CN111400872A - Model-based avionics system virtual integration test method and system - Google Patents
Model-based avionics system virtual integration test method and system Download PDFInfo
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Abstract
A model-based avionics system virtual integration test method and system comprises the following steps: receiving a designed system architecture; generating a virtual test component model framework according to the system architecture, wherein the virtual test component model framework is used for realizing and delivering virtual test components by a model supplier; receiving a virtual test component model, wherein the virtual test component model is obtained by carrying out virtual test component realization and delivery on a virtual test component model framework by a model supplier; and generating an executable test file according to the virtual test component model integrated configuration, wherein the executable test file is used for the system architecture to run virtual test execution of different scenes. And the digital simulation and comprehensive verification of the avionic system are completed, so that the automation degree of the simulation verification is improved, and the development period is shortened.
Description
Technical Field
The invention relates to the technical field of virtual integration test of avionics systems, in particular to a model-based virtual integration test method and system of an avionics system.
Background
Traditionally, manual coding is generally completed in a software-in-loop mode, so that a digital avionics system simulation verification system is established; the hardware-in-loop test is an integrated test method based on a hardware test bench carrying software in a loop, and is widely applied to the field of airborne system test. When a system integrator obtains equipment from an equipment or subsystem supplier, the integration of a plurality of pieces of equipment is needed to be completed, and whether interfaces and interactive logics among the equipment meet design requirements or not is verified; then, the system function requirements are used as input for the system which completes the synthesis, and the system level functions are tested item by item to verify whether the system which completes the synthesis meets the design requirements.
An avionics system is a special field, is different from structures, materials and the like, and needs to test the functions and logic characteristics of the avionics system in an important way. The existing tool software focuses on researching the physical characteristics of system testing, but tools aiming at the special functional and logical characteristics of the avionic system are very rare, and the conventional tool cannot realize the early verification testing method of the model-based avionic system.
Meanwhile, the existing test method has many limitations, such as: the complexity of modern aircraft avionics systems is rapidly rising, hundreds of thousands of avionics systems with data buses are extremely large in terms of signal data interaction, and the traditional means is more effective when the demand is rapidly changed and system faults are continuously generated. In the process of system synthesis and verification in hardware loop test, the problems of large test quantity of electronic interface communication protocols, low manual test efficiency, complex dynamic cross-linking of system integration verification and the like need to be solved. Meanwhile, in the ring test of all models at the present stage, the closed-loop test is mostly performed on a single model such as Simulink and the like, and the method has the limitation of single model type and is difficult to integrate.
Therefore, the traditional ring-in-the-loop test method for hardware, software or models cannot meet the early verification test of the avionics system aiming at the verification requirement.
Disclosure of Invention
Objects of the invention
The invention aims to provide a model-based avionics system virtual integration test method and system, which are used for completing digital simulation and comprehensive verification of an avionics system so as to improve the automation degree of simulation verification and shorten the development period.
(II) technical scheme
In order to solve the above problem, according to an aspect of the present invention, there is provided a model-based avionics system virtual integration test method, including: receiving a designed system architecture; generating a virtual test component model framework according to the system architecture, wherein the virtual test component model framework is used for realizing and delivering virtual test components by a model supplier; receiving a virtual test component model, wherein the virtual test component model is obtained by carrying out virtual test component realization and delivery on a virtual test component model framework by a model supplier; and generating an executable test file according to the virtual test component model integrated configuration, wherein the executable test file is used for the system architecture to run virtual test execution of different scenes.
Further, generating a virtual test component model framework from the system architecture includes: defining a virtual test system simulation architecture according to the system architecture; defining a boundary according to a virtual test system simulation framework, and generating a virtual test component interface according to the defined boundary; and generating a virtual test component model framework according to the virtual test component interface.
Further, receiving a virtual test component model, wherein the virtual test component model is obtained by a model provider implementing and delivering a virtual test component to a virtual test component model framework, and the virtual test component model comprises: customizing the interior of the virtual testing component model frame to obtain a virtual component testing model; and carrying out delivery test on the virtual component test model, judging whether the virtual component test model meets the delivery standard, and receiving the virtual component test model meeting the standard.
Further, generating the executable test file according to the virtual test component model integrated configuration includes: defining a virtual test system simulation architecture according to the system architecture; converting the system architecture into a simulation architecture according to the virtual test system simulation architecture; and generating an executable test file by combining the simulation architecture and the virtual test component model integrated configuration.
