CN117435565A - Full life cycle management method for development source data of flight training simulator - Google Patents

Full life cycle management method for development source data of flight training simulator Download PDF

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CN117435565A
CN117435565A CN202311305813.7A CN202311305813A CN117435565A CN 117435565 A CN117435565 A CN 117435565A CN 202311305813 A CN202311305813 A CN 202311305813A CN 117435565 A CN117435565 A CN 117435565A
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source data
development
nas
files
data
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杨永华
于丽丽
谌杰辉
胡宇强
贾志艳
王勇
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South China Aircraft Industry Co Ltd of China Aviation Industry General Aircraft Co Ltd
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South China Aircraft Industry Co Ltd of China Aviation Industry General Aircraft Co Ltd
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    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F16/00Information retrieval; Database structures therefor; File system structures therefor
    • G06F16/10File systems; File servers
    • G06F16/16File or folder operations, e.g. details of user interfaces specifically adapted to file systems
    • G06F16/168Details of user interfaces specifically adapted to file systems, e.g. browsing and visualisation, 2d or 3d GUIs
    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F16/00Information retrieval; Database structures therefor; File system structures therefor
    • G06F16/10File systems; File servers
    • G06F16/13File access structures, e.g. distributed indices
    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F16/00Information retrieval; Database structures therefor; File system structures therefor
    • G06F16/10File systems; File servers
    • G06F16/18File system types
    • G06F16/1873Versioning file systems, temporal file systems, e.g. file system supporting different historic versions of files

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  • Databases & Information Systems (AREA)
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  • General Engineering & Computer Science (AREA)
  • General Physics & Mathematics (AREA)
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  • Management, Administration, Business Operations System, And Electronic Commerce (AREA)

Abstract

The invention provides a full life cycle management method for development source data of a flight training simulator, which comprises the steps of obtaining a development source data list of the flight training simulator; confirming the required files or the unique data sources corresponding to the digital and analog one by one in a PDM system; constructing a NAS system, storing required data in the NAS system according to a developed source data list, and building a source data structure tree; establishing an association relationship between source data files stored in the NAS system and corresponding file data in the PDM system one by one; creating an NAS system using an account number and an access address; creating a source data change tracking table in the system, and displaying the related attribute information of the data items in the form of a two-dimensional matrix; the changed source data item is highlighted on the source data structure tree. The invention can automatically track engineering changes of design source data cited by FFS development, and realize scientific management of full life cycle changes of source data, thereby improving timeliness and accuracy and avoiding the problem that FFS configuration is inconsistent with a true mechanism type.

Description

Full life cycle management method for development source data of flight training simulator
Technical Field
The invention relates to the technical field of configuration management of a large-scale aircraft flight training simulator, in particular to a full life cycle management method for development source data of the flight training simulator.
Background
An aircraft flight training simulator (FFS below for short) belongs to flight simulation training equipment, is mainly used for pilot flight training and can also be used for engineering verification, wherein the FFS is a vision system which is duplicated in a one-to-one correspondence mode according to aircraft types and cabins, can provide various flight scenes and a motion system which can provide dynamic sense, and is divided into four grades A, B, C and D according to CCAR-60 regulations, namely, flight simulation training equipment management and operation rules. The class D FFS can basically realize the training of all flying subjects, greatly reduce the cost of flying training and improve the safety, can be used for T5 test in the development AEG evaluation (aircraft evaluation) of a large-scale aircraft, and can accelerate the evidence collection progress and reduce the evidence collection cost.
Flight training simulators require extremely high performance fidelity to the aircraft being simulated, with the key to performance fidelity being the mature, complete flight simulator data package. The integrity and the accuracy of the simulation system determine the fidelity of the simulation system in the aspects of airplane system functions, flight characteristics, sensory prompts and the like, so that the quality of flight training and the safety of flight operation are affected.
Therefore, the full life cycle management of FFS development source data is urgently needed, the accuracy and timeliness of source data engineering change transmission are guaranteed, the consistency of FFS and aircraft configuration states is achieved, and the purposes of high quality and high efficiency of flight training are achieved.
The current method is to transfer and track the change manually, and the method is time-consuming and labor-consuming, especially easy to change omission, unable to ensure the accuracy of source data used by FFS, and easy to cause the problem that FFS configuration is inconsistent with that of a true institution, thereby affecting the effectiveness of aircraft evidence collection and pilot training.
