention is not limited to the details given herein.
As shown in fig. 1, in a specific embodiment,
a multi-level componentized model architecture method, the method comprising:
defining and storing model basic data, model performance parameters, model expected parameters and model interaction information of a model component, and constructing a multi-level simulation model architecture to obtain a basic model component database;
and assembling the model components in the basic model component database through assembly simulation model assembly combinations to obtain a simulation application model, and storing the simulation application model in the simulation application model database.
Preferably, the multi-level simulation model architecture defines assembly combination rules;
the assembly and combination of the componentized simulation models are that models with repeatability, cross-field and heterogeneous characteristics in model components are combined through an assembly mechanism and a style;
the simulation application model comprises a simulation application model assembled by a basic model component and a simulation application model directly serving application system construction.
In one embodiment, the assembly and combination of the componentized simulation models are based on specific reusable models, and the simulation models with cross-domain, heterogeneous and other characteristics are quickly and flexibly combined together through various assembly mechanisms and modes. The combinability of the simulation model is embodied in several aspects:
reusable simulation models. The reusable model is a basic condition of model assembly, if a model component does not have reusability or insufficient reusability, the model component is difficult to adapt to different application situations, the flexible assembly capability is affected, and the meaning of component type development is lost.
The rapid and flexible combination and recombination process, namely, various simulation models are provided with rich combination mechanisms and patterns, so that different combination requirements are met.
The ability to integrate heterogeneous models provides the ability to integrate models of different fields, different specifications, and even different resolution levels together.
Effectiveness. Validity requires that the combined result be valid and that the combined structure be able to reliably reflect the combined result of the source system.
Customizable capabilities, i.e., the combination system has a variety of ways of customization, including parameter customization, architecture tuning, member addition or subtraction, and interaction relationship changes, etc.
Preferably, the multi-level simulation model architecture comprises
The first layer is a solid-level model component of a base class in the multi-level simulation model architecture;
the second layer is a platform-level model component and a component-level model component which inherit the base class in the multi-level simulation model architecture;
the third hierarchy includes a platform level subdivision model assembly inheriting the platform level model assembly, and a component level subdivision model assembly inheriting the component level model assembly.
Preferably, the multi-level simulation model architecture comprises at least one of:
parameters of the entity-level model component include the size, weight and country of the model;
parameters of the platform-level model component include platform customization parameters, average travel speed, and maximum travel speed;
parameters of the component level model assembly include size, weight and country of the model;
the platform level subdivision model includes
An aircraft solid model, a ship solid model, a vehicle solid model, a weapon solid model, a satellite solid model, and a ground facility solid model;
the component level subdivision model includes
Sensor models, communication models, interference models, ammunition library models, rack models, and resource center models.
Preferably, the assembly rule is that,
the entity-level model component, the platform-level model component, and the model component subdivided by the platform-level model component are capable of assembling the component-level model component;
the component-level model assembly and the model assembly of the component-level model assembly subdivision cannot be assembled with each other.
In one embodiment, the simulation model architecture includes a entity level, a platform level, a component level, a refined model level, and assembly rules.
The granularity of the entity-level model components is coarse, and main parameters comprise model size, weight, country class and the like. The platform-level model component inherits from the entity-level model component, has finer granularity than the entity-level component, and the main parameters are added with platform customization parameters such as average travelling speed, maximum travelling speed and the like on the basis of the entity-level component.
The platform-level model assembly is further subdivided into an airplane model assembly, a vehicle model assembly and the like, wherein the airplane model assembly is inherited by the platform-level model assembly, and main parameters are added to model-specific parameters on the basis of the platform-level model assembly, for example, the airplane model also comprises a span, a maximum take-off weight, a maximum oil carrying capacity and the like.
The component-level model components are at the same level as the entity-level model components, and the main parameters include model size, weight, country, and the like. The component-level model assembly is further subdivided into a sensor assembly, a motion assembly, a communication assembly and the like, the granularity of the sensor assembly is finer than that of the component-level assembly, and the main parameters are added with component customization parameters on the basis of the component-level assembly, for example, the sensor assembly further comprises parameters such as detection distance, pitch angle, azimuth angle, distance detection precision, azimuth angle detection precision, pitch angle detection precision, maximum detection capacity and the like.
The model inter-component assembly rules include that the entity level and platform level and the sub-divided aircraft, ship, vehicle, etc. models can be assembled at the component level and the sub-divided motion components, sensor components, communication components, etc. The component level and the sub-component subdivision level do not allow for mutual assembly.
The multi-level model system architecture provided by the invention enables mapping of models among different levels to be achieved, so that a user can endow the model with different forms and simulation granularities according to the attention points of the model in different simulation application scenes, and the confidence of the model is improved. The invention can expand model inheritance combination parameters, and a user can not only construct different parts by configuring model assembly parameters, but also expand new parameters for the model assembly, and support the combination of various parts to assemble a model with more complicated and higher level.