Further, generating an executable test file by combining the simulation architecture and the virtual test component model integrated configuration includes: integrating the simulation architecture and the virtual test component model, and converting the simulation model into executable dynamic test model configuration; distributing hardware testing resources; the executable dynamic test model configuration is automatically connected to the hardware test resources to generate an executable test file.
Further, the executable test file is used for the system architecture to run virtual test execution of different scenarios, and the executable test file comprises: and performing virtual test execution on the executable test file based on the operation scenes of different system architectures.
According to another aspect of the present invention, there is provided a model-based avionics system virtual integration test system, comprising: a total design team module for designing a system architecture; the virtual integrated test module is used for receiving a designed system architecture and generating a virtual test component model framework according to the system architecture; the model supplier module is used for realizing and delivering the virtual test component to the virtual test component model framework to obtain a virtual test component model; the virtual integrated test module is also used for receiving the virtual test component model and generating an executable test file according to the virtual test component model integrated configuration; the total design team module is also used for performing virtual test execution on the executable test file.
Further, the overall design team module includes: a system architecture design unit for designing a system architecture; the test execution unit is used for performing virtual test execution on the executable test file; and the operation scene conversion unit is used for converting different operation scenes according to the system architecture, so that the test execution unit performs virtual test execution on the executable test file based on the different operation scenes.
Further, the virtual integration test module comprises: the simulation architecture building unit is used for defining a virtual test system simulation architecture according to the system architecture and converting the system architecture into a simulation architecture according to the virtual test system simulation architecture; the test frame generation unit is used for defining a boundary according to the virtual test system simulation framework, generating a virtual test component interface according to the defined boundary, and finally generating a virtual test component model frame according to the virtual test component interface; the virtual component testing model is also used for receiving the standard-meeting virtual component testing model; and the integrated configuration unit is used for integrating the simulation architecture and the virtual test component model, converting the simulation model into executable dynamic test model configuration, automatically connecting the executable dynamic test model configuration to the hardware test resources after the hardware test resources are distributed, and generating an executable test file.
Further, the model provider module includes: the virtual test component implementation unit is used for customizing the virtual test component model framework to obtain an implemented virtual component test model; and the virtual testing component delivery testing unit is used for carrying out delivery testing on the virtual testing component model and judging whether the virtual testing component model meets the delivery standard.
(III) advantageous effects
The technical scheme of the invention has the following beneficial technical effects:
1. compared with the traditional test method, the method really realizes the simulation integration of multiple models, realizes the modeled transmission in the whole life cycle in the test process, can trace back in two directions with the top-level requirement, and simultaneously can provide input reference for the design stage to realize the transmission process based on the models.
2. The method belongs to a customized method for testing the avionic system, realizes early integrated verification of avionic system functions and logic, and solves a series of problems of low testing efficiency, poor feasibility of complex interface cross-linking testing and the like of traditional hardware and software in-loop testing due to complexity of the avionic system and specificity of early verification.
3. Compared with the traditional model-in-loop testing method, the method breaks through the limitation of the model on the type requirement in the loop testing process, really realizes the integrated verification support of multiple models, and simultaneously, the system for supporting the verification testing method has the characteristic of being capable of automatically generating a frame, so that the problems caused by artificial interface connection and coding in the traditional mode are solved.
4. Meanwhile, a relatively complete personnel division and team architecture required for completing the verification method and the verification process is provided, and the method can be used as a reference basis for dividing the position responsibility of scientific research personnel in future large-scale popularization and implementation.
Drawings
FIG. 1 is a flow chart illustrating the steps of a method for testing virtual integration of an avionics system based on a model according to the present invention;
FIG. 2 is a flowchart of step S2 provided by the present invention;
FIG. 3 is a flowchart of step S3 provided by the present invention;
FIG. 4 is another flowchart of step S3 provided by the present invention;
FIG. 5 is a flowchart of step S43 provided by the present invention;
fig. 6 is a block diagram of a virtual integration test system of an avionics system based on a model according to the present invention.
Reference numerals:
100-total design team module; 101-system architecture design unit; 102-running scene conversion unit; 103-a test execution unit;
200-a virtual integrated test module; 201-a simulation architecture building unit; 202-a test framework generation unit; 203-integrated configuration unit; 204-model integration; 205-hardware test resource allocation; 206-model configuration;
300-model supplier module; 301-a virtual test component implementation unit; 302-virtual test component delivery test unit; 303-virtual components implement the modification iteration unit.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention more apparent, the present invention will be described in further detail with reference to the accompanying drawings in conjunction with the following detailed description. It should be understood that the description is intended to be exemplary only, and is not intended to limit the scope of the present invention. Moreover, in the following description, descriptions of well-known structures and techniques are omitted so as to not unnecessarily obscure the concepts of the present invention.