Disclosure of Invention
The invention aims to provide a full life cycle management method for developing source data of a flight training simulator, which can automatically track engineering changes of design source data cited by FFS development and realize a scientific management method for the full life cycle changes of the source data, thereby improving timeliness and accuracy and avoiding the problem that FFS configuration is inconsistent with a true organization.
The invention provides a full life cycle management method for developing source data of a flight training simulator, which comprises the following steps: acquiring a development source data list of a flight training simulator;
confirming the required files or the unique data sources corresponding to the digital and analog one by one in a PDM system based on the development source data list;
building a NAS system, storing the required three-dimensional digital-analog, files and other data in the NAS system according to the development source data list, and building a source data structure tree;
establishing an association relation between source data files stored in the NAS system and corresponding file data in the PDM system one by one to realize the synchronization of the source data files of the NAS system and the corresponding file versions of the PDM system;
creating an NAS system, using an account number and an access address, and logging in and looking up a required file through the access address and the account number;
developing a source data change visual management system by a development simulator, creating a source data change tracking table in the system, and displaying related attribute information of data items such as digital models, files and the like in a two-dimensional matrix form;
and highlighting the changed source data item on the source data structure tree, so as to realize the closed-loop management of engineering source data change and ensure the consistency of the simulator and the state of a true machine.
According to the full life cycle management method for the development source data of the flight training simulator, the method for acquiring the development source data list of the flight training simulator comprises the following steps:
and according to the development requirement scheme and the development target of the aircraft flight training simulator, the aircraft engineering design source data required by the development process of the simulator are arranged to form a development source data list.
According to the full life cycle management method for the development source data of the flight training simulator, when the development source data list is determined, the source data range comprises three-dimensional digital-analog data for designing the structural appearance, the cockpit layout and the cockpit installation equipment of the simulator, and data for describing functions, principles, compositions and the like of each system; the source data types include three-dimensional modulus, CATPart/. CATProduct format files, and text descriptive files published in PDF format.
According to the full life cycle management method for the development source data of the flight training simulator, provided by the invention, the full life cycle engineering change of design source data quoted by the development of the flight training simulator is tracked and managed, files and three-dimensional digital models corresponding to the development source data list are required to be established in a PDM system to serve as unique data sources, the full life cycle update and version change of the source data are carried out according to the engineering change condition, and the linkage of the source data change is realized by establishing association between the development source data list and the data files corresponding to the PDM system.
According to the full life cycle management method for the development source data of the flight training simulator, when the NAS system is built, a source data structure tree is built in the NAS system according to a simulator development source data list in a hierarchical manner;
the NAS system establishes an interface with the PDM system, acquires and stores corresponding files from the PDM system according to a source data file list on a source data structure tree, and associates with corresponding source data files in the PDM system at the same time so as to ensure that the change of the source data files can be tracked; the NAS system is a server for storing source data files and difference data, the PDM system is a product data management system, design source data are stored in the NAS system, and the design source data are associated and stored with the PDM system source data files through the NAS system.
According to the full life cycle management method for developing source data of the flight training simulator, when the source data files stored in the NAS system and corresponding file data in the PDM system are in one-to-one association relation, the NAS system updates the source data structure tree of the system by reading the latest version information of the source data files in the PDM system, so that the structure tree files on the NAS are synchronous with the versions of the source data files corresponding to the PDM system, meanwhile, data change information is captured in the PDM system according to the source data file items listed in the source data structure tree, and a source data file difference analysis log table is generated in the NAS system.
According to the full life cycle management method for the flight training simulator development source data, when an account number and an access address are used for creating a NAS system, a required file is checked through the access address and the account number in a local area network range, or the required file is checked through an external network by using VPN.
According to the invention, the modification visual management system comprises:
a source data file item change tracking list is created in the system, and related attribute information such as numbers, names, data categories, model numbers/part numbers, required quantity, suppliers, release times, update time and the like are displayed in a table form.
According to the invention, the method for managing the full life cycle of the source data developed by the flight training simulator comprises the following steps of:
highlighting the data file with the engineering change source on the change tracking table by an informatization technical means so as to facilitate a researcher to track the engineering change of the whole life cycle of the source data; and referring to the source data file subjected to modification in the NAS system to evaluate, and confirming whether modification is implemented or not, and restoring normal display of the highlighted item through confirmation operation, so that engineering source data modification closed-loop management is realized, and the consistency of the simulator and the state of a true machine is ensured.
