CN104883392A - Component agent module-based spacecraft interface adapter and data interaction method adopting adapter to realize - Google Patents
Component agent module-based spacecraft interface adapter and data interaction method adopting adapter to realize Download PDFInfo
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- CN104883392A CN104883392A CN201510201781.5A CN201510201781A CN104883392A CN 104883392 A CN104883392 A CN 104883392A CN 201510201781 A CN201510201781 A CN 201510201781A CN 104883392 A CN104883392 A CN 104883392A
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- China
- Prior art keywords
- interface
- equipment
- agent module
- component
- spacecraft
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- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04L—TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
- H04L67/00—Network arrangements or protocols for supporting network services or applications
- H04L67/50—Network services
- H04L67/56—Provisioning of proxy services
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- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04L—TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
- H04L65/00—Network arrangements, protocols or services for supporting real-time applications in data packet communication
- H04L65/1066—Session management
- H04L65/1073—Registration or de-registration
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- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04L—TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
- H04L65/00—Network arrangements, protocols or services for supporting real-time applications in data packet communication
- H04L65/60—Network streaming of media packets
- H04L65/61—Network streaming of media packets for supporting one-way streaming services, e.g. Internet radio
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- Engineering & Computer Science (AREA)
- Multimedia (AREA)
- Computer Networks & Wireless Communication (AREA)
- Signal Processing (AREA)
- Business, Economics & Management (AREA)
- General Business, Economics & Management (AREA)
- Computer And Data Communications (AREA)
Abstract
The invention relates to a component agent module-based spacecraft interface adapter and a data interaction method adopting the adapter to realize, and relates to the field of aerospace adapters. The invention aims to solve the problem that management use of an interface of an existing spacecraft generally adopts a method of display calling, in adoption of the method, interfaces of devices are not unified, thus device management and use are inflexible, and access of the component agent module to the devices is inconvenient, thereby causing poor universality. A device management unit is used for configuring device interfaces and realizing device interface registration, ID configuration and issuing/subscription of information of subjects, and the component agent module is used for registering interfaces and issuing/subscribing to subjects to a bus in the form of components according to device interface registration, ID configuration and issuing/subscription of information of the subjects by the device management unit. The component agent module-based spacecraft interface adapter can be used for being connected with a spacecraft.
Description
Technical field
The present invention relates to a kind of interface adapter of spacecraft construction part module, particularly a kind of spacecraft interface adapter of Component-Based Development module.
Background technology
At present, for improving versatility, spacecraft tension management adopts Component Technology, connected, but building blocks of function also needs to carry out data interaction with physical layer interface between component agent module by bus.At present, spacecraft uses the method generally adopting and show and call to the management of its interface, adopt each equipment interface disunity in this way, and make equipment control dumb with use, component agent module is inconvenient to the access of equipment.
Summary of the invention
The present invention uses to solve existing spacecraft the method generally adopting and show and call to the management of its interface, adopt each equipment interface disunity in this way, make equipment control dumb with use, component agent module is inconvenient to the access of equipment, causes the problem of poor universality.The data interactive method a kind of spacecraft interface adapter of Component-Based Development module being now provided and adopting this adapter to realize.
A spacecraft interface adapter for Component-Based Development module, it comprises device management unit and component agent module,
Device management unit is used for configuration device interface, realizes registering the interface of equipment, the information of configuration ID and publish/subscribe theme,
Component agent module to be used for according to device management unit the information of equipment interface registration, configuration ID and publish/subscribe theme with component form to bus registration interface and publish/subscribe theme.
According to the data interactive method that a kind of spacecraft interface adapter of Component-Based Development module realizes, it comprises the following steps:
Step one, equipment respectively by equipment interface to device management unit device registration interface message, the information of device management unit simultaneously configuration device ID and publish/subscribe theme,
Step 2, component agent module, according to the information of device management unit device registration interface, configuration device ID and publish/subscribe theme, with component form to bus registration interface, realize the data transaction of equipment to spacecraft interface;
Step 3, component agent module, by bus publish/subscribe equipment theme, realize component agent module and communicate with spacecraft equipment.
Beneficial effect of the present invention is: the present invention adopts device management unit can configure each equipment interface, realize the information such as equipment interface registration, management equipment ID, publish/subscribe theme, adopt component agent module according to device management unit information with component form to bus registration interface adapter, realize the data interaction of equipment to spacecraft interface.Can be realized the configuration of the multiple interface of equipment by device management unit and component agent module, make interface use flexibly, then, component agent module, by each equipment theme of bus publish/subscribe, realizes spacecraft and devices communicating, concrete versatility.
Accompanying drawing explanation
Fig. 1 is the principle schematic of the spacecraft interface adapter of a kind of Component-Based Development proxy module described in embodiment one,
The flow chart of the data transfer device that Fig. 2 realizes for the spacecraft interface adapter according to a kind of Component-Based Development proxy module described in embodiment two.
