CN106815013A - A kind of seating plane health control ground support system framework of two-way interactive - Google Patents
A kind of seating plane health control ground support system framework of two-way interactive Download PDFInfo
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Abstract
The invention discloses a kind of seating plane health control ground support system framework of two-way interactive, include successively from top to bottom：Presentation layer, unified structure element development layer, platform services layer and backstage resource layer；The presentation layer is used to process interacting for user and system, there is provided the connecting interface with other systems；The unified structure element development layer is used to provide the loading of component, assembling and unloading service；Each component of platform services layer is instantiated according to user's request, component example is generated；Generated by way of combining assembling and meet the component bag that user requires；The platform services layer is used to provide system general, basic component；And for the component example of unified structure element development layer generation provides running environment and hardware foundation；The backstage resource layer is used to, for the platform services layer provides knowledge, algorithm, the management of data message and accesses, complete the request of data of platform services layer；And the real time data that system operation is produced is stored in Service Database.
Description
Technical Field
The invention relates to the field of civil aviation and software development, in particular to a bidirectional interactive civil airliner health management ground support system architecture.
Background
With the rapid development of electronic technology, information technology, new materials and other technologies, modern civil airliners are becoming increasingly large-scale, complex, high-speed and automatic. The scale and the performance of the airplane system are increased, the coupling among all parts of the system is tighter, so that a plurality of factors causing airplane faults are caused, the fault expression forms are diversified, and complex coupling relations exist among all faults. The method not only brings difficulty to troubleshooting and maintenance work of the airplane, but also brings hidden danger to safe operation of the airplane.
The civil aircraft health management ground support system is a key technology for improving the reliability of the aircraft and ensuring the safe operation of the aircraft, is a technical guarantee for realizing the maintenance according to the situation, and has important significance for the civil aircraft operation and the product technical support. At present, the development work of civil airliners in China just starts, and an open and universal system architecture is not established in an airliner health management system. The traditional software architecture adopts an open mode, but only has one-level openness of system development, and also needs specific software support in specific application, so that the reusability and the portability of the software are poor, and the requirement change of different users in multiple layers, diversification and continuity can not be met. Therefore, it is necessary to design an open and general architecture of the ground support system for health management of the civil airliner, so that the system has bidirectional interaction and self-updating capability, thereby ensuring that the ground support system exerts its proper efficiency.
Disclosure of Invention
The invention aims to overcome the problems of the software architecture of the existing health management system of the passenger plane, provides a ground support system architecture for bidirectional interaction and civil passenger plane health management, and can solve the problem of poor software reusability and portability caused by insufficient openness in the prior art, so that a user can update functions required by the system according to changes of self requirements, and the development cost is saved.
In order to achieve the above object, the present invention provides a bidirectional interactive ground support system architecture for health management of a civil airliner, which comprises, from top to bottom: the system comprises a presentation layer, a unified component development layer, a platform service layer and a background resource layer;
the presentation layer is used for processing the interaction between the user and the system and providing a connection interface with other systems;
the unified component development layer is used for providing loading, assembling and unloading services of components; instantiating each component of a platform service layer according to user requirements to generate a component instance; generating a component package meeting the requirements of a user in a combined assembly mode;
the platform service layer is used for providing a system general and basic component; providing a running environment and a hardware basis for the component examples generated by the unified component development layer;
the background resource layer provides management and access of knowledge, algorithm and data information for the platform service layer to complete the data request of the platform service layer; and storing real-time data generated by the system operation in a service database.
In the above technical solution, the function of the presentation layer specifically includes:
(1) the presentation layer receives data input of a user, translates data information and transmits the translated data information to the unified component development layer, the platform service layer and the background resource layer;
(2) carrying out authority verification on the accessed user;
(3) real-time data generated by the operation of the system is transmitted to other systems through the connecting interface, and auxiliary decision support is provided for dispatching and maintaining the airplane.
In the above technical solution, the other system includes: host manufacturers, airlines, and third party vendors.
In the technical scheme, the platform service layer provides a basic and universal component of a civil passenger plane health management ground support system and a component calling interface for a unified component development layer; the building blocks define interface data, interaction and log content of the building blocks in IDL building block description language.
