CN108829386A - A kind of control system of the modularization spaceborne computer based on SCC mode - Google Patents
A kind of control system of the modularization spaceborne computer based on SCC mode Download PDFInfo
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- CN108829386A CN108829386A CN201810662310.8A CN201810662310A CN108829386A CN 108829386 A CN108829386 A CN 108829386A CN 201810662310 A CN201810662310 A CN 201810662310A CN 108829386 A CN108829386 A CN 108829386A
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- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F8/00—Arrangements for software engineering
- G06F8/30—Creation or generation of source code
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- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F13/00—Interconnection of, or transfer of information or other signals between, memories, input/output devices or central processing units
- G06F13/10—Program control for peripheral devices
- G06F13/102—Program control for peripheral devices where the programme performs an interfacing function, e.g. device driver
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- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F9/00—Arrangements for program control, e.g. control units
- G06F9/06—Arrangements for program control, e.g. control units using stored programs, i.e. using an internal store of processing equipment to receive or retain programs
- G06F9/44—Arrangements for executing specific programs
- G06F9/4401—Bootstrapping
- G06F9/4411—Configuring for operating with peripheral devices; Loading of device drivers
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Abstract
The present invention provides a kind of control systems of modularization spaceborne computer based on SCC mode, are related to the technical field of satellite carried computer, including assembly module, service controller and interface controller, wherein the assembly module includes：Hardware layer components and business processing layer assembly；The service controller provides the interface for calling processing service provided by the business processing layer assembly for being managed to the business processing layer assembly；The interface controller is used to control the circulation of data in the control system, and processing service provided by the service controller is called to be handled, fast assembling and extension of the present invention to realize spaceborne computer software, improve satellite batch and produce efficiency and diversified production capacity.
Description
Technical field
The present invention relates to the technical fields of satellite carried computer, more particularly, to a kind of modularization based on SCC mode
The control system of spaceborne computer.
Background technique
With the development of business space flight, the demand for being commercialized microsatellite is increasing.Microsatellite is due to its volume
The features such as weight is small, with short production cycle, functional diversities, existing Satellite Software framework is excessively single and is not easy to asking for extension
Topic highlights, and becomes one of the bottleneck of limitation microsatellite development.
The bottleneck of limitation microsatellite development is mainly reflected in the following aspects：The global variable of software is more, integrally patrols
It is volume soft together, little by little change may cause the exception of entire software；Traditional embedded development personnel weight function and
Framework is not weighed, the coupling of software is strong, pulls one hair and move the whole body；Lead time is long, once there is a little change, due to coupling
Height, the period of electrical property test of satellite can also increase accordingly.
Several big features such as business microsatellite is relatively single with its function, the lead time is ultrashort, business scope covering is wide are right
Traditional spaceborne computer design scheme proposes challenge, and traditional satellite lead time several years easily, system was also too fat to move
Unbearably, how quick composite software, batch produce spaceborne computer software, and guarantee higher reliability, become existing
Technology urgent problem to be solved.
Summary of the invention
In view of this, the purpose of the present invention is to provide a kind of controls of modularization spaceborne computer based on SCC mode
System improves satellite batch and produces efficiency and diversified production capacity to realize the fast assembling and extension of spaceborne computer software.
In a first aspect, the embodiment of the invention provides a kind of control systems of modularization spaceborne computer based on SCC mode
System, including：Assembly module, service controller and interface controller, wherein the assembly module includes：Hardware layer components and industry
Business processing layer assembly；The service controller provides for being managed to the business processing layer assembly and calls the industry
The interface of processing service provided by business processing layer assembly；The interface controller is for controlling data in the control system
Circulation, and processing service provided by the service controller is called to be handled.
Further, the business processing layer assembly includes：Telemetering processing component, remote processing component, program-controlled processing group
Part, time management component, security management component, thermometric management assembly and data handling component；The telemetering processing component is used for
Telemetering processing service is provided；The remote processing group is for providing remote processing service；The program-controlled processing component is for providing
Process control processing service；The time management component is for providing time management service；The security management component is for mentioning
For security management services；The thermometric management assembly is for providing thermometric management service；The data handling component is for providing
Data processing service.
