CN111130884A - Automatic configuration integration method applied to airborne broadband network system - Google Patents
Automatic configuration integration method applied to airborne broadband network system Download PDFInfo
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- CN111130884A CN111130884A CN201911363121.1A CN201911363121A CN111130884A CN 111130884 A CN111130884 A CN 111130884A CN 201911363121 A CN201911363121 A CN 201911363121A CN 111130884 A CN111130884 A CN 111130884A
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- integrated configuration
- airborne
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- management module
- configuration
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- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04L—TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
- H04L41/00—Arrangements for maintenance, administration or management of data switching networks, e.g. of packet switching networks
- H04L41/08—Configuration management of networks or network elements
- H04L41/0876—Aspects of the degree of configuration automation
- H04L41/0886—Fully automatic configuration
Abstract
The invention discloses an automatic configuration integration method applied to an airborne broadband network system, which comprises the following steps: s1: the automatic integrated configuration device establishes safe encrypted connection with the integrated configuration management module through a communication network 1; the integrated configuration management module has all airborne system information, a bidirectional security encryption authentication function and a data issuing function which need integrated configuration, the automatic integrated configuration device has the bidirectional security encryption authentication function and the automatic integrated configuration function for a target system, and S2: and the automatic integrated configuration device sends unique identification information UIM of the airborne system to the integrated configuration management module. The invention relates to an automatic configuration integration method applied to an airborne broadband network system, which can enable the integrated configuration operation to be simpler, reduce the integrated configuration time to be short and enable the integration quality to be high in consistency in the installation, integration and debugging processes of an airborne broadband communication system and an airborne server.
Description
Technical Field
The invention relates to the technical field of airborne broadband networks, in particular to an automatic configuration integration method applied to an airborne broadband network system.
Background
As communication technologies have been developed, airborne communication applications have increased. In the existing civil aviation passenger aircraft, besides the real-time communication between the traditional communication navigation system and the ground, the real-time communication and data transmission services between the airborne systems such as the avionics system, the passenger cabin system, the entertainment system and the information system and the ground network also urge the development and application of various internal and external communication means, including but not limited to: satellite communication, wireless local area network communication, cellular communication, and the like.
The existing onboard broadband communication system and the onboard server are installed, integrated and debugged, engineers in all professional directions are needed, field manual integrated configuration is needed, time consumption is long, and quality consistency is difficult to guarantee.
Therefore, an automatic configuration integration method applied to an airborne broadband network system is provided.
Summary of the invention
1. Technical problem to be solved
Aiming at the problems in the prior art, the invention aims to provide an automatic configuration integration method applied to an airborne broadband network system, which can enable the integrated configuration operation to be simpler, reduce the integrated configuration time to be short and enable the integration quality to be high in consistency in the installation, integration and debugging processes of an airborne broadband communication system and an airborne server.
2. Technical scheme
In order to solve the above problems, the present invention adopts the following technical solutions.
An automatic configuration integration method applied to an airborne broadband network system comprises the following steps:
s1: the automatic integrated configuration device establishes safe encrypted connection with the integrated configuration management module through a communication network 1;
s2: the automatic integrated configuration device sends unique identification information UIM of the airborne system to the integrated configuration management module;
s3: the integrated configuration management module issues the configuration information consistent with the UIM in S2 to the automatic integrated configuration device;
s4: the automatic integrated configuration device is used for carrying out integrated configuration on each module or unit of the airborne system according to the received configuration information, wherein the module or unit at least comprises an airborne wireless hotspot, an airborne server and an airborne broadband communication device;
s5: and the automatic integrated configuration device indicates the airborne wireless hotspot, the airborne server and the airborne broadband communication device to send information to the integrated configuration management module through the communication network 2, and replies the completion of the integrated configuration.
Furthermore, the integrated configuration management module has all airborne system information, a bidirectional security encryption authentication function and a data issuing function which need integrated configuration.
Furthermore, the automatic integrated configuration device has a bidirectional security encryption authentication function and an automatic integrated configuration function for the target system.
Furthermore, the control interface device provides a uniform onboard equipment management interface for the automatic integrated configuration device, and plays roles in addressing and forwarding configuration information.
Further, the communication network 1 is an opened 4G or airport WIFI network, and the communication network 2 is a satellite network that can use encryption.
3. Advantageous effects
Compared with the prior art, the invention has the advantages that:
the technical scheme aims to provide the automatic configuration integration method applied to the airborne broadband network system, so that the integrated configuration operation is simpler, the integrated configuration time is shortened, and the integration quality consistency is high in the installation, integration and debugging processes of the airborne broadband communication system and the airborne server.
Drawings
FIG. 1 is a schematic overall flow chart of the present invention.
Detailed Description
The technical solution in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention; it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all embodiments, and all other embodiments obtained by those skilled in the art without any inventive work are within the scope of the present invention.
