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 present invention relates to civil aviaton field and field of software development, the seating plane health of more particularly to a kind of two-way interactive
Management ground support system framework.
Background technology
With the fast development of the technologies such as electronic technology, information technology and new material, modern seating plane increasingly tends to
Maximization, complication, high speed and automation.Aircraft system scale also increases therewith with performance, coupling between various parts
Also more tight, this results in and triggers the factor of airplane fault numerous, failure performance diversification of forms, is existed between each failure multiple
Miscellaneous coupled relation.This not only brings difficulty to the troubleshooting maintenance work of aircraft, return aircraft safe operation bring it is hidden
Suffer from.
Civil aircraft health control ground support system is to improve aircraft reliability, ensure the crucial skill of aircraft safety operation
Art, is also the technical guarantee for realizing condition maintenarnce, supports significant for civil aircraft operation and product technology.Mesh
Before, China's seating plane development work is at the early-stage, and passenger plane is health management system arranged not yet to set up open, general system of systems
Framework.And although traditional software architecture employs open mode, but the simply opening of system development one-level, specifically should
Specific software support is also needed in, software reusability is poor with portability, cannot meet different user it is multi-level,
Diversification, lasting changes in demand.Accordingly, it would be desirable to design a kind of opening, general seating plane health control ground support
System architecture, makes system possess two-way interactive and self refresh ability, so that it is guaranteed that ground support system plays its due efficiency.
The content of the invention
It is an object of the invention to the above mentioned problem that the software architecture for overcoming existing passenger plane health management system arranged is present, propose
A kind of two-way interactive and seating plane health control ground support system framework, can solve prior art opening deficiency and lead
Software reusability is caused with portable poor problem so that user can be according to needed for the change more new system of self-demand
Function, saves development cost.
To achieve these goals, system is supported on the seating plane health control ground the invention provides a kind of two-way interactive
System framework, includes successively from top to bottom：Presentation layer, unified structure element development layer, platform services layer and backstage resource layer；
The presentation layer, for processing interacting for user and system, there is provided the connecting interface with other systems；
The unified structure element development layer, loading, assembling and unloading service for providing component；According to user's request example
Change each component of platform services layer, generate component example；Generated by way of combining assembling and meet the component bag that user requires；
The platform services layer, for providing system general, basic component；And for unified structure element development layer is generated
Component example provide running environment and hardware foundation；
The backstage resource layer, it is complete for the platform services layer provides knowledge, algorithm, the management of data message and accesses
Into the request of data of platform services layer；And the real-time data memory for producing system operation is in Service Database.
In above-mentioned technical proposal, the function of the presentation layer is specifically included：
(1), presentation layer receives the data input of user, unified structure element development layer is passed to after data message is translated, is put down
Platform service layer and backstage resource layer；
(2) Authority Verification, is carried out to the user for accessing；
(3), the real time data that system operation is produced is transferred to other systems by the connecting interface, is the group of aircraft
Send maintenance provided auxiliary decision support.
In above-mentioned technical proposal, described other systems include：Main manufacturer, airline and third-party vendor.
In above-mentioned technical proposal, the platform services layer provides seating plane health control ground for unified structure element development layer
The interface that basic, the general component and component of support system are called；Component defines structure using IDL component description languages
The interface data of part, interaction and log content.
In above-mentioned technical proposal, the unified structure element development layer is according to user's request, the component provided service platform layer
Class is instantiated, the demand for making it meet different user differentiation.
In above-mentioned technical proposal, the unified structure element development layer is instantiated to each component, will to combine assembling mode
The Component composition of each instantiation together, forms corresponding instantiation component bag, so that for different users provides service, these
Instantiation component bag is operated in the running environment of platform services layer offer.
In above-mentioned technical proposal, the example component bag transmits the application server into platform services layer by interface,
Application server is connected by LAN or WAN with upper strata, reception processing request, and backstage resource level data storehouse is accessed as requested, will
Processing information returns to presentation layer；Meanwhile, the data of the real-time data memory that system operation is produced to the backstage resource layer
In storehouse, for subsequently using.
In above-mentioned technical proposal, the real time data that the system operation is produced includes：Monitoring data, fault diagnosis result,
Failure predication and health evaluating analysis result.
In above-mentioned technical proposal, the backstage resource layer additionally provides the expanded configuration interface of information resources.