In one embodiment, the base model components stored in the base model component database may be assembled into a simulation application model according to model assembly rules.
The main body of the resource construction and the model reuse of the general simulation model generally adopts a parameterized design method to provide component support for the development of the simulation application model.
In one embodiment, the simulation model developed based on the components has a hierarchical nature. The models are expressed in a tree-like hierarchical manner in a simulation model management system, one model is expressed as a composite class which can be inherited by other composite classes, and finally an object-oriented model structure tree expressed by the composite class is formed. The simulation model can be regarded as a compound class, and in order to enable the models in the model library to have a unified management mode, standard model specifications are defined by adopting an object with inheritance relationship, namely a model dictionary and a model structure.
In one embodiment, the model is stored in two typical ways: 1) Storing metadata; 2) Object oriented databases. In view of the inadequacy and the immaturity of the application of the object-oriented database, the model obtained by the simulation modeling mainly exists in the form of a file, and the storage of the model adopts a metadata storage mode, namely, the identification information, version information, storage positions, performance parameters, the relation with the model and other information of the model and related documents are stored in a table space of the database, and specific model files and related description documents are stored in a file system.
In one embodiment, for ease of storage and management, the attributes and interface data of the model are stored in a table structure of the database, and these tables should include model tables, attribute tables, interface tables, and structure tables, etc., according to the improved object-oriented model description specification mentioned above. The model table comprises model names, various attribute identifiers, interface identifiers, model structure identifiers, model descriptions and the like; the attribute table comprises an attribute identifier, an attribute name, an attribute value, an attribute unit and the like; the interface table comprises the identification of the interface, the name of the interface, the parameters of the interface and the like; the structure table includes an identification of the structure, a name of the structure, a content of the structure, and the like.
In one embodiment, the simulation application model database includes simulation application models with different granularities, and the simulation application models are assembled by a basic model component and directly serve as application layer models for application system construction, and are the main bodies of simulation test application system construction, including specific model information and the like.
The simulation application model database is a model organization and information query oriented system, so that the stored content is information data of any part and any moment of the simulation model in the whole system and the whole life cycle, and the expression form of the information can be various forms such as texts or charts, even three-dimensional models and the like. The simulation application model database is therefore provided with the capability to store, organize, query and display multiple classes of simulation resources.
In a specific embodiment, several stages are generally divided during the development of a simulation system. In each development stage, the coverage range of model information is wide, the content is numerous, the storage and inquiry of the information are finished, unnecessary data redundancy is avoided as much as possible, the difference of specific information structures of different models and the access requirements of various users are considered, the stored information can only be abstracted to a file level, namely, various files describing the models are used as data units, and the information is organized and managed by links with the models as the relationship between the data, so that the inquiry of the model information can be ensured, the different flexibility among specific details of each model can be ensured, and the model information is more preferable. The overall database management system data flow is shown in fig. 2.
As shown in the flowchart of fig. 2, the data items and data structures to be designed are obtained as follows:
applying model type information, including data item model names, data text names and the like;
the authority verification includes the data items of user name, cipher, etc.
In one embodiment, as shown in figure 3,
the second aspect of the present invention provides a multi-level componentized model assembly system, based on a multi-level componentized model system obtained by the architecture method, the system comprising:
the scheme management unit is used for configuring schemes by users;
the model component management unit is used for managing the basic model components in the basic model component database;
the model assembly module is used for providing all the model assembly information capable of being assembled in the scheme for a user to select according to the assembly combination rule of the multi-level componentization model system architecture;
the model test module is used for testing the suitability of all model components and simulation engine versions on the assembled simulation application model through the iterative check verification of models among different levels, and initializing and rationality of model interfaces;
the basic model component database is used for storing basic model components, can also automatically create a table structure of the model components according to a multi-level componentization model system architecture when a user performs scheme design, and responds to the operations of adding, deleting, modifying and inquiring the records of the basic model component database by the user;
and the simulation application model database is used for storing the simulation application models tested by the model test module.
Preferably, the configuration includes model components, models, parts, and assembly information.
Preferably, the management of the model component includes constructing parameters of the model component, creating, modifying or deleting model components and importing and exporting model component model data.
Preferably, the model component management unit includes
The parameter construction module is used for supporting a user to add, modify or delete performance parameters of the model component;
the performance parameters include basic information of the model component including name, unit, default, and data type.
In particular, the method comprises the steps of,
the scheme management module is used for supporting the user to newly build, open, delete and close model configuration schemes, and different models, components and assembly information are stored in different schemes, so that the user can conveniently switch.
The model component management module comprises parameter construction, creation, deletion, modification and import and export of model data.