According to the full life cycle management method for developing source data of the flight training simulator, priority and expected response time are set for NAS systems corresponding to different source data;
allocating caches for each NAS system according to the priority, wherein the NAS system with high priority allocates large cache capacity and the NAS system with low priority allocates small cache capacity; and monitoring each NAS system in real time, judging whether the cache capacity of the corresponding NAS system is matched with the corresponding priority, judging whether the actual response time of the corresponding NAS system is matched with the expected response time, and if not, distributing the cache for each NAS system again.
Therefore, compared with the prior art, the method and the device can quickly, completely and accurately identify the source data engineering change, can realize automatic tracking, change evaluation and change closed-loop processing of the source data engineering change quoted by the aircraft flight training simulator, and further realize accurate management of the full-life configuration of the flight training simulator, thereby achieving the following beneficial effects:
1. the invention can intensively display all the source data quoted by FFS development according to the form of ATA chapter structure tree, which is convenient for FFS development staff to review relevant source data files, and the scattered source data files are collected together for management, thereby improving the working efficiency of development staff;
2. according to the invention, source data change information can be captured at regular time to generate the version difference log form, FFS (fringe field switching) researchers can refer to the difference log form to obtain the source data change information, so that the situation that whether a PDM system is changed or not is checked manually by each part by the researchers is avoided, and a large amount of labor cost is saved;
3. according to the invention, the highlighting of the source data item with the change and the restoration of the normal display after the change are completed are realized, the closed-loop management of the change process is explicit, the occurrence of the change of the source data without the FFS is avoided, and the integrity and the accuracy of the change are improved.
The invention is described in further detail below with reference to the drawings and the detailed description.
Drawings
FIG. 1 is a flow chart of an embodiment of a full life cycle management method for a flight training simulator development source data.
FIG. 2 is a schematic diagram of a first table of a list of development source data files for use in an embodiment of a full life cycle management method for a flight training simulator in accordance with the present invention.
FIG. 3 is a schematic diagram of a second table of a list of development source data files for use in an embodiment of a full life cycle management method for a flight training simulator in accordance with the present invention.
FIG. 4 is a schematic diagram of a tree of source data structures for use in an embodiment of a full life cycle management method for developing source data for a flight training simulator in accordance with the present invention.
FIG. 5 is a schematic diagram of explicit tracking of development source data changes in an embodiment of a full life cycle management method for a flight training simulator according to the present invention.
Detailed Description
For the purpose of making the objects, technical solutions and advantages of the present invention more apparent, the technical solutions of the present invention will be clearly and completely described below with reference to the accompanying drawings, and it is apparent that the described embodiments are some embodiments of the present invention, not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the invention without making any inventive effort, are intended to be within the scope of the invention.
Reference herein to "an embodiment" means that a particular feature, structure, or characteristic described in connection with the embodiment may be included in at least one embodiment of the present application. The appearances of such phrases in various places in the specification are not necessarily all referring to the same embodiment, nor are separate or alternative embodiments mutually exclusive of other embodiments. Those of skill in the art will explicitly and implicitly appreciate that the embodiments described herein may be combined with other embodiments.
First, some of the terms and related techniques referred to in the present application are explained for easy understanding by those skilled in the art.
The chinese name of PDM is product data management (Product Data Management), a technique used to manage all product-related information (including part information, configuration, documents, CAD files, structures, rights information, etc.) and all product-related processes (including process definition and management). By implementing the PDM, the production efficiency can be improved, the management of the whole life cycle of the product is facilitated, the efficient utilization of documents, drawings and data is enhanced, and the workflow is normalized. The PDM manufacturing process data document management system can effectively organize production operation documents such as production process cards, part blueprints, three-dimensional digital models, tool lists, quality files, digital control programs and the like of enterprises, and realizes paperless production of workshops.
The NAS (NetworkAttached Storage: network attached storage) is simply referred to as a network-connected device having a data storage function, and is also referred to as a "network storage". It is a dedicated data storage server. The method takes data as a center, thoroughly separates the storage equipment from the server, and centrally manages the data, thereby releasing bandwidth, improving performance, reducing total ownership cost and protecting investment. Its cost is far lower than using server storage, while its efficiency is far higher than the latter.
