CN108363348A - Space environment simulation facility control device and system - Google Patents
Space environment simulation facility control device and system Download PDFInfo
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- CN108363348A CN108363348A CN201810133425.8A CN201810133425A CN108363348A CN 108363348 A CN108363348 A CN 108363348A CN 201810133425 A CN201810133425 A CN 201810133425A CN 108363348 A CN108363348 A CN 108363348A
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- 238000004088 simulation Methods 0.000 title claims abstract description 82
- 238000012544 monitoring process Methods 0.000 claims abstract description 39
- 238000000034 method Methods 0.000 claims description 33
- 230000008569 process Effects 0.000 claims description 24
- 238000012545 processing Methods 0.000 claims description 18
- 238000007726 management method Methods 0.000 claims description 13
- 238000013515 script Methods 0.000 claims description 9
- 238000004891 communication Methods 0.000 claims description 8
- 238000004458 analytical method Methods 0.000 claims description 4
- 238000013500 data storage Methods 0.000 claims description 3
- 230000000737 periodic effect Effects 0.000 claims description 3
- 238000005516 engineering process Methods 0.000 abstract description 12
- 230000004807 localization Effects 0.000 abstract description 9
- 230000006870 function Effects 0.000 description 16
- 238000010586 diagram Methods 0.000 description 10
- 230000001276 controlling effect Effects 0.000 description 9
- 230000003993 interaction Effects 0.000 description 7
- 230000008901 benefit Effects 0.000 description 5
- 238000012360 testing method Methods 0.000 description 5
- 230000002452 interceptive effect Effects 0.000 description 4
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- 210000004556 brain Anatomy 0.000 description 3
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- 238000010168 coupling process Methods 0.000 description 3
- 238000005859 coupling reaction Methods 0.000 description 3
- 230000005611 electricity Effects 0.000 description 3
- 238000003780 insertion Methods 0.000 description 3
- 230000037431 insertion Effects 0.000 description 3
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- 238000006243 chemical reaction Methods 0.000 description 2
- 230000008878 coupling Effects 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 230000007246 mechanism Effects 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 238000004886 process control Methods 0.000 description 2
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- 238000003860 storage Methods 0.000 description 2
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- 230000004308 accommodation Effects 0.000 description 1
- 230000003044 adaptive effect Effects 0.000 description 1
- 238000004422 calculation algorithm Methods 0.000 description 1
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- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B19/00—Programme-control systems
- G05B19/02—Programme-control systems electric
- G05B19/04—Programme control other than numerical control, i.e. in sequence controllers or logic controllers
- G05B19/05—Programmable logic controllers, e.g. simulating logic interconnections of signals according to ladder diagrams or function charts
- G05B19/054—Input/output
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- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B2219/00—Program-control systems
- G05B2219/10—Plc systems
- G05B2219/11—Plc I-O input output
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Abstract
A kind of Space environment simulation facility control device of present invention offer and system, are related to equipment control technology field, wherein device includes built-in industrial computer, RTU modules, and embedded ring moulds TT＆C software system is equipped in built-in industrial computer；RTU modules are connect with small space environment simulation facility；RTU modules are connect by RS485/232 buses with built-in industrial computer；RTU modules receive the operational order transmitted by embedded ring moulds TT＆C software system, and according to operational order to embedded ring moulds TT＆C software system feedback monitoring data, to realize the TT＆C task of small space environment simulation facility.The present invention is by the way of RTU+ embedded systems+real time operating system+special-purpose software, in a manner of local manipulation, can enhance compact, localization and the convenience of operation of equipment, advantageously reduces the overall cost of environment simulation facility, improves system reliability.
Description
Technical field
The present invention relates to equipment control technology fields, more particularly, to a kind of Space environment simulation facility control device and system.