Further, the service controller further includes：Business processing component interface, the business processing component interface point
It is not connected with the service controller and the business processing layer assembly, for calling the business to the service controller
Handle processing service provided by layer assembly.
Further, under different application platforms or different application scene, the processing of the business processing layer assembly is patrolled
Difference is collected, the business processing component interface is identical.
Further, the service controller is also used to carry out seeervice level encapsulation to the business processing component interface, with
The interface controller is set to call processing service provided by the service controller.
Further, the business processing component interface is the interface encapsulated based on company standard specification, enterprise's mark
Quasi- specification for reality the business processing component that be abstracted of satellite model standard interface agreement.
Further, the bussiness processing layer being connected by identical business processing component interface with the service controller
Between component, it is able to carry out plug replacement.
Further, the system also includes：Hardware Interface Module, wherein the Hardware Interface Module is for realizing institute
State the communication connection of interface controller and the hardware layer components.
Further, the Hardware Interface Module includes at least one of：CAN bus, I2C bus, UART bus,
Spi bus, OC switch block, AD acquisition component.
Further, the system also includes：Hardware drive module, for passing through the Hardware Interface Module and described hard
Part layer assembly is connected, and is configured with the driving to hardware layer related hardware.
Control system provided by the embodiment of the present invention is a kind of modularization spaceborne computer software based on SCC mode
Control system, basic thought of the control system based on SCC design pattern, according to service controller, interface controller and component
The big nucleus module of module design etc. three is packaged the control system of spaceborne computer.Service controller (Service) is system
One maintenance business processing parts, externally provide service call interface；Interface controller (Controler) is control stream compression
Core component, the data of hardware layer components are integrated by interface controller and call relevant business processing logic；Group
Hardware layer, bussiness processing layer are carried out modular design by part module (Component), and the standardization for having taken out enterprise connects
Mouthful, using standard interface as constraint.By above-mentioned processing mode, the present invention realizes the fast assembling and expansion of spaceborne computer software
Exhibition improves satellite batch and produces efficiency and diversified production capacity.
Other features and advantages of the present invention will illustrate in the following description, also, partly become from specification
It obtains it is clear that understand through the implementation of the invention.The objectives and other advantages of the invention are in specification, claims
And specifically noted structure is achieved and obtained in attached drawing.
To enable the above objects, features and advantages of the present invention to be clearer and more comprehensible, preferred embodiment is cited below particularly, and cooperate
Appended attached drawing, is described in detail below.
Detailed description of the invention
It, below will be to specific in order to illustrate more clearly of the specific embodiment of the invention or technical solution in the prior art
Embodiment or attached drawing needed to be used in the description of the prior art be briefly described, it should be apparent that, it is described below
Attached drawing is some embodiments of the present invention, for those of ordinary skill in the art, before not making the creative labor
It puts, is also possible to obtain other drawings based on these drawings.
Fig. 1 is a kind of control system of modularization spaceborne computer based on SCC mode according to an embodiment of the present invention
Schematic diagram；
Fig. 2 be it is according to an embodiment of the present invention the first be optionally based on the control of the modularization spaceborne computer of SCC mode
The schematic diagram of system processed；
Fig. 3 is the control of the second according to an embodiment of the present invention modularization spaceborne computer for being optionally based on SCC mode
The schematic diagram of system processed.
Specific embodiment
In order to make the object, technical scheme and advantages of the embodiment of the invention clearer, below in conjunction with attached drawing to the present invention
Technical solution be clearly and completely described, it is clear that described embodiments are some of the embodiments of the present invention, rather than
Whole embodiments.Based on the embodiments of the present invention, those of ordinary skill in the art are not making creative work premise
Under every other embodiment obtained, shall fall within the protection scope of the present invention.