Referring to fig. 1, the invention provides a full life cycle management method for development source data of a flight training simulator, which comprises the following steps:
step S1, acquiring a development source data list of a flight training simulator;
step S2, confirming the required files or the unique data sources corresponding to the digital and analog one by one in a PDM system based on the development source data list;
step S3, building a NAS system, storing the required three-dimensional digital-analog, files and other data in the NAS system according to the development source data list, and building a source data structure tree so as to facilitate the simulator development personnel to review the required files;
step S4, establishing an association relation between the source data files stored in the NAS system and corresponding file data in the PDM system one by one, and realizing the version synchronization of the source data files of the NAS system and the corresponding files of the PDM system;
step S5, creating an NAS system, using an account number and an access address, and logging in and looking up a required file through the access address and the account number;
step S6, developing a source data change visual management system by a development simulator, creating a source data change tracking table in the system, and displaying related attribute information of data items such as digital models, files and the like in a two-dimensional matrix form;
and S7, highlighting the source data item with the change on the source data structure tree, so that a researcher can easily find the change item, evaluates the change and confirms whether the change is implemented, the engineering source data change closed-loop management is realized, and the consistency of the simulator and the state of a true machine is ensured.
In the step S1, a development source data list of the flight training simulator is obtained, including:
and according to the development requirement scheme and the development target of the aircraft flight training simulator, the aircraft engineering design source data corresponding to the development process of the simulator are arranged to form a development source data list, as shown in fig. 2 and 3.
In the above step S1, when the development source data list is determined, the source data range includes three-dimensional digital-analog data for designing the structural shape of the simulator, the layout of the cockpit, and the installation equipment of the cockpit, and data describing functions, principles, compositions, and the like of each system; the source data types include three-dimensional modulus, CATPart/. CATProduct format files, and text descriptive files published in PDF format.
In the step S2, the aircraft flight training simulator is simulation training equipment used for replacing a pilot for training a real aircraft, and the effectiveness of the simulator training is required to be guaranteed only by completely conforming to the configuration of a driver model.
In the step S3, when the NAS system is built, a source data structure tree is built in the NAS system according to the simulator development source data list in a hierarchical manner, as shown in fig. 4; the NAS system establishes an interface with the PDM system, acquires and stores corresponding files from the PDM system according to a source data file list on a source data structure tree, and associates with corresponding source data files in the PDM system at the same time so as to ensure that the change of the source data files can be tracked; the NAS system is a server for storing source data files and difference data, the PDM system is a product data management system, design source data are stored in the NAS system, and the design source data are associated and stored with the PDM system source data files through the NAS system.
In the step S4, when the association relationship between the source data files stored in the NAS system and the corresponding file data in the PDM system is established, the NAS system updates the source data structure tree of the system by reading the latest version information of the source data files in the PDM system, so that the structure tree files on the NAS system are synchronized with the source data file versions corresponding to the PDM system, and at the same time, the source data file items listed in the source data structure tree capture data modification information in the PDM system, and generate a source data file difference analysis log table in the NAS system.
In the above step S5, when creating the NAS system using the account number and the access address, the simulator developer logs in to refer to the desired file through the access address and the account number within the office lan, or logs in to the NAS system through the external network using the VPN to refer to the desired file.
In the step S6, the development simulator develops the source data modification visual management system, creates a source data file item modification tracking list in the system, and presents the related attribute information such as the number, the name, the data category, the model/part number, the required number, the supplier, the release number, the update time, and the like in the form of a table, as shown in fig. 5.
In the above step S7, highlighting the modified source data item on the source data structure tree includes:
highlighting the source data file with engineering change on a change tracking table by an informatization technical means to remind a researcher that a certain source data file is changed so as to facilitate the researcher to track the engineering change of the whole life cycle of the source data; and the researcher refers to the source data file with the change in the NAS system to evaluate and confirm whether the change is implemented, and the researcher restores the normal display of the highlight display item through the confirmation operation, so that the engineering source data change closed-loop management is realized, and the consistency of the simulator and the state of a true machine is ensured.
In the present embodiment, it is also performed that: setting priority and expected response time for NAS systems corresponding to different source data; allocating caches for each NAS system according to the priority, wherein the NAS system with high priority allocates large cache capacity and the NAS system with low priority allocates small cache capacity; and monitoring each NAS system in real time, judging whether the cache capacity of the corresponding NAS system is matched with the corresponding priority, judging whether the actual response time of the corresponding NAS system is matched with the expected response time, and if not, distributing the cache for each NAS system again.