Background technology
Space environment simulation equipment is in order in environment such as the cold black, high vacuum of ground simulation space, Orbital heat flux, gas ions
And a kind of multifunctional integrated experimental equipment built is developed, it is that astronaut, spacecraft and subsystem, load etc. carry out respectively on ground
The key equipment of the simulation tests such as kind performance, reliability, service life examination.Space environment simulation equipment is by test chamber, heat sink, true
Sky pumping unit, high/low temperature flow, experimental rig platform, temperature sensing device, control unit etc. in groups at.These devices and stream
The condition monitoring of journey is completed by the software run on background computer.Generally use general Project Configuration soft in industry
Part carrys out the diversified software systems of rapid build, to solve the operation monitoring and integrated management of space environment simulation equipment.
The general Engineering configuration software run in PC machine or industry control, there is response sluggishness, operational efficiency is low, expends system
System resource, many unfavorable factors such as data-handling capacity is weak, remote functionality is weak, safety is not strong, intellectual property is difficult to protect.
In particular for small space environment simulation facility, due to small, measurement, control object are relatively fewer, and control flow is relatively easy,
It is unfavorable for the excellent of several aspects such as cost, performance, globality, handling by the way of the upper industrial personal computer+configuration softwares of PLC+
Change.
Invention content
In view of this, the purpose of the present invention is to provide a kind of Space environment simulation facility control device and systems, using insertion
Formula systems technology combines human-computer interaction interface, key control unit and environment simulation facility together, constructs a kind of localization touch screen
Man-machine interactive operation mode, more meet user makes custom.Using RTU+ embedded systems+real time operating system+special-purpose software
Mode can be well solved PC machine platform and general Engineering configuration software in space environment observing and controlling in a manner of local manipulation
The problem of aspect, enhances compact, localization and the convenience of operation of equipment, advantageously reduce environment simulation facility integral into
This, improves system reliability.
In a first aspect, an embodiment of the present invention provides a kind of Space environment simulation facility control devices, including：Built-in industrial electricity
Brain, RTU modules；
Embedded ring moulds TT＆C software system is installed in built-in industrial computer；
RTU modules are connect with small space environment simulation facility；
RTU modules are connect by RS485/232 buses with built-in industrial computer；
RTU modules receive the operational order transmitted by embedded ring moulds TT＆C software system, and according to operational order to embedding
Enter formula ring moulds TT＆C software system feedback monitoring data, to realize the TT＆C task of small space environment simulation facility.
With reference to first aspect, an embodiment of the present invention provides the first possible embodiments of first aspect, wherein also
Including：Message input device；
Message input device includes：Touching display screen and/or keyboard and mouse；
Message input device is connect with built-in industrial computer；
It is defeated to obtain user by message input device for embedded ring moulds TT＆C software system in built-in industrial computer
The operational order entered, and operational order is sent to RTU modules.
With reference to first aspect, an embodiment of the present invention provides second of possible embodiments of first aspect, wherein also
Including：Cooperate with PC machine；
Collaboration PC machine is connect with built-in industrial computer；
It cooperates with PC machine by ICP/IP protocol, monitoring data is obtained from embedded ring moulds TT＆C software system；
And/or
It cooperates with PC machine by ICP/IP protocol, control instruction is sent to embedded ring moulds TT＆C software system, so that embedded
Formula ring moulds TT＆C software system controls small-sized environment simulation facility and executes corresponding operating according to control instruction.
With reference to first aspect, an embodiment of the present invention provides the third possible embodiments of first aspect, wherein embedding
Entering formula ring moulds TT＆C software system includes：Data resolution module, data processing module and instruction sending module；
Data resolution module is connect with RTU modules, instruction sending module, data processing module respectively；
Data resolution module receives the RTU data transmitted by RTU modules, and is parsed to RTU data, after parsing
Data judged, if parsing after data be feedback signal ACK, handled by instruction sending module, if parsing
Data afterwards are monitoring data, then monitoring data are analyzed and handled by data processing module.
With reference to first aspect, an embodiment of the present invention provides the 4th kind of possible embodiments of first aspect, wherein point
Analysis and the mode handled include：Refresh Data, data storage, key operation and node data write-in daily record, to wrong data into
At least one of row alarm.