The present invention will be described in detail below with reference to the accompanying drawings and examples.
Fig. 1 is a flowchart illustrating steps of a virtual integration testing method for model-based avionics systems according to the present invention.
Referring to fig. 1, the present invention provides a model-based avionics system virtual integration test method, which includes the following steps:
s1: a designed system architecture is received.
S2: and generating a virtual test component model framework according to the system architecture, wherein the virtual test component model framework is used for realizing and delivering the virtual test component by a model supplier.
S3: and receiving a virtual test component model, wherein the virtual test component model is obtained by carrying out virtual test component realization and delivery on the virtual test component model framework by a model supplier.
S4: and generating an executable test file according to the virtual test component model integrated configuration, wherein the executable test file is used for the system architecture to run virtual test execution of different scenes.
The application includes:
the general design team is mainly responsible for designing a system architecture and executing executable test files of virtual tests;
the verification design team is mainly responsible for the definition of the test method and the range definition of the test system;
the virtual component management team is mainly responsible for providing a virtual test component model framework for a model supplier and butting a virtual test component model obtained by the supplier realization and delivery;
the test integration team is mainly responsible for generating executable test files according to the virtual test component model integration configuration;
and the model supplier is mainly responsible for realizing and delivering the virtual test component.
The complete personnel division and team architecture provides a reference basis for scientific research personnel to divide the station responsibility in future large-scale popularization and implementation.
Fig. 2 is a flowchart of step S2 provided by the present invention, specifically, please refer to fig. 2, step S2 includes:
s21: defining a virtual test system simulation architecture according to the system architecture;
s22: defining a boundary according to a virtual test system simulation framework, and generating a virtual test component interface according to the defined boundary;
s23: and generating a virtual test component model framework according to the virtual test component interface.
Specifically, a virtual test system simulation architecture is defined according to a system architecture provided by a general design team, and finally generated executable test files are also tested and executed through the general design team, so that a bidirectional tracing effect is achieved.
Meanwhile, the boundary definition refers to defining the boundary of a virtual test component interface, the virtual test component interface is derived from a design model, and only one design model is needed when a simulation framework is generated, so that not all interfaces need to be tested, and only an interested interface needs to be selected for testing. Therefore, before generating the virtual test component interface, the boundary of the virtual test component interface needs to be defined, and then the virtual test component interface is generated according to the defined boundary.
Specifically, defining the virtual test system simulation architecture according to the system architecture comprises defining the external environment of the virtual test system, and editing and perfecting the system architecture.
Fig. 3 is a flowchart of step S3 provided by the present invention, specifically, please refer to fig. 3, step S3 includes:
s31: customizing the interior of the virtual testing component model frame to obtain a virtual component testing model;
s32: and carrying out delivery test on the virtual component test model, judging whether the virtual component test model meets the delivery standard, and receiving the virtual component test model meeting the standard.
Specifically, the generated virtual test component model framework is actually a C-code program, and the code defines and encapsulates all interfaces in the virtual test component model framework, and simultaneously reserves a part of space for programming implementation, so that programming implementation, i.e., customized implementation, can be performed inside the virtual test component model framework without considering interface connection, and mainly can be performed according to the structure and function of the virtual test component model framework.
And the delivery standard is judged according to the system architecture and the simulation architecture, and the virtual component test model which cannot meet the requirements of the system and the design team is correspondingly modified and iterated and then is judged whether to reach the delivery standard.
Fig. 4 is another flowchart of step S3 provided by the present invention, preferably, please refer to fig. 4, wherein step S3 further includes:
s31: customizing the interior of the virtual testing component model frame to obtain a virtual component testing model;
s32: deliver test the virtual component test model and determine if the virtual component test model meets the delivery criteria?
S33: if the delivery standard is met, receiving a virtual component test model meeting the standard;
if the virtual component test model does not meet the delivery standard, the virtual component test model which does not meet the standard is not received, the delivery test is carried out after the corresponding modification iteration is carried out on the virtual component test model which does not meet the standard, and whether the virtual component test model meets the delivery standard or not is judged.