Further, different expected response times are set for NAS systems corresponding to different service applications according to performance requirements and priorities of each source data. The priorities of the NAS systems include unlimited priority, high priority, medium priority, and low priority. Allocating dedicated caches for high priority NAS systems may be implemented such that the high priority NAS systems obtain large bandwidths and achieve near-targeted expected response times; dynamically adjusting cache allocation according to the result of monitoring the continuous performance of the NAS system; multiple applications with different I/O performance requirements can be integrated into one storage system, so that the service performance requirements are met.
In this embodiment, the NAS system and the PDM system form an FFS source data management system, and this embodiment further provides a cloud management platform, which is configured to implement data interaction between a user side and the FFS source data management system, and deploy services of the user side and the FFS source data management system.
Specifically, the cloud management platform comprises a manager module, a cloud orchestrator module and a controller module, wherein the manager module is used for processing a service request from an application and providing agile service deployment for a user; the cloud orchestrator module is used for resource configuration of cloud resources and instantiation operation of the cloud resources; the controller module is used for carrying out information interaction with the SFC manager module.
Further, the manager module includes:
the Tosca analyzer is used for analyzing the cloud service input request;
the decomposition module is used for dividing cloud resources and network resources into two types: cloud resources/cloud services deployed to the cloud orchestrator, cloud resources/chaining paths deployed to the SDN;
the cloud orchestration converter is used for converting the cloud resources/cloud services which are deployed to the cloud orchestrator and are decomposed by the decomposition module into template languages which can be identified by the cloud orchestrator;
the cloud resource instantiation module is used for instantiating the template language converted by the cloud arrangement converter;
an SFC manager to handle cloud resource/chaining path requirements deployed to an SDN: after acquiring cloud resources/interlinked paths deployed to the SDN, the SFC manager processes the cloud resources and interlinked path requirements, sends a processing result to an SDN controller module, and informs the SDN controller module to instantiate the cloud resources/interlinked path requirements deployed to the SDN;
and the monitoring module is used for monitoring the operation process of the SLC manager module.
Therefore, the embodiment also combines related technologies of SDN and cloud arrangement to design an implementation agile service management system so as to ensure that application and service management can fully utilize the advantages of a software network architecture and virtualized network functions, thereby being capable of realizing full life cycle management of a wireless network, providing differentiated services for wireless network business and realizing network value-added and agile cloud service management.
In summary, by adopting the technical scheme, the embodiment can quickly, completely and accurately identify the source data engineering change, can realize automatic tracking, change evaluation and change closed-loop processing of the source data engineering change quoted by the aircraft flight training simulator, and further realizes accurate management of the full-life configuration of the flight training simulator.
Furthermore, the FFS source data management system can intensively display all source data quoted by FFS development according to the form of an ATA chapter structure tree, so that FFS development staff can conveniently review related source data files, and the scattered source data files are collected together for management, thereby improving the working efficiency of the development staff;
further, the FFS source data management system can regularly capture source data change information to generate a version difference log table, FFS researchers can review the difference log table to obtain source data change information, so that the situation that whether a change occurs or not is avoided when the researchers go to a PDM system for manual check is avoided, and a large amount of labor cost is saved;
furthermore, in the embodiment, the normal display is restored by highlighting the source data item with the change and completing the change, so that the closed-loop management of the change process is explicit, the occurrence of the change of the source data is avoided, the FFS is not implemented, and the integrity and the accuracy of the change are improved.
The technical features of the above embodiments may be arbitrarily combined, and all possible combinations of the technical features in the above embodiments are not described for brevity of description, however, as long as there is no contradiction between the combinations of the technical features, they should be considered as the scope of the description.
The above embodiments are only preferred embodiments of the present invention, and the scope of the present invention is not limited thereto, but any insubstantial changes and substitutions made by those skilled in the art on the basis of the present invention are intended to be within the scope of the present invention as claimed.