With reference to first aspect, an embodiment of the present invention provides the 5th kind of possible embodiments of first aspect, wherein embedding
Entering formula ring moulds TT＆C software system further includes：Software configuration module；
The content that software configuration module is configured includes：In interface information file, device parameter file, process scripts file
It is at least one；
Structure, scale and technological process of the software configuration module for customized small space environment simulation facility again.
With reference to first aspect, an embodiment of the present invention provides the 6th kind of possible embodiments of first aspect, wherein embedding
The operating mode for entering formula ring moulds TT＆C software system includes：Debugging module, operating mode.
With reference to first aspect, an embodiment of the present invention provides the 7th kind of possible embodiments of first aspect, wherein embedding
The function module for entering formula TT＆C system includes：Procedure module, monitoring modular, journal module, debugging module, setup module, user
At least one of management module, help module；
Procedure module includes：In automatic overall process unit, vacuum process unit, pyroprocess unit, chilling process unit
At least one of；
Monitoring modular includes：At least one of flow monitoring unit, Condition Monitoring Unit, temperature monitoring unit；
Journal module includes：Unit is checked in daily record；
Debugging module includes：Port numbering is adjusted with weights setting unit, port diagnostic threshold setting unit, pid parameter
At least one of with download unit；
Setup module includes：Communication port setting unit, data periodic unit, the customized unit of software interface, hardware adapt to
At least one of property setting unit, process scripts dispensing unit；
User management module includes：At least one of account and Password Management unit, rights management unit.
With reference to first aspect, an embodiment of the present invention provides the 8th kind of possible embodiments of first aspect, wherein also
Including：Warning device；
Warning device is connect with built-in industrial computer；
Warning device receives the alarm command transmitted by embedded ring moulds TT＆C software system, and is carried out according to alarm command
Alarm.
Second aspect, the embodiment of the present invention provide a kind of Space environment simulation facility control system, which includes：Intelligent terminal
And Space environment simulation facility control device as described in relation to the first aspect；
Intelligent terminal is connect with the built-in industrial compunlcation in Space environment simulation facility control device；
Intelligent terminal receives the monitoring data transmitted by built-in industrial computer, so that staff refers to.
The embodiment of the present invention brings following advantageous effect：
In Space environment simulation facility control device provided in an embodiment of the present invention, including built-in industrial computer, RTU moulds
Block, wherein embedded ring moulds TT＆C software system is equipped in built-in industrial computer；RTU modules are set with small space ring moulds
Standby connection；RTU modules are connect by RS485/232 buses with built-in industrial computer；RTU modules receive embedded ring moulds observing and controlling
Operational order transmitted by software systems, and according to operational order to embedded ring moulds TT＆C software system feedback monitoring data,
To realize the TT＆C task of small space environment simulation facility.Space environment simulation facility control device provided by the present invention, using insertion
Formula systems technology combines human-computer interaction interface, key control unit and environment simulation facility together, constructs a kind of localization touch screen
Man-machine interactive operation mode, more meet user makes custom.Using RTU+ embedded systems+real time operating system+special-purpose software
Mode can be well solved PC machine platform and general Engineering configuration software in space environment observing and controlling in a manner of local manipulation
The problem of aspect, enhances compact, localization and the convenience of operation of equipment, advantageously reduce environment simulation facility integral into
This, improves system reliability.
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 purpose of the present invention and other advantages are in specification, claims
And specifically noted structure is realized and is obtained in attached drawing.
To enable the above objects, features and advantages of the present invention to be clearer and more comprehensible, preferred embodiment cited below particularly, and coordinate
Appended attached drawing, is described in detail below.
Description of the drawings
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 are briefly described, it should be apparent that, in being 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, other drawings may also be obtained based on these drawings.
