CN110518420A - A kind of connector, satellite system, Star Service subsystem, Star Service host and method - Google Patents
A kind of connector, satellite system, Star Service subsystem, Star Service host and method Download PDFInfo
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- CN110518420A CN110518420A CN201910820950.1A CN201910820950A CN110518420A CN 110518420 A CN110518420 A CN 110518420A CN 201910820950 A CN201910820950 A CN 201910820950A CN 110518420 A CN110518420 A CN 110518420A
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- star service
- connector
- cable
- star
- subsystem
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01R—ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
- H01R13/00—Details of coupling devices of the kinds covered by groups H01R12/70 or H01R24/00 - H01R33/00
- H01R13/02—Contact members
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01R—ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
- H01R13/00—Details of coupling devices of the kinds covered by groups H01R12/70 or H01R24/00 - H01R33/00
- H01R13/46—Bases; Cases
- H01R13/502—Bases; Cases composed of different pieces
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01R—ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
- H01R27/00—Coupling parts adapted for co-operation with two or more dissimilar counterparts
- H01R27/02—Coupling parts adapted for co-operation with two or more dissimilar counterparts for simultaneous co-operation with two or more dissimilar counterparts
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01R—ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
- H01R31/00—Coupling parts supported only by co-operation with counterpart
- H01R31/06—Intermediate parts for linking two coupling parts, e.g. adapter
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- Management, Administration, Business Operations System, And Electronic Commerce (AREA)
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Abstract
The embodiment of the present application provides a kind of connector, satellite system, Star Service subsystem, Star Service host and method.The satellite system includes Star Service host and Star Service subsystem, the both ends of the connector are separately connected the Star Service host and the Star Service subsystem, the connector includes connecting line and the connector that is connected with the connecting line, the connecting line includes multi-cable, the multi-cable includes the cable for being used for transmission data and the cable for being used for transmission electric energy, the connector is made of hard material, power supply terminal and data terminal are integrated on the connector, the cable that electric energy is used for transmission in the power supply terminal and the multi-cable is connected, the data terminal with the cable for being used for transmission data in the multi-cable for being connected.Since power supply terminal and data terminal are all integrated on connector by the present invention, electrically connected and data connection just only can be completed by a connecting moves, convenient for operation.
Description
Technical field
This application involves satellite technology fields, in particular to a kind of connector, satellite system, Star Service subsystem, star
Business host and method.
Background technique
Satellite system generally includes Star Service host and multiple Star Service subsystems, and the Star Service host is for managing the Star Service
Subsystem, the Star Service subsystem for example including position and attitude control subsystem, communication subsystem, temperature control subsystem,
Power subsystem, storage subsystem, load subsystem (for remote sensing satellite, load subsystem can be camera subsystem) etc..
In current traditional satellite system, the Star Service host and the Star Service subsystem and the Star Service point are
It between system and the Star Service subsystem, requires to be attached by cable, and is used for transmission the cable of electric energy and for passing
The cable of transmission of data needs to be attached respectively.Therefore there is connections often, connects inconvenient problem.
Summary of the invention
The embodiment of the present application is designed to provide a kind of connector, satellite system, Star Service subsystem, Star Service host and side
Method, to reduce the action frequency of connecting cable.
In a first aspect, being used for satellite system, the satellite system includes Star Service host this application provides a kind of connector
With Star Service subsystem, the both ends of the connector are separately connected the Star Service host and the Star Service subsystem, the connector
Including connecting line and the connector being connected with the connecting line, the connecting line includes multi-cable, and the multi-cable includes
It is used for transmission the cable of data and is used for transmission the cable of electric energy, the connector is made of hard material, the connector
On be integrated with power supply terminal and data terminal, the cable phase of electric energy is used for transmission in the power supply terminal and the multi-cable
Even, the data terminal with the cable for being used for transmission data in the multi-cable for being connected.
In the embodiment of the present application, since power supply terminal and data terminal to be all integrated on connector, so that Star Service master
Only need a connecting moves that can complete the company of electric power and data between machine and Star Service subsystem and Star Service subsystem
It connects.
With reference to first aspect, in the first possible implementation kind, the power supply terminal includes main power supply terminal and standby
Power supply terminal, the main power supply terminal and the available electric terminal receive the supply voltage of same size from the Star Service host；
The data terminal includes master data terminal and standby data terminal, and the master data terminal and the standby data terminal are from the star
Business host receives identical Star Service data.
