CN104869072B - A kind of spacecraft bus router of Component- Based Development module - Google Patents
A kind of spacecraft bus router of Component- Based Development module Download PDFInfo
- Publication number
- CN104869072B CN104869072B CN201510201784.9A CN201510201784A CN104869072B CN 104869072 B CN104869072 B CN 104869072B CN 201510201784 A CN201510201784 A CN 201510201784A CN 104869072 B CN104869072 B CN 104869072B
- Authority
- CN
- China
- Prior art keywords
- bus
- component
- intermediate member
- spacecraft
- module
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Classifications
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04L—TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
- H04L45/00—Routing or path finding of packets in data switching networks
- H04L45/74—Address processing for routing
Abstract
A kind of spacecraft bus router of Component- Based Development module, is related to a kind of spacecraft bus router.Existing spacecraft is solved because multibus and the form of depositing bring difficult communication between bus, the problem of causing communication efficiency low.The bus router includes bus registration management module and intermediate member data exchange module, and bus router is communicated with N number of component respectively by multiple bus, N is positive integer, bus registration management module, for managing spacecraft bus registration, bus component subject is extracted, according to component communication mapping table between bus component subject management bus, registers intermediate member;Intermediate member data exchange module includes multiple intermediate members, for realizing the data exchange between intermediate member.It is used primarily in the information communication in spacecraft field.
Description
Technical field
The present invention relates to a kind of spacecraft bus router.
Background technology
At present, to improve versatility, spacecraft tension management uses Component Technology, connected between component by software bus
Connect, preferably to play component generalization advantage, spacecraft employs a plurality of software bus.Spacecraft is because of multibus and deposits form
The problem of bringing difficult communication between bus.
The content of the invention
The present invention is to solve existing spacecraft because multibus and the form of depositing bring difficult communication between bus, cause to communicate
The problem of efficiency is low.The invention provides a kind of spacecraft bus router of Component- Based Development module.
A kind of spacecraft bus router of Component- Based Development module, the bus router include bus registration management mould
Block and intermediate member data exchange module, and bus router is communicated with N number of component respectively by multiple bus, N is just
Integer,
Bus registration management module, for managing spacecraft bus registration, bus component subject is extracted, according to total line components
Component communication mapping table, registers intermediate member between Subject Manager bus;
Intermediate member data exchange module includes multiple intermediate members, for realizing the data exchange between intermediate member.
Described bus registration management module, for managing spacecraft bus registration, bus component subject is extracted, according to total
Component communicates mapping table between line components Subject Manager bus, register the detailed process of intermediate member as:
Spacecraft software bus is total to this bus of bus registration management Module registers, bus router extraction spacecraft software
Line components address,
According to spacecraft software bus component address, bus router seeks bus component subject all over, when a component need to be with
During other total line components communications, communication means are inserted into mapping table, register intermediate member.
The intermediate member data exchange module includes multiple intermediate members, for realizing the data exchange between intermediate member
Detailed process be:
Component communication time slot between wait bus, bus router component mapping table is searched according to component subject,
If without corresponding bus router component mapping list item, terminate this communication;
Otherwise, according to component subject, the component that need to be communicated is sent in the bus where the component that need to be communicated to this, bus
Data exchange is carried out with the intermediate member corresponding to the component that need to be communicated and another intermediate member in router component mapping table, and
Another intermediate member is sent data in other buses beyond the bus needed where communication means,
With needing communication means corresponding by communication means number is read from the bus for receiving another intermediate member and sending data
According to the data exchange between completion intermediate member.
The beneficial effect that the present invention is brought is that the invention provides a kind of spacecraft bus of Component- Based Development module route
Device, the communication between bus is preferably realized, communication efficiency is improved more than 50%.
Brief description of the drawings
Fig. 1 is a kind of principle schematic of the spacecraft bus router of Component- Based Development module of the present invention;
Fig. 2 is the principle schematic that intermediate member 1 and intermediate member 2 carry out data exchange;
Fig. 3 is the flow chart that intermediate member 1 and intermediate member 2 carry out data exchange.
Embodiment
Embodiment one:Illustrate present embodiment, a kind of Component- Based Development mould described in present embodiment referring to Fig. 1
The spacecraft bus router of block, the bus router include bus registration management module and intermediate member data exchange mould
Block, and bus router is communicated with N number of component respectively by multiple bus, N is positive integer,
Bus registration management module, for managing spacecraft bus registration, bus component subject is extracted, according to total line components
Component communication mapping table, registers intermediate member between Subject Manager bus;
Intermediate member data exchange module includes multiple intermediate members, for realizing the data exchange between intermediate member.