Specifically, step S4 includes:
s41: defining a virtual test system simulation architecture according to the system architecture;
s42: converting the system architecture into a simulation architecture according to the virtual test system simulation architecture;
s43: and generating an executable test file by combining the simulation architecture and the virtual test component model integrated configuration.
Specifically, after receiving the virtual component test model meeting the delivery standard, the virtual component test model in multiple disciplines and multiple fields can be effectively integrated under a top-level framework based on the simulation architecture. Meanwhile, corresponding technicians need to build a virtual integrated test hardware environment according to the performance requirements of the system and the requirements of corresponding system hardware resources, so that the configuration generation of the virtual component test model is completed.
The configuration contains corresponding interface and internal functional structure information, and can be directly used as an executable test file.
Before completing the configuration generation of the virtual component test model, hardware test resources are also required to be allocated, preferably, fig. 5 is a flowchart of step S43 provided by the present invention, please refer to fig. 5, where the step S43 further includes the following steps:
s431: integrating the simulation architecture and the virtual test component model, and converting the simulation model into executable dynamic test model configuration;
s432: distributing hardware testing resources;
s433: the executable dynamic test model configuration is automatically connected to the hardware test resources to generate an executable test file.
Specifically, for an implemented virtual component test model, the simulation model needs to be converted into an executable dynamic test model configuration through virtual verification, and the configuration can be automatically imported into a test platform for simulation test and can automatically connect hardware resources on the simulation test platform.
In one embodiment, the executable test file is used for virtual test execution of a system architecture running different scenes, and comprises the following steps: and performing virtual test execution on the executable test file based on the operation scenes of different system architectures.
Specifically, after receiving an executable test file, an overall design team completes early integrated verification test of the model in the ring avionics system based on different operation scenes, realizes rapid prototyping evaluation of the model and effective balance verification of system alternatives, and provides design input for a realization stage in real system development; meanwhile, the test device can be used as an effective test component for hybrid verification, and provides early verification support for the system integration stage.
Preferably, the virtual test execution of the executable test file by the overall design team comprises the following steps:
receiving an executable test file;
converting different operation scenes based on different designed system architectures;
and performing virtual test execution on the executable test file.
Fig. 6 is a block diagram of a virtual integration test system of an avionics system based on a model according to the present invention.
Referring to fig. 6, a model-based avionics system virtual integration test system corresponding to the above method includes: an overall design team module 100, a virtual integration test module 200, and a model supplier module 300.
The overall design team module 100 is used to design the system architecture and perform virtual test execution on the executable test files.
The virtual integrated test module 200 is configured to receive a designed system architecture, and generate a virtual test component model frame according to the system architecture; and meanwhile, the virtual testing component model is received, and an executable testing file is generated according to the virtual testing component model integrated configuration.
The model supplier module 300 is configured to implement and deliver a virtual test component to the virtual test component model framework, so as to obtain a virtual test component model.
The model-based avionics system virtual integration test method and system are mainly carried out through the following three parts:
(1) system architecture design input and virtual test execution directed by the overall design team module 100.
(2) The model-based avionics system virtual integrated test module 200 is used for building a simulation framework on the system, automatically generating a virtual test model framework and configuring model integrated test resources.
(3) The virtual test component model with internal implementation is implemented and delivered by the model provider module 300.
The three modules have stronger coupling performance and can be traced back in a two-way mode. While the verification environment of the virtual integration test module 200 depends on the iterative inputs of the overall design team module 100 and the model vendor module 300.
In one embodiment, the overall design team module 100 includes: a system architecture design unit 101, a test execution unit 103 and an operation scenario conversion unit 102.
The system architecture design unit 101 is used for designing a system architecture; the test execution unit 103 is configured to perform virtual test execution on an executable test file; the operation scenario conversion unit 102 is configured to convert different operation scenarios according to the system architecture, so that the test execution unit performs virtual test execution on the executable test file based on the different operation scenarios.
In one embodiment, the virtual integration test module 200 includes: the simulation architecture building unit 201, the test framework generating unit 202 and the integrated configuration unit 203.
The simulation architecture building unit 201 is configured to define a virtual test system simulation architecture according to the system architecture, and convert the system architecture into a simulation architecture according to the virtual test system simulation architecture.
The test frame generation unit 202 is configured to perform boundary definition according to the virtual test system simulation framework, generate a virtual test component interface according to the defined boundary, and finally generate a virtual test component model frame according to the virtual test component interface, and transmit the virtual test component model frame to the model provider module 300 for implementation; the test framework generation unit 202 is further configured to receive a standard-compliant virtual component test model.