In the embodiment of the present application, Star Service host is loaded together by independent to main power supply terminal and available electric terminal respectively
The supply voltage of one size, when guaranteeing to have in main power supply terminal and available electric terminal any one terminal to damage, additionally it is possible to logical
Crossing remaining terminal normally is the power supply of Star Service subsystem, improves the stability of satellite operation.In addition, Star Service host is by independent
Identical Star Service data are provided to master data terminal and standby data terminal, to guarantee to have in master data terminal and standby data terminal
When people's one terminal damage, additionally it is possible to by remaining terminal normally be that satellite system transmits data, improve the steady of satellite operation
It is qualitative.
With reference to first aspect, in the second possible implementation, the connector supports network protocol.
In the embodiment of the present application, since connector supports network protocol, different types of Star Service data that can lead to
It crosses different types of data packet to be distinguish, without being distinguished by different data/address bus, therefore can reduce
The multi-cable being arranged to build multiple bus.On the one hand the reduction of number of cables can mitigate the weight of cable on satellite
Amount saves resource, and being on the other hand conducive to the promptly positioning in debugging process, there are the cables of failure.
With reference to first aspect, in the third possible implementation, the connector further includes protective case, the protection
Set is for wrapping up the multi-cable.
In the embodiment of the present application, since the protective case that connector provides wraps up multi-cable, Star Service host can be reduced
When connecting with Star Service subsystem, it is exposed to the quantity of outer cable, the probability of cable aging breakage is reduced, improves the steady of satellite operation
It is qualitative.Further, since multi-cable is bundled together with a protective case, it can avoid each cable and spread out and other devices
The cable for causing extension to drag, while being bundled together is also convenient for grabbing.
With reference to first aspect, in the fourth possible implementation, protective case is made of rigid material.
In the embodiment of the present application, it is made due to protective case of rigid material, it can be in order to which connecting line be on satellite
Mechanical erection.
Second aspect, this application provides a kind of satellite systems, comprising: Star Service host, Star Service subsystem and such as first
Connector described in any possible implementation of aspect and first aspect, the Star Service host is for controlling the star
Business subsystem, the Star Service subsystem are connected to receive the electricity of Star Service host offer with the Star Service host by the connector
The data that can and transmit.
In conjunction with second aspect, in the first possible implementation, the Star Service subsystem and the Star Service host it
Between data are transmitted using network protocol, a Star Service subsystem in the Star Service subsystem by the Star Service host and its
He exchanges data at Star Service subsystem.In the embodiment of the present application, due to using net between Star Service subsystem and the Star Service host
Network agreement transmits data, therefore can avoid the need for transmitting different data using a variety of data protocols, so as to avoid
Data are transmitted using multi-cable in order to transmit the data of various protocols in the prior art, so as to save the number of cable
Amount.Further, since each Star Service subsystem is to be interacted by Star Service host with other Star Service subsystems, rather than pass through cable
It is individually connect with other Star Service subsystems on satellite, so as to be further reduced the usage quantity of cable on satellite.Cable
On the one hand the reduction of quantity can mitigate the weight of cable on satellite, save resource, be on the other hand conducive in debugging process
Promptly determine that there are the cables of failure.
The third aspect, this application provides a kind of Star Service subsystems, comprising:
There is a connecting line, the connecting line includes multi-cable, wherein the more electricity in the Star Service subsystem
Cable includes the cable for being used for transmission data and the cable for being used for transmission electric energy, and the connecting line is connected with connector, the company
It is integrated with power supply terminal and data terminal on connector, the cable phase of electric energy is used for transmission in the power supply terminal and the connecting line
Even, the data terminal with the cable for being used for transmission data in the connecting line for being connected, and the connector is used for and Star Service
Host connects firmly.
Fourth aspect, this application provides a kind of Star Service hosts, comprising:
There is a connecting line, the connecting line includes multi-cable, wherein the multi-cable on the Star Service host
Including being used for transmission the cable of data and being used for transmission the cable of electric energy, the connecting line is connected with connector, the connection
It is integrated with power supply terminal and data terminal on head, the cable phase of electric energy is used for transmission in the power supply terminal and the connecting line
Even, the data terminal with the cable for being used for transmission data in the connecting line for being connected, and the connector is used for and Star Service
Subsystem connects firmly.
5th aspect, this application provides a kind of Star Service data interactive method of satellite system, the satellite system includes
Star Service host, Star Service subsystem and the connection as described in any possible implementation of first aspect and first aspect
Device, the Star Service subsystem are connected by the connector with the Star Service host, and the method is applied to Star Service host, described
Method includes:
Receiving a Star Service of the other Star Service subsystems in the Star Service subsystem into the Star Service subsystem
When the subsystem access request that subsystem is sent, judge whether other subsystems have the one Star Service subsystem of access
Permission；
Working condition is adjusted to from dormant state if so, then controlling one Star Service subsystem, then by the subsystem
Access request is sent to one Star Service subsystem.