In the above technical solution, the unified component development layer instantiates the component class provided by the service platform layer according to the user requirements, so that the component class meets the differentiated requirements of different users.
In the above technical solution, the unified component development layer instantiates each component, and combines the instantiated components together in a combined assembly manner to form a corresponding instantiated component package, so as to provide services for different users, and the instantiated component packages operate in an operating environment provided by the platform service layer.
In the technical scheme, the instance component package is transmitted to an application server in a platform service layer through an interface, the application server is connected with an upper layer through a LAN or a WAN, receives a processing request, accesses a background resource layer database according to a requirement, and returns processing information to the presentation layer; meanwhile, real-time data generated by system operation is stored in the database of the background resource layer for subsequent use.
In the above technical solution, the real-time data generated by the system operation includes: monitoring data, fault diagnosis results, fault prediction and health evaluation analysis results.
In the above technical solution, the background resource layer further provides an expansion configuration interface of the information resource.
The invention has the advantages that:
1. the invention establishes an open and universal system architecture facing civil airliners, and meets the requirements of different users, multi-level and diversified health management application;
2. the system architecture of the invention enables the system to have self-updating and self-reorganization capabilities, can quickly and flexibly realize the service requirements of users, and lays a foundation for the function expansion of the system;
3. the system designed by the system architecture can improve the troubleshooting efficiency of operation monitoring personnel and maintenance support personnel of an airline company, and provides reference for the design improvement of the airplane;
4. the system designed by the system architecture can improve the dispatch reliability of the airplane, reduce the operation cost of the airline company and provide technical support for realizing the maintenance according to the situation.
Drawings
FIG. 1 is a schematic diagram of the bi-directional interactive civil airliner health management ground support system architecture of the present invention;
FIG. 2 is a schematic diagram of the bidirectional interaction and self-updating operation of a civil airliner health management ground support system provided by an embodiment of the present invention;
fig. 3 is a schematic structural diagram of a civil passenger plane health management ground support system provided by an embodiment of the present invention.
Detailed Description
In order to ensure the openness and universality of the system architecture, the invention provides a bidirectional interactive civil passenger plane health management ground support system architecture, which is further described in detail below with reference to the accompanying drawings and embodiments.
In order to improve the reusability of software and achieve multi-level, diversified and continuous demand changes of different users, the embodiment of the invention provides a bidirectional interactive civil passenger plane health management ground support system architecture, as shown in fig. 1. The system architecture comprises an expression (access) layer, a unified component development platform layer, a platform service layer and a background resource layer from top to bottom. Wherein,
the presentation layer is used for realizing man-machine interaction and communication with an external system. This layer transfers the user's input command translation to the underlying business layer. Meanwhile, a connection interface with an external system is also provided;
and the unified component development layer calls the components of the platform service layer according to the system instruction and instantiates the components. The service function of the system is realized through a combined assembly mode;
the platform service layer provides basic components of the fault prediction and health management ground support system, such as an operation component, a basic component, a business component and the like, for the unified component development platform, and provides an interface called by an upper layer. Meanwhile, the service platform layer also provides a running environment and infrastructure for the upper-layer component instance;
the background resource layer provides management and access of information such as knowledge, algorithms and data for the upper layer, and data requests of the upper layer are completed. Meanwhile, analysis results such as fault diagnosis, real-time monitoring, fault prediction and the like generated by the system operation are transmitted to the background resource layer and stored in the service database. The background resource layer also provides an expansion configuration interface of the information resources.
The invention provides a bidirectional interactive civil passenger plane health management ground support system architecture. Different users can call the basic components provided by the service platform layer according to the self requirement characteristics, instantiate the basic components in the unified component development layer, expand the functions of the components and realize the dynamic extensible characteristic of the system. The functional requirements of different users are realized by the components in a combined assembly mode, the bidirectional interaction and self-updating capability of the system is realized, the reusability of software is improved, and the development cost of the software is reduced. The system bidirectional interaction and sub-update work process can be seen in fig. 2.