According to embodiments of the present invention, a kind of control system of modularization spaceborne computer based on SCC mode is provided
Embodiment of the method, it should be noted that step shown in the flowchart of the accompanying drawings can be in the executable finger of such as one group of computer
It is executed in the computer system of order, although also, logical order is shown in flow charts, and it in some cases, can be with
The steps shown or described are performed in an order that is different from the one herein.
Fig. 1 is a kind of control system of modularization spaceborne computer based on SCC mode according to an embodiment of the present invention
Schematic diagram, as shown in Figure 1, the system includes：Assembly module 10, service controller 20 and interface controller 30.Wherein, described group
Part module includes：Hardware layer components 11 and business processing layer assembly 12.
Specifically, the service controller is for being managed the business processing layer assembly, and provides described in calling
The interface of processing service provided by business processing layer assembly；
The interface controller is used to control the circulation of data in the control system, and calls the service controller institute
The processing service of offer is handled.Specifically, the data interaction of hardware layer components has been carried out specification and whole by interface controller
It closes, according to data routing Design, calls corresponding service interface, data are handled and are stored.
Control system provided by the embodiment of the present invention is a kind of modularization spaceborne computer software based on SCC mode
Control system, basic thought of the control system based on SCC design pattern, according to service controller, interface controller and component
The big nucleus module of module design etc. three is packaged the control system of spaceborne computer.Service controller (Service) is system
One maintenance business processing parts, externally provide service call interface；Interface controller (Controler) is control stream compression
Core component, the data of hardware layer components are integrated by interface controller and call relevant business processing logic；Group
Hardware layer, bussiness processing layer are carried out modular design by part module (Component), and the standardization for having taken out enterprise connects
Mouthful, using standard interface as constraint.By above-mentioned processing mode, the present invention realizes the fast assembling and expansion of spaceborne computer software
Exhibition improves satellite batch and produces efficiency and diversified production capacity.
In the present embodiment, as shown in Fig. 2, business processing layer assembly 12 includes：Telemetering processing component 121, remote processing
Component 122, program-controlled processing component 123, time management component 124, security management component 125, thermometric management assembly 126 and data
Processing component 127.
The telemetering processing component 121 is for providing telemetering processing service；
The remote processing component 122 is for providing remote processing service；
The program-controlled processing component 123 is for providing process control processing service；
The time management component 124 is for providing time management service；
The security management component 125 is for providing security management services；
The thermometric management assembly 126 is for providing thermometric management service；
The data handling component 127 is for providing data processing service, wherein the data processing refers to significant data
It is handled, the content of specific significant data can be set according to actual needs.
In the present embodiment, as shown in Fig. 2, service controller 20 further includes：Business processing component interface 21.
The business processing component interface 21 is for realizing between the service controller and the business processing layer assembly
Connection, service is handled provided by the business processing layer assembly for calling to the service controller.
In an optional embodiment, under different application platforms or different application scene, the business processing
The processing logic of layer assembly is different, and the business processing component interface is identical.Business processing component interface is based on company standard
Standardize the interface of encapsulation, the company standard specification be to reality the business processing group that is abstracted of satellite model
The standard interface of part is arranged.
Specifically, business processing component is designed according to enterprise standardization specification, different platform, load and application scenarios
Under, the business processing logic of component is not necessarily identical, but Interface design is identical, and the component of same-interface can be replaced mutually
Generation.
In an optional embodiment, the service controller is also used to carry out the business processing component interface
Seeervice level encapsulation, so that the interface controller calls processing service provided by the service controller.
Specifically, service controller module has business processing assembly management function, by the external interface of various components into
The encapsulation of row seeervice level, is called for interface controller.
In an optional embodiment, it is connected by identical business processing component interface with the service controller
Between the business processing layer assembly connect, it is able to carry out plug replacement.
Specifically, in the present embodiment, enterprise standardization specification is enterprise according to reality model be abstracted,
The standard interface agreement of the bottom component, business processing component that extract, based on the component that interface protocol is realized, same-interface
Between component support plug replacement.
In an optional embodiment, as shown in Fig. 2, the system also includes：Hardware Interface Module 40, wherein
The Hardware Interface Module for realizing the interface controller and the hardware layer components communication connection.