Example 1:
referring to fig. 1, an automatic configuration integration method applied to an airborne broadband network system includes the following steps:
s1: the automatic integrated configuration device establishes safe encrypted connection with the integrated configuration management module through a communication network 1; the integrated configuration management module has all airborne system information, a bidirectional security encryption authentication function and a data issuing function which need integrated configuration, and the automatic integrated configuration device has the bidirectional security encryption authentication function and the automatic integrated configuration function for a target system;
s2: the automatic integrated configuration device sends unique identification information UIM of the airborne system to the integrated configuration management module; the control interface device provides a uniform onboard equipment management interface for the automatic integrated configuration device, and plays roles in addressing and forwarding configuration information;
s3: the integrated configuration management module issues the configuration information consistent with the UIM in S2 to the automatic integrated configuration device;
s4: the automatic integrated configuration device is used for carrying out integrated configuration on each module or unit of the airborne system according to the received configuration information, wherein the module or unit at least comprises an airborne wireless hotspot, an airborne server and an airborne broadband communication device;
s5: and the automatic integrated configuration device indicates the airborne wireless hotspot, the airborne server and the airborne broadband communication device to send information to the integrated configuration management module through the communication network 2, and replies the completion of integrated configuration, wherein the communication network 1 is opened 4G or airport WIFI, and the communication network 2 is a satellite network which can use encryption.
In the technical scheme, the communication network 1 is used for establishing safe encrypted connection with the integrated configuration management module, then unique identification information UI of the airborne system is sent to the integrated configuration management module, the integrated configuration management module sends configuration information consistent with UIM in S2 to the automatic integrated configuration device, the automatic integrated configuration device carries out integrated configuration on each module or unit of the airborne system according to the received configuration information, the module or unit at least comprises an airborne wireless hotspot, an airborne server and an airborne broadband communication device, the automatic integrated configuration device indicates the airborne wireless hotspot, the airborne server and the airborne broadband communication device to send information to the integrated configuration management module through the communication network 2, and the integrated configuration is replied to be completed. The integration configuration time is shortened, and the integration quality consistency is high.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (5)
1. An automatic configuration integration method applied to an airborne broadband network system is characterized by comprising the following steps:
s1: the automatic integrated configuration device establishes safe encrypted connection with the integrated configuration management module through a communication network 1;
s2: the automatic integrated configuration device sends unique identification information UIM of the airborne system to the integrated configuration management module;
s3: the integrated configuration management module issues the configuration information consistent with the UIM in S2 to the automatic integrated configuration device;
s4: the automatic integrated configuration device is used for carrying out integrated configuration on each module or unit of the airborne system according to the received configuration information, wherein the module or unit at least comprises an airborne wireless hotspot, an airborne server and an airborne broadband communication device;
s5: and the automatic integrated configuration device indicates the airborne wireless hotspot, the airborne server and the airborne broadband communication device to send information to the integrated configuration management module through the communication network 2, and replies the completion of the integrated configuration.
2. The method of claim 1, wherein the method comprises the following steps: the integrated configuration management module has all airborne system information needing integrated configuration, a bidirectional security encryption authentication function and a data issuing function.
3. The method of claim 1, wherein the method comprises the following steps: the automatic integrated configuration device has a bidirectional security encryption authentication function and an automatic integrated configuration function for a target system.
4. The method of claim 1, wherein the method comprises the following steps: the control interface device provides a uniform onboard equipment management interface for the automatic integrated configuration device, and plays roles in addressing and forwarding configuration information.
5. The method of claim 1, wherein the method comprises the following steps: the communication network 1 is an opened 4G or airport WIFI, and the communication network 2 is a satellite network which can use encryption.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201911363121.1A CN111130884A (en) | 2019-12-26 | 2019-12-26 | Automatic configuration integration method applied to airborne broadband network system |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201911363121.1A CN111130884A (en) | 2019-12-26 | 2019-12-26 | Automatic configuration integration method applied to airborne broadband network system |
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| CN111130884A true CN111130884A (en) | 2020-05-08 |
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| CN106656641A (en) * | 2017-03-21 | 2017-05-10 | 迈普通信技术股份有限公司 | Network device and configuration method thereof |
| CN108462957A (en) * | 2017-02-20 | 2018-08-28 | 中国移动通信有限公司研究院 | A kind of function module initial method and its terminal |
| CN110290015A (en) * | 2019-07-24 | 2019-09-27 | 无锡华云数据技术服务有限公司 | Remote deployment method, apparatus and storage medium |
| CN110493249A (en) * | 2019-08-31 | 2019-11-22 | 天宇经纬（北京）科技有限公司 | Unmanned plane end load real-time control method and system based on multiple network switching |
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- 2019-12-26 CN CN201911363121.1A patent/CN111130884A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104185299A (en) * | 2013-05-23 | 2014-12-03 | 华为终端有限公司 | Near field communication method, user equipment and mobile management entity |
| CN106604247A (en) * | 2016-12-12 | 2017-04-26 | 重庆金美通信有限责任公司 | Method for intelligent registration of second-generation satellite network through Beidou short message channel |
| CN108462957A (en) * | 2017-02-20 | 2018-08-28 | 中国移动通信有限公司研究院 | A kind of function module initial method and its terminal |
| CN106656641A (en) * | 2017-03-21 | 2017-05-10 | 迈普通信技术股份有限公司 | Network device and configuration method thereof |
| CN110290015A (en) * | 2019-07-24 | 2019-09-27 | 无锡华云数据技术服务有限公司 | Remote deployment method, apparatus and storage medium |
| CN110493249A (en) * | 2019-08-31 | 2019-11-22 | 天宇经纬（北京）科技有限公司 | Unmanned plane end load real-time control method and system based on multiple network switching |
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Application publication date: 20200508 |