Advantage of the invention is that：
1st, the present invention establishes a kind of opening towards seating plane, general system architecture, meets different user, multilayer
Secondary, diversification health control application demand；
2nd, system architecture of the invention system is possessed self refresh, from restructuring ability, can quickly, flexibly realize user's
Business demand, is that the Function Extension of system lays the first stone；
3rd, operation monitoring personnel can be improved using system architecture designed system of the invention and airline repairs and protects
The troubleshooting efficiency of barrier personnel, reference is provided for the design of aircraft is improved；
4th, the dispatch reliability of aircraft can be improved using system architecture designed system of the invention, airline is reduced
Operating cost, to realize that condition maintenarnce provides technical support.
Brief description of the drawings
Fig. 1 is the schematic diagram of the seating plane health control ground support system framework of two-way interactive of the invention；
Seating plane health control ground support system two-way interactive and self refresh that Fig. 2 is provided by the embodiment of the present invention
Operating diagram；
The seating plane health control ground support system structural representation that Fig. 3 embodiment of the present invention is provided.
Specific embodiment
It is strong the invention provides a kind of seating plane of two-way interactive in order to ensure the opening and versatility of system architecture
Kang Guanli ground support system frameworks, below in conjunction with accompanying drawing and embodiment, the present invention will be described in further detail.
In order to different user is multi-level, diversification, lasting changes in demand, improve software reusability, the present invention is implemented
Example provides a kind of seating plane health control ground support system framework of two-way interactive, as shown in Figure 1.The system architecture from
It is up to lower to include performance (access) layer, unified structure element development platform layer, platform services layer and backstage resource layer.Wherein,
Presentation layer is used to realize man-machine interaction and the communication with external system.The input instruction of user is translated and passed by this layer
It is defeated by following operation layer.Meanwhile, the connecting interface with external system is also provided；
Unified structure element development layer is instantiated according to the component of system command calling platform service layer to it.By group
Attach together the business function that the mode matched somebody with somebody realizes system；
The base of prognostic and health management ground support system is provided in platform services layer for unified structure element development platform
This component such as computing component, basic component, business component etc., and the interface that upper strata is called is provided.Meanwhile, service platform layer is also
For upper strata component example provides running environment and infrastructure；
Backstage resource layer provides the management of the information such as knowledge, algorithm, data and accesses for upper strata, and the data for completing upper strata please
Ask.Meanwhile, the analysis result such as fault diagnosis, monitor in real time, failure predication that system operation is produced is transmitted to backstage resource layer, is deposited
In storing up Service Database.Backstage resource layer also provides the expanded configuration interface of information resources.
A kind of seating plane health control ground support system framework of the two-way interactive proposed in the present invention.Different user
The basic component of service platform layer offer can be provided according to the characteristics of demand of itself, it is carried out in unified structure element development layer
Instantiation, extends the function of component, realizes the dynamic scalable characteristic of system.Each component is realized by way of combining assembling
The functional requirement of different user, realizes the two-way interactive and self refresh ability of system, improves the reusability of software, reduces soft
The development cost of part.System bidirectional is interacted and see Fig. 2 with the son renewal course of work.
In the present embodiment, Fig. 3 shows the frame of the seating plane health control ground support system with two-way interactive
Structure schematic diagram.As shown in figure 3, backstage resource layer includes data resource two parts that existing resource and system operation are produced.It is existing
Resource including produced business datum, run monitoring data, maintain handbook, historical failure case, user profile etc. and pass through
The technical transmissions such as Web Services, XML are to backstage resource layer.
In the present embodiment, the performance main completion system of (access) layer is exchanged such as the verification of input with external data.One side
Face, presentation layer receives the data input of user, and information translation is passed into unified structure element development layer, platform services layer and backstage
Resource layer.On the other hand, system is produced real-time monitoring data, fault diagnosis result, failure predication and health evaluating analysis knot
Fruit is transferred to main manufacturer's system, airline system and third party supply by system and the connecting interface of external system
Such as fast acoustic system of quotient system system, is that sending for aircraft repairs provided auxiliary decision support.
According to the definition and planning of seating plane prognostic and health management ground support system, system is divided into base
The basic business work(such as monitoring, prognostics and health management after plinth service, data transmit-receive and treatment, monitor in real time, fault diagnosis, boat
Energy.Each functional module is further segmented, and including message reception, message decoding, message coding, parameter monitoring, failure monitoring, hand
The subfunctions such as volume diagnosis, case diagnosis.Basic in systemic-function, general partial encapsulation is risen using different component classes
Come, storage to platform services layer.Each component is provided a series of services in the form of interface to upper strata.The present embodiment uses IDL structures
The contents such as part description language, interface data, interaction, security strategy, affairs, the daily record of Unify legislation component.