In this embodiment, fig. 3 shows an architectural schematic of a civil airliner health management ground support system with bi-directional interaction. As shown in fig. 3, the background resource layer includes two parts, namely, an existing resource and a data resource generated by the system running. The existing resources comprise generated service data, operation monitoring data, a maintenance manual, historical fault cases, user information and the like, and are transmitted to a background resource layer through technologies such as Web Services and XML.
In this embodiment, the presentation (access) layer mainly completes the exchange of the system with external data, such as the verification of the input. On one hand, the presentation layer receives data input of a user and transmits information translation to the unified component development layer, the platform service layer and the background resource layer. On the other hand, real-time monitoring data, fault diagnosis results, fault prediction and health evaluation analysis results generated by the system are transmitted to a main manufacturer system, an airline system and a third party supplier system such as a quick response system through a connection interface of the system and an external system, so that auxiliary decision support is provided for dispatching and maintaining the airplane.
According to the definition and planning of the civil airliner fault prediction and health management ground support system, the system is divided into basic service functions such as basic service, data receiving, sending, receiving and processing, real-time monitoring, fault diagnosis, post-aviation monitoring, prediction and health management. Each functional module is further subdivided and comprises sub-functions of message receiving, message decoding, message encoding, parameter monitoring, fault monitoring, manual diagnosis, case diagnosis and the like. And encapsulating basic and universal parts in the system functions by adopting different component classes and storing the encapsulated parts in a platform service layer. Each component provides a series of services to the upper layer in the form of an interface. In the embodiment, an IDL component description language is adopted to uniformly describe the contents of interface data, interaction, security policy, transaction, log and the like of the component.
The unified component development layer gives the parameters of the component class by calling the interface of the platform service layer. The user can expand the component functions according to the self requirements and generate the component examples meeting the user requirements, so that the system meets the functional requirements of object differentiation of different users. Each component instance forms a component package capable of realizing corresponding service functions through assembly and control, and the quality and the development efficiency of software are greatly improved. The instance build package is transmitted to an application server in the platform services layer through an interface. The application server is connected with the upper layer through the LAN or WAN, receives the processing request, accesses the background resource layer database according to the request and returns the processing information to the presentation layer. Meanwhile, the analysis result and the service data generated in the operation process of the system are stored in the database for subsequent use. For example, the user management component in the platform service layer mainly provides registration, deletion, modification and access resource authorization services of the user. User objects such as the aircraft owner manufacturer, airline, etc. may invoke user management components provided by the platform services layer. And setting the resource authorization authority of different users according to the self requirements so as to ensure different requirements of the users on the access authority of the system.
By applying the technical scheme, the user can call the universal component provided by the service platform layer to generate the component instance meeting the user requirement according to the characteristics of the self requirement. The component instances are combined together to form corresponding software in a combined assembly mode, and business logic and software development are separated, so that the requirements of users are quickly and flexibly met, and the system has self-updating capability. In addition, the interfaces provided by the service platform are unified, so that the components in the service platform layer can provide services for different users, thereby realizing the bidirectional interaction between the users and the service platform, realizing the multi-level continuous demand change of the users quickly and flexibly, reducing the operation and maintenance cost of a civil aircraft operation unit and improving the operation and maintenance efficiency.
Claims (9)
1. A bidirectional interactive civil passenger plane health management ground support system architecture comprises the following components in sequence from top to bottom: the system comprises a presentation layer, a unified component development layer, a platform service layer and a background resource layer; it is characterized in that the preparation method is characterized in that,
the presentation layer is used for processing the interaction between the user and the system and providing a connection interface with other systems;
the unified component development layer is used for providing loading, assembling and unloading services of components; instantiating each component of a platform service layer according to user requirements to generate a component instance; generating a component package meeting the requirements of a user in a combined assembly mode;
the platform service layer is used for providing a system general and basic component; providing a running environment and a hardware basis for the component examples generated by the unified component development layer;
the background resource layer provides management and access of knowledge, algorithm and data information for the platform service layer to complete the data request of the platform service layer; and storing real-time data generated by the system operation in a service database.