Optionally, the Hardware Interface Module includes at least one of：CAN bus, I2C bus, UART bus, SPI
Bus, OC switch block, AD acquisition component.
In an optional embodiment, as shown in Fig. 2, the system also includes：Hardware drive module 50, for leading to
It crosses the Hardware Interface Module to be connected with the hardware layer components, be configured with the driving to hardware layer related hardware.
Specifically, hardware driving unit module, according to the common processor chips of microsatellite, driving relevant to hardware
It is configured, the support as bottom component.
Compared with the prior art, the invention has the advantages that：
The present invention is based on the design patterns of SCC, have carried out framework again to spaceborne computer software, have improved the mould of software
Block reduces coupling, convenient for the replacement between module, reduces bring security risk due to software modification.
Software effectively may be potentially isolated to modules, in component by the present invention extremely, improve system
Reliability is reduced because software modification brings the coverage of abnormal problem.
The present invention improves the production efficiency of microsatellite, substantially reduces the production cycle by architecture design.
General business and hardware have been carried out Groupware encapsulation by the present invention, and the general service of system is allowed to pass through type
It number is constantly accumulated, the reusable degree of nucleus module for once improving enterprise is only used compared to traditional model number software.
Fig. 3 is a kind of control system of modularization spaceborne computer based on SCC mode according to an embodiment of the present invention
Schematic diagram, as shown in figure 3, the system includes：
Business processing component specifically includes telemetering processing component, remote processing component, program-controlled processing component, time management
Component, security management component, thermometric management assembly and data handling component etc.；
The company standard specification of a set of business processing parts interface；
Service controller is managed and integrates to business processing component, externally provides business processing service；
Interface controller, controls the stream compression of entire spaceborne computer, the data of each slave computer, spaceborne computer from
The data of body are uniformly integrated by interface controller, and the service for calling service controller to provide is handled；
Hardware driving unit module configures the ARM chip of different model, as entire spaceborne computer software system
The supporting module of system；
The company standard specification of a set of Hardware Interface Module；
One group of Hardware Interface Module, including CAN bus, I2C bus, UART bus, spi bus, OC switch block, AD are adopted
Collect component etc..
Optionally, in the present embodiment, business processing component is designed according to enterprise standardization specification, different platform,
Under load and application scenarios, the business processing logic of component is not necessarily identical, but Interface design is identical, the component of same-interface
It can be substituted for each other.
Optionally, in the present embodiment, service controller module has business processing assembly management function, by each group
The external interface of part carries out seeervice level encapsulation, calls for interface controller.
Optionally, in the present embodiment, enterprise standardization specification is enterprise according to reality model be abstracted,
The standard interface agreement of the bottom component, business processing component that extract, based on the component that interface protocol is realized, same-interface
Between component support plug replacement.
Optionally, in the present embodiment, hardware driving unit module, it is right according to the common processor chips of microsatellite
The relevant driving of hardware is configured, the support as bottom component.
In addition, in the description of the embodiment of the present invention unless specifically defined or limited otherwise, term " installation ", " phase
Even ", " connection " shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection, or be integrally connected；It can
To be mechanical connection, it is also possible to be electrically connected；It can be directly connected, can also can be indirectly connected through an intermediary
Connection inside two elements.For the ordinary skill in the art, above-mentioned term can be understood at this with concrete condition
Concrete meaning in invention.
In the description of the present invention, it should be noted that term " center ", "upper", "lower", "left", "right", "vertical",
The orientation or positional relationship of the instructions such as "horizontal", "inner", "outside" be based on the orientation or positional relationship shown in the drawings, merely to
Convenient for description the present invention and simplify description, rather than the device or element of indication or suggestion meaning must have a particular orientation,
It is constructed and operated in a specific orientation, therefore is not considered as limiting the invention.In addition, term " first ", " second ",
" third " is used for descriptive purposes only and cannot be understood as indicating or suggesting relative importance.
It is apparent to those skilled in the art that for convenience and simplicity of description, the system of foregoing description,
The specific work process of device and unit, can refer to corresponding processes in the foregoing method embodiment, and details are not described herein.