In this embodiment, the data that a Star Service subsystem passes through Star Service host and other Star Service subsystems are realized
Exchange.Star Service subsystem in a dormant state, can save electric power when not working.Star Service host is only judging other Star Services point
System just starts Star Service subsystem in a dormant state when having access authority, avoids unnecessary starting, so as into
One step saves electric power.
Detailed description of the invention
Technical solution in ord to more clearly illustrate embodiments of the present application will make below to required in the embodiment of the present application
Attached drawing is briefly described, it should be understood that the following drawings illustrates only some embodiments of the application, therefore should not be seen
Work is the restriction to range, for those of ordinary skill in the art, without creative efforts, can be with
Other relevant attached drawings are obtained according to these attached drawings.
Fig. 1 is a kind of structural block diagram of satellite system provided by the embodiments of the present application；
Fig. 2 is a kind of first structure diagram of satellite system provided by the embodiments of the present application；
Fig. 3 is a kind of second structural schematic diagram of satellite system provided by the embodiments of the present application；
Fig. 4 is a kind of third structural schematic diagram of satellite system provided by the embodiments of the present application；
Fig. 5 is a kind of 4th structural schematic diagram of satellite system provided by the embodiments of the present application；
Fig. 6 is the structural schematic diagram of connector in a kind of satellite system provided by the embodiments of the present application；
Fig. 7 is the structural schematic diagram of contact surface on connector in a kind of satellite system provided by the embodiments of the present application；
Fig. 8 is a kind of 5th structural schematic diagram of satellite system provided by the embodiments of the present application；
Fig. 9 is a kind of 6th structural schematic diagram of satellite system provided by the embodiments of the present application；
Figure 10 is a kind of first pass figure of Star Service data interactive method provided by the embodiments of the present application；
Figure 11 is a kind of second flow chart of Star Service data interactive method provided by the embodiments of the present application；
Figure 12 is a kind of third flow chart of Star Service data interactive method provided by the embodiments of the present application.
Icon: 10- satellite system；100- connector；110- connector；111- head end；The end face 1111-；112- tail end；
113- protective shell；120- connecting line；121- protective case；130- power supply terminal；140- data terminal；150- ground terminal；200-
Star Service host；300- Star Service subsystem.
Specific embodiment
Below in conjunction with the attached drawing in the embodiment of the present application, technical solutions in the embodiments of the present application is described.
Referring to Fig. 1, some embodiments of the present application provide a kind of satellite system 10, which can be installed
On satellite, satellite can be traditional satellite or emerging cube star, the satellite system 10 may include: connector 100,
Star Service host 200 and Star Service subsystem 300.Star Service host 200 can be the primary control on satellite, Star Service subsystem
300 are connected by connector 100 with Star Service host 200.
It should be noted that can be according to actual application scenarios needs on satellite, one or more Star Services point, which are arranged, is
Simultaneously connector 100 identical with 300 quantity of Star Service subsystem is arranged in system 300.One Star Service subsystem 300 and a connector
100 is corresponding.When in satellite system 10 including multiple Star Service subsystems 300, each Star Service subsystem 300 passes through respective company respectively
Device 100 is connect to be connected with Star Service host 200.Star Service host 200 can be corresponding Star Service subsystem 300 by each connector 100
Power supply and transmission data.
In addition, Star Service host 200 can form local by each connector 100 and all Star Service subsystems 300 together
Net, in this way, Star Service host 200 can control the operation of each Star Service subsystem 300 in local area network, each Star Service subsystem 300
It can be interacted by Star Service host 200 with other Star Service subsystems 300.
It is understood that since each Star Service subsystem 300 is big in such a way that connector 100 connects Star Service host 200
Cause it is identical, for avoid it is tired state, the present embodiment connects a Star Service master by a connector 100 with a Star Service subsystem 300
For machine 200, to the connection structure of connector 100, Star Service host 200 how to be powered for Star Service subsystem 300 and Star Service master
How machine 200, which controls the operation of Star Service subsystem 300, is described in detail.
As shown in Fig. 2, connector 100 includes connecting line 120 in some possible implementations, connecting line 120 includes phase
Pair first end and second end, the first end is the one end connecting with the Star Service subsystem 300, and the second end is and star
One end that business host 200 connects.
As shown in figure 3, in one embodiment, the connector 100 further includes connector 110, the connecting line 120
First end be connected with the connector 110, connect by connector 110 with Star Service subsystem 300, the connecting line 120
Second end is directly connect with Star Service host 200.
As shown in figure 4, in another embodiment, 120 first end of connecting line is directly connect with Star Service subsystem 300,
120 second end of connecting line is connected with connector 110, is connect by connector 110 with Star Service host 200.