Claims (10)

1. A full life cycle management method for developing source data of a flight training simulator is characterized by comprising the following steps:
acquiring a development source data list of a flight training simulator;
confirming the required files or the unique data sources corresponding to the digital and analog one by one in a PDM system based on the development source data list;
building a NAS system, storing required file data in the NAS system according to the development source data list, and building a source data structure tree;
establishing an association relation between source data files stored in the NAS system and corresponding file data in the PDM system one by one to realize the synchronization of the source data files of the NAS system and the corresponding file versions of the PDM system;
creating an NAS system, using an account number and an access address, and logging in and looking up a required file through the access address and the account number;
developing a source data change visual management system by a development simulator, creating a source data change tracking table in the system, and displaying the related attribute information of the data item in a two-dimensional matrix form;
and highlighting the changed source data item on the source data structure tree, so as to realize the closed-loop management of engineering source data change and ensure the consistency of the simulator and the state of a true machine.
2. The method of claim 1, wherein the obtaining a source data inventory for development of the flight training simulator comprises:
and according to the development requirement scheme and the development target of the aircraft flight training simulator, the aircraft engineering design source data required by the development process of the simulator are arranged to form a development source data list.
3. The method according to claim 1, characterized in that:
when determining the development source data list, the source data range comprises three-dimensional digital-analog data for designing the structural appearance, the cockpit layout and the cockpit installation equipment of the simulator, and data for describing functions, principles, compositions and the like of each system; the source data types include three-dimensional modulus, CATPart/. CATProduct format files, and text descriptive files published in PDF format.
4. The method according to claim 1, characterized in that:
the method comprises the steps of carrying out full life cycle engineering change on design source data quoted by development of a flight training simulator, and carrying out tracking management, wherein files and three-dimensional digital models corresponding to a development source data list are required to be established in a PDM system to serve as unique data sources, the source data are updated and replaced in full life cycle according to engineering change conditions, and the development source data list and the data files corresponding to the PDM system are associated to realize linkage of source data change.
5. The method according to claim 1, characterized in that:
when the NAS system is built, a source data structure tree is built in the NAS system according to a simulator development source data list in a hierarchical manner;
the NAS system establishes an interface with the PDM system, acquires and stores corresponding files from the PDM system according to a source data file list on a source data structure tree, and associates with corresponding source data files in the PDM system at the same time so as to ensure that the change of the source data files can be tracked; the NAS system is a server for storing source data files and difference data, the PDM system is a product data management system, design source data are stored in the NAS system, and the design source data are associated and stored with the PDM system source data files through the NAS system.
6. The method according to claim 1, characterized in that:
when the association relation between the source data files stored in the NAS system and the corresponding file data in the PDM system is established, the NAS system updates the source data structure tree of the system by reading the latest version information of the source data files in the PDM system, so that the structure tree files on the NAS are synchronous with the versions of the source data files corresponding to the PDM system, meanwhile, the data change information is captured in the PDM system according to the source data file items listed in the source data structure tree, and a source data file difference analysis log table is generated in the NAS system.
7. The method according to any one of claims 1 to 6, wherein:
when the NAS system is created and uses the account number and the access address, the required file is checked through the access address and the account number in the range of the local area network, or the required file is checked through the external network by using the VPN.
8. The method of any of claims 1 to 6, wherein the modification visualization management system comprises:
a source data file item change tracking list is created in the system, and related attribute information such as numbers, names, data categories, model numbers/part numbers, required quantity, suppliers, release times, update time and the like are displayed in a table form.
9. The method of any of claims 1 to 6, wherein highlighting the changed source data item on the source data structure tree comprises:
highlighting the data file with the engineering change source on the change tracking table by an informatization technical means so as to facilitate a researcher to track the engineering change of the whole life cycle of the source data; and referring to the source data file subjected to modification in the NAS system to evaluate, and confirming whether modification is implemented or not, and restoring normal display of the highlighted item through confirmation operation, so that engineering source data modification closed-loop management is realized, and the consistency of the simulator and the state of a true machine is ensured.
10. The method according to any one of claims 1 to 6, wherein:
setting priority and expected response time for NAS systems corresponding to different source data;
allocating caches for each NAS system according to the priority, wherein the NAS system with high priority allocates large cache capacity and the NAS system with low priority allocates small cache capacity; and monitoring each NAS system in real time, judging whether the cache capacity of the corresponding NAS system is matched with the corresponding priority, judging whether the actual response time of the corresponding NAS system is matched with the expected response time, and if not, distributing the cache for each NAS system again.
CN202311305813.7A 2023-10-10 2023-10-10 Full life cycle management method for development source data of flight training simulator Pending CN117435565A (en)

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