The construction parameter function supports the addition, deletion and modification of performance parameters of users, mainly basic information of models, including names, units, default values, data types and the like, wherein the data types of data items can be basic data types generated by sources and can also be other defined complex data structures, so that the nesting of the complex data structures is supported. After the construction of the performance parameters is completed, the software interface updates the model element table display elements.
The model assembly module assembles the combination rule according to the model system, and provides all the information of the parts which can be assembled in the current scheme for the user to select. The user can set parameters such as the assembly name, the assembly position, etc. for the component.
The model test module tests suitability, initialization, model interface and other rationality of all model component libraries and simulation engine versions on the assembled model through iterative check verification of models among different levels, and also supports one-key testing of users.
The database module comprises a basic model component database and a simulation application model database; and automatically creating a table structure of the model according to the simulation model system when a user performs scheme design, and responding to operations of adding, deleting, modifying, inquiring and the like of the database records by the user.
As shown in fig. 4, a multi-level componentization model assembling method includes:
the third aspect of the invention provides an assembling method based on a multi-level componentized model assembling system, the method comprising:
s1: publishing the basic component database outwards;
specifically, the simulation model system is used for organizing the simulation models from different levels, so that the characteristics concerned by the models of different levels are more clearly expressed, and the users can be favorably endowed with different forms and simulation granularities according to the concerned points of the models in different simulation application scenes.
For example, a user may choose to instantiate from a solid or platform level model or an airplane model to simulate airplanes of different granularities. In addition, the user can assemble the model with the required components, such as moving components, sensor components, data processing components, etc. These parts may also choose to inherit from a part-level model or a corresponding component model to simulate assembled parts of different granularities. In terms of assembly rules, models of the entity and platform levels and the underlying sub-divided aircraft, ship, vehicle, etc. may be assembled with component levels and the underlying sub-divided motion components, sensor components, communication components, etc. The component level and the sub-component subdivision level do not allow for mutual assembly.
S2: managing basic model components in a basic model component database, and configuring a scheme;
s3: according to the information provided by the assembly system, all the model components which can be assembled in the scheme are selected to be assembled in a combined mode, so that a simulation model with a complex model is obtained.
Specifically, when a user determines a model component to be instantiated, the multi-level componentized model assembly system automatically obtains configurable parameters of the model component from a model system, and the user can configure the parameters to form different models. If the model is derived from a user-defined model, a user can also specify a parameter format for the model, and support variable names, default values, value ranges, variable types and descriptions of user-defined parameters, wherein the variable types can be basic data types generated by the source or complex data structures defined by the user at a data definition layer. The step generates an association relation between the parameter format and the complex data structure, and completes the parameter design of the model, and the model with the same performance parameter format is the same.
S4: testing the suitability of the simulation model and the version of the simulation engine, initialization and rationality of a model interface;
specifically, based on the established model assembly combination rule, the user can assemble the components in a combined way to form a model with more complexity and higher hierarchy. The model needs to be tested to ensure that the model can be loaded by a simulation engine correctly, and the suitability, initialization, model interface and the like of all model component libraries and simulation engine versions on the assembled model are mainly tested.
S5: and storing the simulation model subjected to the test into the simulation application model database, and analyzing the information of the simulation model by a simulation engine.
Specifically, after the simulation model is assembled, it needs to be parsed by the simulation engine. It is therefore necessary to store the assembled simulation model. The selection is stored in the form of database records in an assembly table, which contains model basic information, assembly component basic information, assembly name, assembly position and the like.
In particular, according to the present embodiment, the procedure described in the above flowcharts may be implemented as a computer software program. For example, the present embodiments include a computer program product comprising a computer program tangibly embodied on a computer-readable medium, the computer program containing program code for performing the method shown in the flowchart. In such embodiments, the computer program may be downloaded and installed from a network via a communication portion, and/or installed from a removable medium.
The flowcharts and diagrams in the figures illustrate the architecture, functionality, and operation of possible implementations of systems, methods and computer program products according to the present embodiments. In this regard, each block in the flowchart or schematic 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 shown 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 diagrams and/or flowchart illustration, and combinations of blocks in the 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 modules involved in the present embodiment may be implemented in software or in hardware. The described modules may also be provided in a processor.
On the other hand, the present embodiment also provides a nonvolatile computer storage medium, which may be the nonvolatile computer storage medium included in the apparatus in the above embodiment or may be a nonvolatile computer storage medium existing separately and not incorporated in the terminal.