As shown in figure 5, in another embodiment, first end is connect by connector 110 with Star Service subsystem 300,
Second end is connect by connector 110 with Star Service host 200.
With reference to Fig. 2-Fig. 5, more cables are enclosed in connecting line 120.To avoid cable damage, wrapped up on connecting line 120
The protective case 121 of more cables can be made such as rubber material and be made by flexible, wear-resisting and corrosion-resistant material.In addition,
For the mechanical erection convenient for connecting line 120 on satellite, protective case 121 can also use rigid, wear-resisting and resistant material system
It is made at such as titanium alloy material.
Referring to Fig. 6, when connecting line 120 is connected by connector 110 with 300/ Star Service host 200 of Star Service subsystem,
First terminal corresponding with the cable is connected each cable in connecting line 120 respectively and on connector 110, the terminal of connector 110
It is connected again with the terminal of 300/ Star Service host 200 of Star Service subsystem.Hereinafter, also that the connection of terminal and terminal is referred to as hard
It connects.When connecting line 120 is directly connected with 300/ Star Service host 200 of Star Service subsystem, each cable in connecting line 120 directly with
The terminal of 300/ Star Service host 200 of Star Service subsystem is connected.Hereinafter, the connection of cable and terminal is also known as soft connect.
Connector 110 can be strip structure made of hard material, (no for example, by using highstrenghtpiston, alloy material
Rust steel, titanium alloy etc.) etc. materials be made.Since connector 110 is strip structure, therefore connector 110 has opposite both ends,
In, one end is head end 111, and the other end is tail end 112.
For the head end 111 convenient for connector 110 can by way of plug with 200/ Star Service subsystem 300 of Star Service host
It connects firmly, is integrated with terminal on the end face 1111 of the head end 111 of connector 110.
Optionally, in the present embodiment, connector 110 can also include: protective shell.Protective shell can be set in end face
On 1111, by the terminal protecting integrated on end face 1111 in shell.And it is in connector 100 and 200/ Star Service of Star Service host point
When system 300 connects firmly, protective shell 113 can be by fixing in the slot in insertion 200/ Star Service subsystem 300 of Star Service host
Connector 110 guarantees the stability connect firmly.
In conjunction with Fig. 6, and refering to Fig. 7, in the present embodiment, the terminal integrated on connector 110 may include: power supply terminal
130 and data terminal 140.
Illustratively, power supply terminal 130 can be multiple, and multiple power supply terminals 130 are segmented into main 130 He of power supply terminal
Available electric terminal 130.After the terminal and Star Service host 200 integrated on connector 100 connects firmly, Star Service host 200 is used for will be same
One supply voltage is loaded into main power supply terminal 130 and available electric terminal 130 respectively, to pass through main power supply terminal 130 and available electricity
Terminal 130 again loads supply voltage to Star Service subsystem 300, guarantees the normal power supply of Star Service subsystem 300.
Illustratively, Star Service subsystem 300 runs the voltage that various businesses need all size, therefore Star Service host 200 is also
It can be the supply voltage that Star Service subsystem 300 loads all size by multiple power supply terminals 130.For example, Star Service host 200
It can be by the corresponding supply voltage for loading 3.3V, 5V and 12V size to Star Service subsystem 300 of multiple power supply terminals 130, to protect
Demonstrate,prove the normal operation of the various businesses of Star Service subsystem 300.
As load supply voltage optional way, Star Service host 200 supply voltage of every kind of size can be loaded to
A corresponding power supply terminal 130.Alternatively, Star Service host 200 can also load the supply voltage of every kind of size to corresponding
At least two power supply terminals 130, in other words, the supply voltage of same size is loaded into corresponding master by Star Service host 200 respectively
Power supply terminal 130 and available electric terminal 130.For example, including 3 power supply terminals 130, Star Service master in a-quadrant in conjunction with Fig. 6 and Fig. 7
The supply voltage of 12V is loaded into power supply terminal A1, power supply terminal A2 and power supply terminal A3 in a-quadrant by machine 200；B area
Inside include 3 power supply terminals 130, power supply terminal B1 that the supply voltage of 5V is loaded into B area by Star Service host 200, supplies
Electric terminal B2 and power supply terminal B3；It include 2 power supply terminals 130 in the region C, Star Service host 200 is equal by the supply voltage of 3.3V
The power supply terminal C1 and power supply terminal C2 being loaded into the region C.
Certainly, aforesaid way is also not necessarily limited to the load of supply voltage, for example, Star Service host 200 can also be big by every kind
Small supply voltage is loaded at least one corresponding power supply terminal 130, i.e. a part of power supply terminal 130 without spare terminal, and
Another part power supply terminal 130 includes main power supply terminal and available electric terminal.