Embodiment two:The boat of present embodiment and a kind of Component- Based Development module described in embodiment one
The difference of its device bus router is that described bus registration management module, for managing spacecraft bus registration, extraction is total
Line components theme, component between bus is managed according to bus component subject and communicated mapping table, register the detailed process of intermediate member as:
Spacecraft software bus is total to this bus of bus registration management Module registers, bus router extraction spacecraft software
Line components address,
According to spacecraft software bus component address, bus router seeks bus component subject all over, when a component need to be with
During other total line components communications, communication means are inserted into mapping table, register intermediate member.
Embodiment three:The boat of present embodiment and a kind of Component- Based Development module described in embodiment one
The difference of its device bus router is that the intermediate member data exchange module includes multiple intermediate members, in realization
Between the detailed process of data exchange between component be:
Component communication time slot between wait bus, bus router component mapping table is searched according to component subject,
If without corresponding bus router component mapping list item, terminate this communication;
Otherwise, according to component subject, the component that need to be communicated is sent in the bus where the component that need to be communicated to this, bus
Data exchange is carried out with the intermediate member corresponding to the component that need to be communicated and another intermediate member in router component mapping table, and
Another intermediate member is sent data in other buses beyond the bus needed where communication means,
With needing communication means corresponding by communication means number is read from the bus for receiving another intermediate member and sending data
According to the data exchange between completion intermediate member.In present embodiment, in being illustrated by taking intermediate member 1 and intermediate member 2 as an example
Between data exchange between component principle, referring specifically to Fig. 2;
Component communication time slot between wait bus, bus router component mapping table is searched according to component subject;
If without correspondence mappings list item, terminate this communication;
Otherwise, sent data to according to component subject, component 1 in bus 1, intermediate member 1 reads data from bus 1;
Bus router realizes 1,2 data exchange of intermediate member;
Intermediate member 2 is sent data in bus 2, and counterpart member 2 reads data from bus 2, this sign off, etc.
Treat that next communication time slot arrives.
Intermediate member 1 and intermediate member 2 carry out the workflow diagram of data exchange referring to Fig. 3.
Claims (2)
1. a kind of spacecraft bus router of Component- Based Development module, the spacecraft bus router includes bus registration pipe
Module and intermediate member data exchange module are managed, and spacecraft bus router is carried out with N number of component respectively by multiple bus
Communication, N is positive integer,
Bus registration management module, for managing spacecraft bus registration, component subject is extracted, bus is managed according to component subject
Between component communication mapping table, register intermediate member module;
Intermediate member data exchange module includes multiple intermediate member modules, for realizing that the data of intermediate member intermodule are handed over
Change;
Characterized in that, the intermediate member data exchange module includes multiple intermediate member modules, for realizing intermediate member
The detailed process of the data exchange of intermodule is:
Wait bus between component communication time slot, according to component subject search bus between component communicate mapping table,
If without component communication mapping item between corresponding bus, terminate this communication;
Otherwise, according to component subject, the component that need to be communicated is sent in the bus where the component that need to be communicated to this, structure between bus
In part communication mapping table data friendship is carried out with the intermediate member module corresponding to the component that need to be communicated and another intermediate member module
Change, and another intermediate member module is sent data in other buses beyond the bus needed where communication means,
With needing communication means corresponding by communication means number is read from the bus for receiving another intermediate member module and sending data
According to the data exchange of completion intermediate member intermodule.