In the description of the present invention, it should be noted that the azimuth or positional relationship indicated by the terms "upper", "lower", etc. are based on the azimuth or positional relationship shown in the drawings, and are merely for convenience of describing the present invention and simplifying the description, and are not indicative or implying that the apparatus or element in question must have a specific azimuth, be constructed and operated in a specific azimuth, and thus should not be construed as limiting the present invention. Unless specifically stated or limited otherwise, the terms "mounted," "connected," and "coupled" are to be construed broadly, and may be, for example, fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; can be directly connected or indirectly connected through an intermediate medium, and can be communication between two elements. The specific meaning of the above terms in the present invention can be understood by those of ordinary skill in the art according to the specific circumstances.
It is further noted that in the description of the present invention, relational terms such as first and second, and the like are used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Moreover, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus. Without further limitation, an element defined by the phrase "comprising one … …" does not exclude the presence of other like elements in a process, method, article, or apparatus that comprises the element.
It should be understood that the foregoing examples of the present invention are provided merely for clearly illustrating the present invention and are not intended to limit the embodiments of the present invention, and that various other changes and modifications may be made therein by one skilled in the art without departing from the spirit and scope of the present invention as defined by the appended claims.
Claims (10)
1. A multi-level componentized model architecture method, the method comprising:
defining and storing model basic data, model performance parameters, model expected parameters and model interaction information of a model component, and constructing a multi-level simulation model architecture to obtain a basic model component database;
and assembling the model components in the basic model component database through assembly simulation model assembly combinations to obtain a simulation application model, and storing the simulation application model in the simulation application model database.
2. The method of claim 1, wherein the step of determining the position of the substrate comprises,
the multi-level simulation model architecture defines assembly combination rules;
the assembly and combination of the componentized simulation models are that models with repeatability, cross-field and heterogeneous characteristics in model components are combined through an assembly mechanism and a style;
the simulation application model comprises a simulation application model assembled by a basic model component and a simulation application model directly serving application system construction.
3. The method of claim 1, wherein the multi-level simulation model architecture comprises
The first layer is a solid-level model component of a base class in the multi-level simulation model architecture;
the second layer is a platform-level model component and a component-level model component which inherit the base class in the multi-level simulation model architecture;
the third hierarchy includes a platform level subdivision model assembly inheriting the platform level model assembly, and a component level subdivision model assembly inheriting the component level model assembly.
4. The method of claim 3, wherein the multi-level simulation model architecture comprises at least one of:
parameters of the entity-level model component include the size, weight and country of the model;
parameters of the platform-level model component include platform customization parameters, average travel speed, and maximum travel speed;
parameters of the component level model assembly include size, weight and country of the model;
the platform level subdivision model includes
An aircraft solid model, a ship solid model, a vehicle solid model, a weapon solid model, a satellite solid model, and a ground facility solid model;
the component level subdivision model includes
Sensor models, communication models, interference models, ammunition library models, rack models, and resource center models.
5. The method of claim 4, wherein the assembly combining rule is,
the entity-level model component, the platform-level model component, and the model component subdivided by the platform-level model component are capable of assembling the component-level model component;
the component-level model assembly and the model assembly of the component-level model assembly subdivision cannot be assembled with each other.
6. A multi-level componentized model assembly system, characterized in that it is based on a multi-level componentized model system obtained by the architecture method according to any one of claims 1 to 5, said system comprising:
the scheme management unit is used for configuring schemes by users;
the model component management unit is used for managing the basic model components in the basic model component database;
the model assembly module is used for providing all the model assembly information capable of being assembled in the scheme for a user to select according to the assembly combination rule of the multi-level componentization model system architecture;
the model test module is used for testing the suitability of all model components and simulation engine versions on the assembled simulation application model through the iterative check verification of models among different levels, and initializing and rationality of model interfaces;
the basic model component database is used for storing basic model components, can automatically create a table structure of the model components according to a multi-level componentization model system architecture when a user performs scheme design, and responds to the operations of adding, deleting, modifying and inquiring the records of the basic model component database by the user;
and the simulation application model database is used for storing the simulation application models tested by the model test module.
7. The system of claim 6, wherein the configuration scheme includes model components, models, parts, and assembly information.
8. The system of claim 6, wherein managing the model component includes constructing parameters of the model component, creation, modification, or deletion of model component models, and import and export of model component model data.
9. The system of claim 6, the model component management unit comprises
The parameter construction module is used for supporting a user to add, modify or delete performance parameters of the model component;
the performance parameters include basic information of the model component including name, unit, default, and data type.
10. A method of assembling based on the assembly system of any one of claims 6 to 9, the method comprising:
s1: publishing the basic component database outwards;
s2: managing basic model components in a basic model component database, and configuring a scheme;
s3: according to the information of all the model components which can be assembled in the scheme provided by the assembly system, selecting the model components for combined assembly to obtain a simulation model with a complex model;
s4: testing the suitability of the simulation model and the version of the simulation engine, initialization and rationality of a model interface;
s5: and storing the simulation model subjected to the test into the simulation application model database, and analyzing the information of the simulation model by a simulation engine.
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