Illustratively, data terminal 140 may be multiple, and referring to Fig. 7, multiple data terminals 140 are segmented into main number
According to terminal D and standby data terminal E.After the terminal and Star Service host 200 integrated on connector 100 connects firmly, Star Service host 200 is used
It exports in by same Star Service data to master data terminal D and standby data terminal E, to pass through master data terminal D and standby data terminal
Sub- E cooperates the Star Service data to continue to output to Star Service subsystem 300；Alternatively, for passing through master data terminal D or standby data terminal
E cooperation receives Star Service subsystem 300 and exports same Star Service data.
In conjunction with Fig. 7, when there is the damage of any one terminal in master data terminal D1, D2, D3 and D4, remaining standby data terminal
E1, E2, E3 and E4 still be able to it is independent Star Service data are continued to output to Star Service subsystem 300, alternatively, passing through remaining standby number
The Star Service data that independent reception Star Service subsystem 300 continues to output still are able to according to terminal E1, E2, E3 and E4, guarantee Star Service master
It can also continue normal data interaction between machine 200 and Star Service subsystem 300, improve the stability of satellite operation.
In addition, being additionally provided with ground terminal 150 on the end face 1111 in other way of example.Wherein, ground terminal
The setting principle of son 150 can refer to power supply terminal 130 above-mentioned or data terminal 140, just be not repeated again.For example, knot
Fig. 6 and Fig. 7 is closed, includes 5 ground terminals 150 in the region H, Star Service host 200 passes through the ground terminal H1 in the region H, ground connection
Terminal H2, ground terminal H3, ground terminal H4 and ground terminal H5 are grounded.
In one embodiment, connector 100 supports network protocol, the Star Service host 200 and the Star Service subsystem
300 transmit data by network protocol.
Due to the difference of business on star, need to transmit a plurality of types of stars between Star Service host 200 and Star Service subsystem 300
Business data, such as discrete telemetry and filestream data packet.In traditional satellite system, different types of data need
It is transmitted by the bus of different agreement, such as discrete telemetry needs generally to transmit by IIC or CAN bus, file
Stream packets are needed through SPI or LVDS bus transfer, and are built every bus and required several cables.In the present embodiment
In, data, different types of a variety of Star Service data are transmitted using network protocol between Star Service host 200 and Star Service subsystem 300
It can be distinguish, rather than be distinguished by different buses, therefore inhomogeneity by different types of data packet
The data packet of type can be transmitted by same group of cable D1, D2, D3 and D4 in connector.
Referring to Fig. 8, connector 100 and Star Service host 200 can be integral type knot in some possible implementations
Structure, i.e. connector 100 can be a part of Star Service host 200.In other words, in the third possible implementation, connector
100 are not independent physical equipment, but rely on the presence of Star Service host 200.In this case, have on Star Service host 200
Piece connecting line 120 (a part that connecting line 120 is Star Service host 200), on one end of connecting line 120 and Star Service host 200
Corresponding terminal is integrally formed structures, and the other end of connecting line 120 is equipped with connector 110, and connector 110 then can be with star
Business subsystem 300 connects firmly.
It is understood that the structure and working principle of connector 100 described in this implementation can also be refering to aforementioned
The structure and working principle of connector 100 described in implementation, are just not repeated herein.
Referring to Fig. 9, connector 100 and Star Service subsystem 300 can be integral type knot in some possible implementations
Structure, i.e. connector 100 can be a part of Star Service subsystem 300.In other words, in the 4th kind of possible implementation, connection
Device 100 is also to rely on the presence of Star Service subsystem 300.In this case, there is a connecting line 120 in Star Service subsystem 300
(a part that connecting line 120 is Star Service subsystem 300), one end and the corresponding terminal in Star Service subsystem 300 of connecting line 120 are
The other end of integrally formed structure, connecting line 120 is equipped with connector 110, and connector 110 then can be with Star Service host 200
It connects firmly.
It is understood that the structure and working principle of connector 100 described in this implementation can also be refering to aforementioned
The structure and working principle of connector 100 described in implementation, are just not repeated herein.
Further, described referring to Fig. 1, after Star Service host 200 connect by connector 100 with Star Service subsystem 300
Star Service host 200 constitutes local area network with the Star Service subsystem 300 together, and Star Service host 200 can also control each Star Service point
The operation of system 300, to realize Star Service subsystem 300 and Star Service host 200, Star Service subsystem 300 and Star Service subsystem 300 it
Between interaction.
Specifically, Star Service subsystem 300 is in the heavy data processing task of no progress, for power saving, Star Service point is
System 300 can control itself in a dormant state, or controls the Star Service subsystem 300 by Star Service host 200 and be in suspend mode shape
State.