The interface that unified structure element development layer passes through calling platform service layer, provides the parameter of component class.User can be according to certainly
Body demand extends member function, and generation meets the component example of user's requirement so that system meets different user object disparity
Functional requirement.Each component example is by assembling and controls, and formation can realize the component bag of corresponding service function, greatly improve
The quality and development efficiency of software.Example component bag transmits the application server into platform services layer by interface.Using
Server is connected by LAN or WAN with upper strata, reception processing request, and backstage resource level data storehouse is accessed as requested, will be processed
Information returns to presentation layer.Meanwhile, analysis result and the business datum storage that will be produced in the running of system to database
In, for subsequently using.For example, the user management component in platform services layer be mainly to provide the registration of user, deletion, modification with
And access resource authorization service.The use that the user objects such as the main manufacturer of aircraft, airline can be provided with calling platform service layer
Family management component.The authority of the resource authorization of different users is set according to self-demand, they are ensured for system with this
The different requirements of user's access rights.
Using above-mentioned technical proposal, user can call the general of service platform layer offer according to the characteristics of self-demand
Component generation meet the component example of user's request.Each component example combination is formed together by way of combining assembling
Corresponding software, service logic is separated with software development, so as to quickly, neatly realize the demand of user so that be
System has self refresh ability.Additionally, the interface that service platform is provided is unified standard, this allows for the structure in service platform layer
Part can provide service for different users, so as to realize the two-way interactive of user and user, user and service platform, quick, spirit
The multi-level lasting changes in demand of user is realized livingly, the O＆M cost of civil aircraft unit of operation is reduced, and lifts O＆M efficiency.
Claims (9)
1. a kind of seating plane health control ground support system framework of two-way interactive, includes successively from top to bottom：Presentation layer,
Unified structure element development layer, platform services layer and backstage resource layer；Characterized in that,
The presentation layer, for processing interacting for user and system, there is provided the connecting interface with other systems；
The unified structure element development layer, loading, assembling and unloading service for providing component；It is flat according to user's request instantiation
Each component of platform service layer, generates component example；Generated by way of combining assembling and meet the component bag that user requires；
The platform services layer, for providing system general, basic component；And be the structure of unified structure element development layer generation
Part example provides running environment and hardware foundation；
The backstage resource layer, for the platform services layer provides knowledge, algorithm, the management of data message and accesses, completes flat
The request of data of platform service layer；And the real-time data memory for producing system operation is in Service Database.
2. the seating plane health control ground support system framework of two-way interactive according to claim 1, its feature exists
In the function of the presentation layer is specifically included：
(1), presentation layer receives the data input of user, and unified structure element development layer, platform clothes are passed to after data message is translated
Business layer and backstage resource layer；
(2) Authority Verification, is carried out to the user for accessing；
(3), the real time data that system operation is produced is transferred to other systems by the connecting interface, is that aircraft sends dimension
Repair provided auxiliary decision support.
3. the seating plane health control ground support system framework of two-way interactive according to claim 1 and 2, its feature
It is that described other systems include：Main manufacturer, airline and third-party vendor.
4. the seating plane health control ground support system framework of two-way interactive according to claim 1, its feature exists
In, the platform services layer for unified structure element development layer provide seating plane health control ground support system it is basic,
The interface that general component and component is called；Component using IDL component description languages define the interface data of component, interaction and
Log content.
5. the seating plane health control ground support system framework of a kind of two-way interactive according to claim 1, it is special
Levy and be, the unified structure element development layer is instantiated according to user's request to the component class that service platform layer is provided, and makes it
Meet the demand of different user differentiation.
6. a kind of seating plane health control ground support system framework of the two-way interactive stated according to claim 1, its feature
It is that the unified structure element development layer is instantiated to each component, to combine assembling mode by the Component composition of each instantiation
Together, corresponding instantiation component bag is formed, so that for different users provides service, these instantiation component bags are operated in
In the running environment that platform services layer is provided.
7. the seating plane health control ground support system framework of a kind of two-way interactive according to claim 6, it is special
Levy and be, the example component bag transmits the application server into platform services layer by interface, application server passes through LAN
Or WAN is connected with upper strata, reception processing request accesses backstage resource level data storehouse as requested, and processing information is returned into table
Existing layer；Meanwhile, in the real-time data memory that system operation is produced to the database of the backstage resource layer, for subsequently using.
8. the seating plane health control ground support system framework of the two-way interactive according to claim 1 or 2 or 7, its
It is characterised by, the real time data that the system operation is produced includes：Monitoring data, fault diagnosis result, failure predication and health
Analysis and assessment result.
9. the seating plane health control ground support system framework of a kind of two-way interactive according to claim 1, it is special
Levy and be, the backstage resource layer additionally provides the expanded configuration interface of information resources.
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
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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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| 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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