2. The bi-directional interactive civil airliner health management ground support system architecture of claim 1, wherein the functionality of the presentation layer specifically comprises:
(1) the presentation layer receives data input of a user, translates data information and transmits the translated data information to the unified component development layer, the platform service layer and the background resource layer;
(2) carrying out authority verification on the accessed user;
(3) real-time data generated by the operation of the system is transmitted to other systems through the connecting interface, and auxiliary decision support is provided for dispatching and maintaining the airplane.
3. The bi-directional interactive civil airliner health management ground support system architecture of claim 1 or 2, wherein the other systems comprise: host manufacturers, airlines, and third party vendors.
4. The bi-directional interactive civil airliner health management ground support system architecture of claim 1, wherein the platform services layer provides a unified component development layer with an interface for basic, generic components and component calls of a civil airliner health management ground support system; the building blocks define interface data, interaction and log content of the building blocks in IDL building block description language.
5. The architecture of claim 1, wherein the unified component development layer instantiates component classes provided by the service platform layer according to user requirements, so that the component classes meet different user differentiation requirements.
6. The architecture of claim 1, wherein the unified component development layer instantiates components and combines the instantiated components together in a modular assembly to form instantiated component packages that run in a runtime environment provided by the platform services layer to provide services to different users.
7. The bidirectional interactive ground support system architecture for health management of civil airliners as defined in claim 6, wherein said instance component package is transmitted to an application server in the platform service layer through an interface, the application server is connected to the upper layer through a LAN or WAN, receives the processing request, accesses the background resource layer database as required, and returns the processing information to the presentation layer; meanwhile, real-time data generated by system operation is stored in the database of the background resource layer for subsequent use.
8. The bi-directional interactive civil airliner health management ground support system architecture of claim 1, 2, or 7, wherein the real-time data generated by operation of the system comprises: monitoring data, fault diagnosis results, fault prediction and health evaluation analysis results.
9. The bi-directional interactive civil airliner health management ground support system architecture defined in claim 1, wherein said background resource layer further provides an extended configuration interface for information resources.
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| CN109685933A (en) * | 2018-12-12 | 2019-04-26 | 中国航空工业集团公司西安航空计算技术研究所 | The customization event and parameter logistics of a kind of aircraft condition monitoring define method |
| CN112612465A (en) * | 2020-12-18 | 2021-04-06 | 中国人民解放军陆军工程大学 | Domain ontology multiplexing-oriented information system and development method |
| CN112734174A (en) * | 2020-12-28 | 2021-04-30 | 镇江市高等专科学校 | Intelligent interaction and service system of underwater robot |
| CN114580842A (en) * | 2022-01-25 | 2022-06-03 | 中国电子产品可靠性与环境试验研究所（（工业和信息化部电子第五研究所）（中国赛宝实验室）） | Vehicle dispatch reliability analysis method and device and computer equipment |
| CN114915533A (en) * | 2022-04-29 | 2022-08-16 | 武汉烽火技术服务有限公司 | Platform-based northbound interface implementation method and architecture |
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| CN112612465A (en) * | 2020-12-18 | 2021-04-06 | 中国人民解放军陆军工程大学 | Domain ontology multiplexing-oriented information system and development method |
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| CN112734174A (en) * | 2020-12-28 | 2021-04-30 | 镇江市高等专科学校 | Intelligent interaction and service system of underwater robot |
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| CN114580842A (en) * | 2022-01-25 | 2022-06-03 | 中国电子产品可靠性与环境试验研究所（（工业和信息化部电子第五研究所）（中国赛宝实验室）） | Vehicle dispatch reliability analysis method and device and computer equipment |
| CN114580842B (en) * | 2022-01-25 | 2022-12-09 | 中国电子产品可靠性与环境试验研究所（（工业和信息化部电子第五研究所）（中国赛宝实验室）） | Method and device for analyzing dispatch reliability of vehicle and computer equipment |
| CN114915533A (en) * | 2022-04-29 | 2022-08-16 | 武汉烽火技术服务有限公司 | Platform-based northbound interface implementation method and architecture |
| CN114915533B (en) * | 2022-04-29 | 2023-05-30 | 武汉烽火技术服务有限公司 | Method and architecture for realizing north interface based on platform |
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