2. the spacecraft bus router of a kind of Component- Based Development module according to claim 1, it is characterised in that described
Bus registration management module, for manage spacecraft bus registration, extract component subject, according to component subject manage bus between
Component communicates mapping table, register the detailed process of intermediate member module as:
Spacecraft software bus extracts spacecraft software to this bus of bus registration management Module registers, spacecraft bus router
The component address of bus,
According to the component address of spacecraft software bus, spacecraft bus router seeks component subject all over, when a component need to be with
During other component communications, by component communication mapping table between communication means insertion bus, intermediate member module is registered.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201510201784.9A CN104869072B (en) | 2015-04-25 | 2015-04-25 | A kind of spacecraft bus router of Component- Based Development module |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201510201784.9A CN104869072B (en) | 2015-04-25 | 2015-04-25 | A kind of spacecraft bus router of Component- Based Development module |
Publications (2)
Publication Number | Publication Date |
---|---|
CN104869072A CN104869072A (en) | 2015-08-26 |
CN104869072B true CN104869072B (en) | 2018-01-30 |
Family
ID=53914604
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201510201784.9A Active CN104869072B (en) | 2015-04-25 | 2015-04-25 | A kind of spacecraft bus router of Component- Based Development module |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN104869072B (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107577541A (en) * | 2017-09-05 | 2018-01-12 | 浪潮通用软件有限公司 | A kind of application and a kind of call method of component |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101510827A (en) * | 2009-03-31 | 2009-08-19 | 中国人民解放军信息工程大学 | Routing exchange device, method and method for updating business of routing exchange device |
CN103297542A (en) * | 2013-06-24 | 2013-09-11 | 浪潮电子信息产业股份有限公司 | Operating system bus and balancing method supporting online expansion and retraction of components |
CN104239037A (en) * | 2014-08-25 | 2014-12-24 | 中国电子科技集团公司第二十九研究所 | Software framework with reconfigurable business function |
CN104361424A (en) * | 2014-10-11 | 2015-02-18 | 中国电子科技集团公司第十研究所 | Master data system integration method based on enterprise service bus (ESB) |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB0420673D0 (en) * | 2004-09-17 | 2004-10-20 | Ibm | Data sharing system, method and software tool |
-
2015
- 2015-04-25 CN CN201510201784.9A patent/CN104869072B/en active Active
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101510827A (en) * | 2009-03-31 | 2009-08-19 | 中国人民解放军信息工程大学 | Routing exchange device, method and method for updating business of routing exchange device |
CN103297542A (en) * | 2013-06-24 | 2013-09-11 | 浪潮电子信息产业股份有限公司 | Operating system bus and balancing method supporting online expansion and retraction of components |
CN104239037A (en) * | 2014-08-25 | 2014-12-24 | 中国电子科技集团公司第二十九研究所 | Software framework with reconfigurable business function |
CN104361424A (en) * | 2014-10-11 | 2015-02-18 | 中国电子科技集团公司第十研究所 | Master data system integration method based on enterprise service bus (ESB) |
Also Published As
Publication number | Publication date |
---|---|
CN104869072A (en) | 2015-08-26 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN105245456B (en) | A kind of method and system of the interior unloading SDN virtual network function of Cloud Server | |
CN104484301B (en) | A kind of IO bus units based on FPGA with self-recognition function | |
IN2011CN06800A (en) | ||
CN105956659A (en) | Data processing device, data processing system and server | |
CN103530245B (en) | A kind of SRIO interconnecting and switching device based on FPGA | |
WO2012112460A3 (en) | Offer insertion system | |
CN103346982A (en) | Star-shaped structure Rapid IO interconnecting system and exchanger configuration method thereof | |
CN104731028A (en) | Automatic embedded multi-CPU-board signal exchange method based on signal names | |
CN104869072B (en) | A kind of spacecraft bus router of Component- Based Development module | |
CN103414587A (en) | Method and device for allocating slot positions of rack-mounted device | |
CN102938711A (en) | Internet access information configuration method and network equipment | |
CN105224327A (en) | A kind of embedded equipment variable exchanges transport address off-line distribution method | |
CN107566301A (en) | A kind of method and device realized RapidIO exchange system bus speed and automatically configured | |
CN205230035U (en) | PCIEBox integrated circuit board based on high -end server | |
CN105027518B (en) | Interconnection system for communication equipment | |
CN104104594B (en) | VSU protocol massages are sent and method of reseptance, equipment and system | |
CN206948301U (en) | A kind of switching device of eSIM cards | |
CN104464554A (en) | LED display splicing system splicing unit identification ID generating method | |
CN109166074A (en) | computing system | |
CN104539528B (en) | Multi-core communication equipment and its message interaction method between radius server | |
CN203324391U (en) | General bus test system | |
CN207529315U (en) | A kind of PCIe ReDriver card devices | |
CN202145308U (en) | Multi-master module management interface module of severe-environment-resistant computer | |
CN206977451U (en) | A kind of 1,000,000,000 5 path switching mechanism network interface cards based on PCIeX1 | |
CN105871917A (en) | Transmission control protocol TCP connection scheduling method and device |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
EXSB | Decision made by sipo to initiate substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
GR01 | Patent grant | ||
GR01 | Patent grant |