In application scenes, it is assumed that a Star Service subsystem 300 in Star Service subsystem 300 is in suspend mode shape
State, if other Star Service subsystems 300 at this time in Star Service subsystem 300 are initiated to access to the Star Service subsystem 300 of the suspend mode,
Star Service host 200 can receive the subsystem for the Star Service subsystem 300 for the suspend mode that other Star Service subsystems 300 are sent
Access request.By parsing subsystem access request, Star Service host 200 determines the access carried in subsystem access request
Location is the address (the Star Service subsystem 300 that expression needs to access the suspend mode) of the Star Service subsystem 300 of the suspend mode.Therefore Star Service host
200 can send wake up instruction to the Star Service subsystem 300 of the suspend mode by connector 100, to be somebody's turn to do by wake up instruction control
The Star Service subsystem 300 of suspend mode is adjusted to working condition from dormant state.After the Star Service subsystem 300 of suspend mode is waken up, star
Subsystem access request is transmitted to the Star Service subsystem 300 by connector 100 again by business host 200.
Further, it is the safety for guaranteeing access, each Star Service subsystem 300 is preset in Star Service host 200 to it
The access authority of its Star Service subsystem.Determine that the access address carried in Star Service subsystem access request is in Star Service host 200
Behind the address of the Star Service subsystem 300 of suspend mode, Star Service host 200 can first judge that it is initiated the Star Service subsystem of request and stops to this
Whether the Star Service subsystem 300 of dormancy has access authority.If it is determined that Star Service host 200 is without waking up suspend mode without access authority
Star Service subsystem 300, and terminate the access of the Star Service subsystem for initiating request.If it is determined that have access authority, Star Service host
200 just wake up the Star Service subsystem 300 of the suspend mode by connector 100, and are to the Star Service of the suspend mode point by connector 100
300 forwarding subsystem access request of system.
Pass through Star Service host 200 and Star Service point below by star's business subsystem 300 for a specific application scenarios
The interaction of system 300.
Assuming that: a Star Service subsystem 300 is camera load system on star, another Star Service subsystem 300 is to deposit on star
Storage system.After camera load system completes shooting task over the ground on star, camera load system is needed the photograph of shooting on star
Piece is transferred to storage system on star and stores, therefore camera load system by Star Service host 200, send out by the storage system on star on star
Send access.After Star Service host 200 receives the subsystem access request that camera load system is sent on star, determine mutually airborne on star
G system has the access authority to storage system on star, and determines that storage system is that off-mode (is in suspend mode shape on star
State), Star Service host 200 can control storage system on star and be switched on.After storage system booting is run successfully on determining star, Star Service
The address of camera load system and number of pictures on the star carried in subsystem access request can be sent on star by host 200
Storage system.In this way, storage system can be according on the address of camera load system on star and number of pictures access star on star
(storage system is also by Star Service host to the access of camera load system on star to the file directory of camera load system on star
200 initiate), with from star camera load system obtain the photo of the shooting.Storage system stores the photo of shooting on star
After the completion, storage system continues to be restored to off-mode on star.
In other application scenarios, if ground telemetering station or other satellites need to acquire the whole starlike state of this satellite
When, ground telemetering station or other satellites can (such as the communications point of Star Service subsystem 300 into this satellite with communication capacity
System) whole starlike state acquisition instructions are sent, which passes through connector 100 for the whole starlike state acquisition instructions again
It is transmitted to Star Service host 200.
It, can be according to the whole starlike state acquisition instructions, timesharing after Star Service host 200 receives the whole starlike state acquisition instructions
Wake up all Star Service subsystems 300 in a dormant state on satellite.Then, Star Service host 200 can pass through connector 100
The operation data and Star Service host 200 that obtain each Star Service subsystem 300 also obtain the operation data of itself.Star Service host
200 can be packaged the operation data of the operation data of each Star Service subsystem 300 and Star Service host 200 itself together, and will
Data after packing are sent to the Star Service subsystem 300 with ground telemetering station or other satellite communications, the star by connector 100
Data after packing are transmitted to destination again by business subsystem 300, and destination is, for example, ground telemetering station or other satellites.
Figure 10-Figure 12 is please referred to, based on the same inventive concept, the embodiment of the present application provides a kind of Star Service data interaction side
Method, applied to the Star Service host in satellite system, the Star Service data interactive method includes:
Step S100: other Star Service subsystems in the Star Service subsystem are being received into the Star Service subsystem
When the subsystem access request that one Star Service subsystem is sent, one Star Service subsystem is controlled from dormant state and is adjusted to work
Make state.
Step S200: the subsystem access request is sent to one Star Service subsystem.