The integration configuration unit 203 is configured to integrate the simulation architecture and the virtual test component model, convert the simulation model into an executable dynamic test model configuration, and automatically connect the executable dynamic test model configuration to the hardware test resource after the hardware test resource is allocated, thereby generating an executable test file. And transmits the executable test file to the test execution unit 103, and finally completes the virtual test and verification process based on the model.
In one embodiment, model provider module 300 includes: a virtual test component implementation unit 301 and a virtual test component delivery test unit 302.
The virtual test component implementation unit 301 is configured to implement customization on a virtual test component model framework to obtain an implemented virtual component test model;
the virtual testing component delivery testing unit 302 is configured to perform delivery testing on the virtual testing component model, and determine whether the virtual testing component model meets a delivery standard.
Preferably, the model provider module 300 further comprises: the virtual component implementation modification iteration unit 303 receives a virtual component test model meeting the delivery standard if the virtual component implementation modification iteration unit meets the delivery standard; if the virtual component test model does not meet the delivery standard, the virtual component test model which does not meet the standard is not received, and the virtual component implementation modification iteration unit 303 is used for performing corresponding modification iteration on the virtual component test model which does not meet the standard and then performing delivery test, and judging whether the virtual component test model meets the delivery standard.
Specifically, the virtual integration test module 200 may capture a system architecture from the design input of the total design team module 100, and the virtual integration test module 200 and its function are defined by the simulation architecture building unit 201 according to the system architecture.
Preferably, the above definition includes defining the external environment of the virtual integrated test module 200, editing and perfecting the system architecture; and defining a simulation test boundary, and automatically generating a virtual test component interface according to the defined test boundary.
The simulation architecture building unit 201 can recognize the system architecture input from the total design team module 100 according to the defined simulation architecture, and realize the automatic generation of the virtual test component interface and the virtual test component model framework based on the C code.
The virtual test component model framework can inherit the simulation framework of the virtual integration test module 200 and map the system framework input by the total design team module 100. Meanwhile, the virtual test component model framework can be delivered to the model supplier module 300 for further implementation, and the implementation of the model-based early-stage to-be-tested component is completed.
The model supplier module 300 customizes the interior of the virtual test component model framework transferred by the virtual integrated test module 200, and mainly can implement code level implementation according to the structure and function of the virtual test component model framework, and meanwhile, the delivery condition of the model supplier module 300 judges with reference to the designed system framework and simulation framework, and for the implementation model which cannot meet the requirements of the system and design team, the model supplier module 300 transfers the implementation model to the virtual integrated test module 200 after corresponding modification iteration is performed by the virtual component implementation iteration unit 303.
The virtual integration test module 200 receives the virtual test component model implemented by the model provider module 300, and under the top-level framework based on the simulation architecture, can effectively integrate the multidisciplinary and multi-domain virtual integration component model.
Preferably, the integrated configuration unit 203 includes: model integration 204, hardware test resource allocation 205, and model configuration 206.
Model integration 204 is used to integrate the simulation architecture and the virtual test component model, converting the simulation model into an executable dynamic test model configuration.
The hardware test resource allocation 205 is used to allocate hardware test resources.
Model configuration 206 is used to automatically connect the executable dynamic test model configuration to the hardware test resources, generating an executable test file.
Meanwhile, the allocation 205 of hardware testing resources also includes the definition of the connection relationship of the interfaces and the allocation of hardware testing resources. According to the performance requirements of the system and the requirements of hardware resources of the corresponding system, corresponding technicians build a virtual integrated test hardware environment to carry the model-based avionics system virtual integrated test system, so that the configuration generation of the object to be tested is completed, the configuration contains the interface and internal functional structure information of the corresponding model, and the interface and internal functional structure information can be directly used as executable test resources.
The invention aims to protect a model-based avionics system virtual integration test method and system, and the method comprises the following steps: receiving a designed system architecture; generating a virtual test component model framework according to the system architecture, wherein the virtual test component model framework is used for realizing and delivering virtual test components by a model supplier; receiving a virtual test component model, wherein the virtual test component model is obtained by carrying out virtual test component realization and delivery on a virtual test component model framework by a model supplier; and generating an executable test file according to the virtual test component model integrated configuration, wherein the executable test file is used for the system architecture to run virtual test execution of different scenes.