Embodiment
Embodiment one: illustrate present embodiment, the spacecraft interface adapter of a kind of Component-Based Development proxy module described in present embodiment with reference to Fig. 1, it comprises device management unit 1 and component agent module 2,
Device management unit 1, for configuration device interface, realizes registering the interface of equipment, the information of configuration ID and publish/subscribe theme,
Component agent module 2 for according to the information of the registration of the device management unit 1 pair of equipment interface, configuration ID and publish/subscribe theme with component form to bus registration interface and publish/subscribe theme.
In present embodiment, device management unit manages each equipment interface, realizes the information such as equipment interface registration, management equipment ID, publish/subscribe theme.Log-on message is as follows:
| Sequence number | Component | Equipment |
| 1 | Component handle | Equipment interface 1 |
| 2 | Component handle | Equipment interface 2 |
| 3 | Component handle | Equipment interface 3 |
| …… | …… | …… |
| N | Component handle | Equipment interface N |
Wherein: Parameter N numerical value is how many and determine according to spacecraft particular device parameter.
Embodiment two: illustrate present embodiment with reference to Fig. 2, the adaptation method of the spacecraft interface adapter realization of a kind of Component-Based Development proxy module according to embodiment one, it comprises the following steps:
Step one, equipment respectively by equipment interface to device management unit 1 device registration interface message, the information of device management unit 1 simultaneously configuration device ID and publish/subscribe theme,
Step 2, component agent module 2, according to the information of device management unit 1 device registration interface, configuration device ID and publish/subscribe theme, with component form to bus registration interface, realize the data interaction of equipment to spacecraft interface;
Step 3, component agent module 2, by bus publish/subscribe equipment theme, realize component agent module and communicate with spacecraft equipment.
In present embodiment, equipment registers this equipment to each interface, the information such as device management unit management equipment ID, publish/subscribe theme;
Interface adapter activates, and interface adapter is registered to software bus.By other components of software bus, equipment can publish/subscribe theme, realizes devices communicating.
Devices communicating, other components by bus publish/subscribe theme, when theme conforms to interface adapter, then other components can with interface adapter exchanges data.The corresponding equipment of interface adapter operation, thus realize communicating with spacecraft equipment.
Claims (2)
1. a spacecraft interface adapter for Component-Based Development proxy module, is characterized in that, it comprises device management unit (1) and component agent module (2),
Device management unit (1), for configuration device interface, realizes registering the interface of equipment, the information of configuration ID and publish/subscribe theme,
Component agent module (2) for according to device management unit (1) to the information of equipment interface registration, configuration ID and publish/subscribe theme with component form to bus registration interface and publish/subscribe theme.
2. the exchange method of the spacecraft interface adapter realization of a kind of Component-Based Development proxy module according to claim 1, it is characterized in that, it comprises the following steps:
Step one, equipment respectively by equipment interface to device management unit (1) device registration interface message, the information of device management unit (1) simultaneously configuration device ID and publish/subscribe theme,
Step 2, component agent module (2) are according to the information of device management unit (1) device registration interface, configuration device ID and publish/subscribe theme, with component form to bus registration interface, realize the data interaction of equipment to spacecraft interface;
Step 3, component agent module (2), by bus publish/subscribe equipment theme, realize component agent module and communicate with spacecraft equipment.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510201781.5A CN104883392A (en) | 2015-04-25 | 2015-04-25 | Component agent module-based spacecraft interface adapter and data interaction method adopting adapter to realize |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510201781.5A CN104883392A (en) | 2015-04-25 | 2015-04-25 | Component agent module-based spacecraft interface adapter and data interaction method adopting adapter to realize |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104883392A true CN104883392A (en) | 2015-09-02 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510201781.5A Pending CN104883392A (en) | 2015-04-25 | 2015-04-25 | Component agent module-based spacecraft interface adapter and data interaction method adopting adapter to realize |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104883392A (en) |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20030144983A1 (en) * | 2002-01-29 | 2003-07-31 | International Business Machines Corporation | Object-oriented framework for generic adaptive control |
| CN101246421A (en) * | 2008-02-22 | 2008-08-20 | 山东中创软件工程股份有限公司 | Universal frame work based on workflow engine |
| CN101510236A (en) * | 2009-03-11 | 2009-08-19 | 上海坦瑞信息技术有限公司 | Plug and play system based on field operating platform |
-
2015
- 2015-04-25 CN CN201510201781.5A patent/CN104883392A/en active Pending
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20030144983A1 (en) * | 2002-01-29 | 2003-07-31 | International Business Machines Corporation | Object-oriented framework for generic adaptive control |
| CN101246421A (en) * | 2008-02-22 | 2008-08-20 | 山东中创软件工程股份有限公司 | Universal frame work based on workflow engine |
| CN101510236A (en) * | 2009-03-11 | 2009-08-19 | 上海坦瑞信息技术有限公司 | Plug and play system based on field operating platform |
Non-Patent Citations (2)
| Title |
|---|
| 张翼翔，马亚平，邹宏伟: "基于总线的模型构件数据交互控制方法", 《2013第一届中国指挥控制大会论文集》 * |
| 王军，熊桂喜: "基于软总线构件技术的数据传输处理系统开发", 《现代计算机(专业版)》 * |
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| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20150902 |