In several embodiments provided herein, it should be understood that disclosed systems, devices and methods, it can be with
It realizes by another way.The apparatus embodiments described above are merely exemplary, for example, the division of the unit,
Only a kind of logical function partition, there may be another division manner in actual implementation, in another example, multiple units or components can
To combine or be desirably integrated into another system, or some features can be ignored or not executed.Another point, it is shown or beg for
The mutual coupling, direct-coupling or communication connection of opinion can be through some communication interfaces, device or unit it is indirect
Coupling or communication connection can be electrical property, mechanical or other forms.
The unit as illustrated by the separation member may or may not be physically separated, aobvious as unit
The component shown may or may not be physical unit, it can and it is in one place, or may be distributed over multiple
In network unit.It can select some or all of unit therein according to the actual needs to realize the mesh of this embodiment scheme
's.
It, can also be in addition, the functional units in various embodiments of the present invention may be integrated into one processing unit
It is that each unit physically exists alone, can also be integrated in one unit with two or more units.
It, can be with if the function is realized in the form of SFU software functional unit and when sold or used as an independent product
It is stored in the executable non-volatile computer-readable storage medium of a processor.Based on this understanding, of the invention
Technical solution substantially the part of the part that contributes to existing technology or the technical solution can be with software in other words
The form of product embodies, which is stored in a storage medium, including some instructions use so that
One computer equipment (can be personal computer, server or the network equipment etc.) executes each embodiment institute of the present invention
State all or part of the steps of method.And storage medium above-mentioned includes：USB flash disk, mobile hard disk, read-only memory (ROM, Read-
Only Memory), random access memory (RAM, Random Access Memory), magnetic or disk etc. are various can be with
Store the medium of program code.
Finally it should be noted that：Embodiment described above, only a specific embodiment of the invention, to illustrate the present invention
Technical solution, rather than its limitations, scope of protection of the present invention is not limited thereto, although with reference to the foregoing embodiments to this hair
It is bright to be described in detail, those skilled in the art should understand that：Anyone skilled in the art
In the technical scope disclosed by the present invention, it can still modify to technical solution documented by previous embodiment or can be light
It is readily conceivable that variation or equivalent replacement of some of the technical features；And these modifications, variation or replacement, do not make
The essence of corresponding technical solution is detached from the spirit and scope of technical solution of the embodiment of the present invention, should all cover in protection of the invention
Within the scope of.Therefore, the protection scope of the present invention shall be subject to the protection scope of the claims.
Claims (10)
1. a kind of control system of the modularization spaceborne computer based on SCC mode, which is characterized in that including：Assembly module, industry
It is engaged in controller and interface controller, wherein the assembly module includes：Hardware layer components and business processing layer assembly；
The service controller provides for being managed to the business processing layer assembly and calls the bussiness processing layer group
The interface of processing service provided by part；
The interface controller is used to control the circulation of data in the control system, and the service controller is called to be provided
Processing service handled.
2. control system according to claim 1, which is characterized in that the business processing layer assembly includes：Telemetering processing
Component, remote processing component, program-controlled processing component, time management component, security management component, at thermometric management assembly and data
Manage component；
The telemetering processing component is for providing telemetering processing service；The remote processing group is for providing remote processing service；
The program-controlled processing component is for providing process control processing service；The time management component is for providing time management clothes
Business；The security management component is for providing security management services；The thermometric management assembly is for providing thermometric management service；
The data handling component is for providing data processing service.
3. control system according to claim 1, which is characterized in that the service controller further includes：
Business processing component interface, the business processing component interface is for realizing the service controller and the business processing
Connection between layer assembly handles service for calling to the service controller provided by the business processing layer assembly.
4. control system according to claim 3, which is characterized in that in different application platforms or different application scene
Under, the processing logic of the business processing layer assembly is different, and the business processing component interface is identical.
5. control system according to claim 3, which is characterized in that the service controller is also used to at the business
It manages component interface and carries out seeervice level encapsulation, so that the interface controller calls processing clothes provided by the service controller
Business.