Optionally, Star Service data interactive method can also include:
Step S101: it receives the subsystem access that other Star Service subsystems are sent to one Star Service subsystem and asks
It asks.
Step S201: according to the subsystem access request, judge whether other Star Service subsystems have described in access
The permission of one Star Service subsystem.
Step S301: if so, the subsystem access request is forwarded to one Star Service subsystem.
Optionally, Star Service data interactive method can also include:
Step S110: whole starlike state acquisition instructions are received.
Step S210: according to the whole starlike state acquisition instructions, timesharing obtains the operation data of the Star Service host itself,
And the operation data of the Star Service subsystem.
Step S310: by it is described itself operation data and the Star Service subsystem operation data be packaged, and will be packaged
Data afterwards are sent to the Star Service subsystem for communication, so that the Star Service subsystem for communication again will be after the packing
Data be transmitted to destination.
It should be noted that for convenience and simplicity of description, the specific implementation procedure of foregoing description method, before can referring to
The corresponding process in the embodiment of system, device and unit is stated, details are not described herein.
The some embodiments of the application additionally provide a kind of storage medium of non-volatile program code that computer is executable,
The storage medium can be general storage medium, such as mobile disk, hard disk.It is stored with program code on the storage medium,
The program code executes the step of Star Service data interactive method of any of the above-described embodiment when being run by computer.
The program code product of Star Service data interactive method provided by the embodiment of the present application, including store program code
Computer readable storage medium, the instruction that program code includes can be used for executing the method in previous methods embodiment, specifically
It realizes and can be found in embodiment of the method, details are not described herein.
In conclusion the embodiment of the present application provide a kind of connector, satellite system, Star Service subsystem, Star Service host and
Method.It can be subtracted by connector Star Service host and Star Service subsystem since the protective case that connector provides wraps up multi-cable
When few Star Service host is connected with Star Service subsystem, it is exposed to the quantity of outer cable, reduces the probability of cable aging breakage, raising is defended
The stability of star work.
In embodiment provided herein, it should be understood that disclosed device and method, it can be by others side
Formula is realized.The apparatus embodiments described above are merely exemplary, for example, the division of the unit, only one kind are patrolled
Function division is collected, there may be another division manner in actual implementation, in another example, multiple units or components can combine or can
To be integrated into another system, or some features can be ignored or not executed.Another point, shown or discussed is mutual
Coupling, direct-coupling or communication connection can be INDIRECT COUPLING or communication link by some communication interfaces, device or unit
It connects, can be electrical property, mechanical or other forms.
In addition, unit may or may not be physically separated as illustrated by the separation member, as unit
The component of display may or may not be physical unit, it can and it is in one place, or may be distributed over more
In a network unit.Some or all of unit therein can be selected to realize this embodiment scheme according to the actual needs
Purpose.
Furthermore each functional module in each embodiment of the application can integrate one independent portion of formation together
Point, it is also possible to modules individualism, an independent part can also be integrated to form with two or more modules.
Herein, relational terms such as first and second and the like be used merely to by an entity or operation with it is another
One entity or operation distinguish, and without necessarily requiring or implying between these entities or operation, there are any this reality
Relationship or sequence.
The above description is only an example of the present application, the protection scope being not intended to limit this application, for ability
For the technical staff in domain, various changes and changes are possible in this application.Within the spirit and principles of this application, made
Any modification, equivalent substitution, improvement and etc. should be included within the scope of protection of this application.
Claims (10)
1. a kind of connector, which is characterized in that be used for satellite system, the satellite system includes Star Service host and Star Service point is
System, the both ends of the connector are separately connected the Star Service host and the Star Service subsystem, and the connector includes connecting line
The connector being connected with the connecting line, the connecting line include multi-cable, and the multi-cable includes being used for transmission number
According to cable and be used for transmission the cable of electric energy, the connector is made of hard material, is integrated with confession on the connector
The cable that electric energy is used for transmission in electric terminal and data terminal, the power supply terminal and the multi-cable is connected, the data
Terminal with the cable for being used for transmission data in the multi-cable for being connected.
2. connector according to claim 1, which is characterized in that the power supply terminal includes main power supply terminal and available electricity
Terminal, the main power supply terminal and the available electric terminal receive the supply voltage of same size from the Star Service host；It is described
Data terminal includes master data terminal and standby data terminal, and the master data terminal and the standby data terminal are from the Star Service master
Machine receives identical Star Service data.
3. connector according to claim 1, which is characterized in that the connector supports network protocol.
4. connector according to claim 1, which is characterized in that the connector further includes protective case, the protective case
For wrapping up the multi-cable.
5. connector according to claim 4, which is characterized in that the protective case is made of rigid material.