It is to be understood that the above-described embodiments of the present invention are merely illustrative of or explaining the principles of the invention and are not to be construed as limiting the invention. Therefore, any modification, equivalent replacement, improvement and the like made without departing from the spirit and scope of the present invention should be included in the protection scope of the present invention. Further, it is intended that the appended claims cover all such variations and modifications as fall within the scope and boundaries of the appended claims or the equivalents of such scope and boundaries.
Claims (10)
1. A virtual integration test method of an avionics system based on a model is characterized by comprising the following steps:
receiving a designed system architecture;
generating a virtual test component model framework according to the system architecture, wherein the virtual test component model framework is used for realizing and delivering virtual test components by a model supplier;
receiving a virtual test component model, wherein the virtual test component model is obtained by a model supplier performing virtual test component realization and delivery on the virtual test component model framework;
and generating an executable test file according to the virtual test component model integrated configuration, wherein the executable test file is used for the system architecture to run virtual test execution of different scenes.
2. The method of claim 1, wherein generating a virtual test component model framework from the system architecture comprises:
defining a virtual test system simulation architecture according to the system architecture;
defining a boundary according to the virtual test system simulation framework, and generating a virtual test component interface according to the defined boundary;
and generating the virtual test component model framework according to the virtual test component interface.
3. The method of claim 1,
receiving a virtual test component model, wherein the virtual test component model is obtained by a model provider through virtual test component implementation and delivery of the virtual test component model framework, and the virtual test component model comprises:
customizing the interior of the virtual testing component model frame to obtain a virtual testing component model;
and carrying out delivery test on the virtual component test model, judging whether the virtual component test model meets the delivery standard, and receiving the virtual component test model meeting the standard.
4. The method of claim 1, wherein generating an executable test file from the virtual test component model integration configuration comprises:
defining a virtual test system simulation architecture according to the system architecture;
converting the system architecture into a simulation architecture according to the virtual test system simulation architecture;
and generating an executable test file by combining the simulation architecture and the virtual test component model integrated configuration.
5. The method of claim 4,
generating an executable test file by combining the simulation architecture and the virtual test component model integrated configuration comprises the following steps:
integrating the simulation architecture and the virtual test component model, and converting a simulation model into an executable dynamic test model configuration;
distributing hardware testing resources;
the executable dynamic test model configuration is automatically connected to the hardware test resources to generate an executable test file.
6. The method of claim 1,
the executable test file is used for the system architecture to run virtual test execution of different scenes and comprises the following steps:
and performing virtual test execution on the executable test file based on different operation scenes of the system architecture.
7. A model-based avionics system virtual integration test system, comprising:
a total design team module for designing a system architecture;
the virtual integrated test module is used for receiving the designed system architecture and generating a virtual test component model framework according to the system architecture;
the model supplier module is used for realizing and delivering the virtual test component to the virtual test component model framework to obtain the virtual test component model;
the virtual integrated test module is also used for receiving the virtual test component model and generating an executable test file according to the virtual test component model integrated configuration;
the total design team module is also used for performing virtual test execution on the executable test file.
8. The system of claim 7, wherein the overall design team module comprises:
a system architecture design unit for designing the system architecture;
the test execution unit is used for performing virtual test execution on the executable test file;
and the operation scene conversion unit is used for converting different operation scenes according to the system architecture, so that the test execution unit performs virtual test execution on the executable test file based on different operation scenes.
9. The system of claim 7, wherein the virtual integration test module comprises:
the simulation architecture building unit is used for defining a virtual test system simulation architecture according to the system architecture and converting the system architecture into a simulation architecture according to the virtual test system simulation architecture;
the test frame generating unit is used for defining the boundary according to the virtual test system simulation framework, generating a virtual test component interface according to the defined boundary and finally generating the virtual test component model frame according to the virtual test component interface;
the virtual component testing model is also used for receiving the standard-meeting virtual component testing model;
and the integrated configuration unit is used for integrating the simulation architecture and the virtual test component model, converting the simulation model into executable dynamic test model configuration, automatically connecting the executable dynamic test model configuration to the hardware test resources after the hardware test resources are distributed, and generating an executable test file.
10. The system of claim 7, wherein the model provider module comprises:
the virtual test component implementation unit is used for customizing the virtual test component model framework to obtain an implemented virtual component test model;
and the virtual testing component delivery testing unit is used for carrying out delivery testing on the virtual component testing model and judging whether the virtual component testing model meets the delivery standard.
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