6. control system according to claim 3, which is characterized in that the business processing component interface is to be marked based on enterprise
The interface of quasi- specification encapsulation, the company standard specification be to reality the business processing that is abstracted of satellite model
The standard interface of component is arranged.
7. control system according to claim 3, which is characterized in that by identical business processing component interface with it is described
Between the business processing layer assembly that service controller is connected, it is able to carry out plug replacement.
8. control system according to claim 1, which is characterized in that the system also includes：
Hardware Interface Module, wherein the Hardware Interface Module is for realizing the interface controller and the hardware layer components
Communication connection.
9. control system according to claim 8, which is characterized in that the Hardware Interface Module include it is following at least it
One：CAN bus, I2C bus, UART bus, spi bus, OC switch block, AD acquisition component.
10. control system according to claim 1, which is characterized in that the system also includes：
Hardware drive module, for being connected by the Hardware Interface Module with the hardware layer components, to hardware layer phase
The driving for closing hardware is configured.
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Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102841966A (en) * | 2012-08-28 | 2012-12-26 | 曾安里 | Vpp-STK satellite simulation development and operation platform system |
| CN102999331A (en) * | 2012-11-13 | 2013-03-27 | 北京空间飞行器总体设计部 | Hardware blocking layer of onboard software and onboard data communication method |
| CN104750475A (en) * | 2013-12-31 | 2015-07-01 | 深圳航天东方红海特卫星有限公司 | Micro satellite on-orbit reconstruction frame system and method |
| CN105487867A (en) * | 2015-11-26 | 2016-04-13 | 中国空间技术研究院 | Lightweight visual satellite testing program design system and method |
| CN105739416A (en) * | 2016-05-06 | 2016-07-06 | 上海航天测控通信研究所 | Satellite-borne comprehensive electronic computer |
| CN106598019A (en) * | 2016-10-31 | 2017-04-26 | 航天东方红卫星有限公司 | Satellite housekeeping simulator and simulation method for development and test of micro-nano satellite control module |
| CN107943459A (en) * | 2017-11-20 | 2018-04-20 | 中国运载火箭技术研究院 | A kind of generalization spacecraft Integrated Electronic System |
| CN108153374A (en) * | 2017-12-26 | 2018-06-12 | 中国空间技术研究院 | A kind of high rail satellite integrated electronics computer system and control method |
-
2018
- 2018-06-25 CN CN201810662310.8A patent/CN108829386A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102841966A (en) * | 2012-08-28 | 2012-12-26 | 曾安里 | Vpp-STK satellite simulation development and operation platform system |
| CN102999331A (en) * | 2012-11-13 | 2013-03-27 | 北京空间飞行器总体设计部 | Hardware blocking layer of onboard software and onboard data communication method |
| CN104750475A (en) * | 2013-12-31 | 2015-07-01 | 深圳航天东方红海特卫星有限公司 | Micro satellite on-orbit reconstruction frame system and method |
| CN105487867A (en) * | 2015-11-26 | 2016-04-13 | 中国空间技术研究院 | Lightweight visual satellite testing program design system and method |
| CN105739416A (en) * | 2016-05-06 | 2016-07-06 | 上海航天测控通信研究所 | Satellite-borne comprehensive electronic computer |
| CN106598019A (en) * | 2016-10-31 | 2017-04-26 | 航天东方红卫星有限公司 | Satellite housekeeping simulator and simulation method for development and test of micro-nano satellite control module |
| CN107943459A (en) * | 2017-11-20 | 2018-04-20 | 中国运载火箭技术研究院 | A kind of generalization spacecraft Integrated Electronic System |
| CN108153374A (en) * | 2017-12-26 | 2018-06-12 | 中国空间技术研究院 | A kind of high rail satellite integrated electronics computer system and control method |
Non-Patent Citations (1)
| Title |
|---|
| 徐伟，朴永杰: "从Pleiades剖析新一代高性能小卫星技术发展", 《中国光学》 * |
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Application publication date: 20181116 |