6. a kind of satellite system characterized by comprising appoint in Star Service host, Star Service subsystem and such as claim 1 to 5
Connector described in one, the Star Service host pass through the company for controlling the Star Service subsystem, the Star Service subsystem
Device is connect to be connected with the Star Service host to receive the data of the electric energy of Star Service host offer and transmission.
7. satellite system according to claim 6, which is characterized in that between the Star Service subsystem and the Star Service host
Data are transmitted using network protocol, a Star Service subsystem in the Star Service subsystem passes through the Star Service host and other
Star Service subsystem exchanges data.
8. a kind of Star Service subsystem characterized by comprising
There is a connecting line, the connecting line includes multi-cable, wherein the multi-cable packet in the Star Service subsystem
The cable for being used for transmission data and the cable for being used for transmission electric energy are included, the connecting line is connected with connector, the connector
On be integrated with power supply terminal and data terminal, the cable that electric energy is used for transmission in the power supply terminal and the connecting line is connected,
For being connected with the cable for being used for transmission data in the connecting line, the connector is used for and Star Service host the data terminal
It connects firmly.
9. a kind of Star Service host characterized by comprising
There is a connecting line, the connecting line includes multi-cable, wherein the multi-cable includes on the Star Service host
It is used for transmission the cable of data and is used for transmission the cable of electric energy, the connecting line is connected with connector, on the connector
It is integrated with power supply terminal and data terminal, the cable that electric energy is used for transmission in the power supply terminal and the connecting line is connected, institute
Data terminal is stated for being connected with the cable for being used for transmission data in the connecting line, the connector is used for and Star Service subsystem
It connects firmly.
10. a kind of Star Service data interactive method of satellite system, which is characterized in that the satellite system includes Star Service host, star
Be engaged in subsystem and connector according to any one of claims 1 to 5, the Star Service subsystem by the connector with
The Star Service host is connected, and the method is applied to Star Service host, which comprises
It is receiving a Star Service of the other Star Service subsystems in the Star Service subsystem into the Star Service subsystem point
When the subsystem access request sent of uniting, judge whether other subsystems have the power for accessing one Star Service subsystem
Limit；
It is adjusted to working condition from dormant state if so, then controlling one Star Service subsystem, then the subsystem is accessed
Request is sent to one Star Service subsystem.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910820950.1A CN110518420B (en) | 2019-08-30 | 2019-08-30 | Connector, satellite system, satellite affair subsystem, satellite affair host and method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910820950.1A CN110518420B (en) | 2019-08-30 | 2019-08-30 | Connector, satellite system, satellite affair subsystem, satellite affair host and method |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN110518420A true CN110518420A (en) | 2019-11-29 |
| CN110518420B CN110518420B (en) | 2021-02-02 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910820950.1A Active CN110518420B (en) | 2019-08-30 | 2019-08-30 | Connector, satellite system, satellite affair subsystem, satellite affair host and method |
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| CN (1) | CN110518420B (en) |
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| DE202005020115U1 (en) * | 2005-12-23 | 2006-02-23 | Zweibrüder Optoelectronics GmbH | Extension cable with plug at one end and socket strip at the other, includes on-off switch which is remote from socket strip |
| CN205264985U (en) * | 2015-12-21 | 2016-05-25 | 中新科技集团股份有限公司 | Full signal transmission line |
| CN108321606A (en) * | 2018-02-02 | 2018-07-24 | 深圳爱影科技有限公司 | A kind of electric connector and the shared electronic equipment using the electric connector |
| CN109508160A (en) * | 2017-09-14 | 2019-03-22 | 钟志刚 | Display integrates connecting line |
| CN208923527U (en) * | 2018-11-29 | 2019-05-31 | 东莞市宇亮电子有限公司 | A kind of wire pair board connector |
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| JPH11154570A (en) * | 1997-11-21 | 1999-06-08 | Matsushita Electric Works Ltd | Plural-kind wiring mixed plug, electric outlet and tap using this |
| DE202005020115U1 (en) * | 2005-12-23 | 2006-02-23 | Zweibrüder Optoelectronics GmbH | Extension cable with plug at one end and socket strip at the other, includes on-off switch which is remote from socket strip |
| CN205264985U (en) * | 2015-12-21 | 2016-05-25 | 中新科技集团股份有限公司 | Full signal transmission line |
| CN109508160A (en) * | 2017-09-14 | 2019-03-22 | 钟志刚 | Display integrates connecting line |
| CN108321606A (en) * | 2018-02-02 | 2018-07-24 | 深圳爱影科技有限公司 | A kind of electric connector and the shared electronic equipment using the electric connector |
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Also Published As
| Publication number | Publication date |
|---|---|
| CN110518420B (en) | 2021-02-02 |
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