Fig. 1 is a kind of schematic diagram for Space environment simulation facility control device that the embodiment of the present invention one provides；
Fig. 2 is the schematic diagram for another Space environment simulation facility control device that the embodiment of the present invention one provides；
Fig. 3 is embedded ring moulds TT＆C software in a kind of Space environment simulation facility control device that the embodiment of the present invention one provides
System top level data flow diagram；
Fig. 4 is the data from RTU modules in a kind of Space environment simulation facility control device that the embodiment of the present invention one provides
Process chart；
Fig. 5 is equipment control and parameter modification in a kind of Space environment simulation facility control device that the embodiment of the present invention one provides
Data flow diagram；
Fig. 6 is embedded ring moulds TT＆C software in a kind of Space environment simulation facility control device that the embodiment of the present invention one provides
The customized flow chart of adaptability；
Fig. 7 is embedded ring moulds TT＆C software in a kind of Space environment simulation facility control device that the embodiment of the present invention one provides
Functional block diagram；
Fig. 8 is a kind of schematic diagram of Space environment simulation facility control system provided by Embodiment 2 of the present invention.
Specific implementation mode
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
Lower obtained every other embodiment, shall fall within the protection scope of the present invention.
Existing small space environment simulation facility, due to small, measurement, control object are relatively fewer, and control flow is opposite
Simply, it is unfavorable for several aspects such as cost, performance, globality, handling by the way of the upper industrial personal computer+configuration softwares of PLC+
Optimization.
Based on this, a kind of Space environment simulation facility control device of offer of the embodiment of the present invention and system, using embedded system
Technology combines human-computer interaction interface, key control unit and environment simulation facility together, constructs a kind of man-machine friendship of localization touch screen
Interoperability mode, more meet user makes custom.By the way of RTU+ embedded systems+real time operating system+special-purpose software,
In a manner of local manipulation, PC machine platform and general Engineering configuration software asking in terms of space environment observing and controlling can be well solved
Topic, enhances compact, localization and the convenience of operation of equipment, advantageously reduces the overall cost of environment simulation facility, improves system
System reliability.
For ease of understanding the present embodiment, first to a kind of Space environment simulation facility control disclosed in the embodiment of the present invention
Device processed describes in detail.
Embodiment one：
An embodiment of the present invention provides a kind of Space environment simulation facility control devices, shown referring to Fig. 1 and Fig. 2, the device packet
It includes：Built-in industrial computer 11, RTU modules 12.Wherein, embedded ring moulds TT＆C software is installed in built-in industrial computer 11
System 111；RTU modules 12 are connect with small space environment simulation facility 13；RTU modules 12 by RS485/232 buses with it is embedded
Industrial computer 11 connects；RTU modules 12 receive the operational order transmitted by embedded ring moulds TT＆C software system 111, and according to
Operational order is to embedded 111 feedback monitoring data of ring moulds TT＆C software system, to realize the survey of small space environment simulation facility 13
Control task.
RTU modules 12 are the abbreviations of REMOTE TERMINAL UNIT, Chinese be remote measurement and control terminal for monitoring,
The application of control and data acquisition, has telemetering, remote signalling, remote regulating, distant control function.In the present embodiment, RTU modules 12 include digital-to-analogue
Conversion module, data receiver sending module, relay module and analog-to-digital conversion module etc. are, it can be achieved that soft with embedded ring moulds observing and controlling
The instruction and data of part system 111 interacts.
The space environment control device that the present embodiment is provided is mainly using built-in industrial computer 11, RS485/232
Bus, RTU modules are realized with lower cost, higher flexibility, and more open software and hardware architecture to small space ring
The electric control function of mould equipment 13.
For the higher temperature automatic control flow of requirement of real-time, in another embodiment, using lower layer's PID tune
The system architecture that section device is combined with upper layer FUZZY ALGORITHMS FOR CONTROL, temperature control system include：Heater, Fan Regulation valve
Deng, wherein the power control of heater is completed by bottom PID regulator, and wind turbine and control valve pass through built-in industrial electricity
FUZZY ALGORITHMS FOR CONTROL program in brain 11 is completed.Fuzzy algorithmic approach program is used for coarse adjustment, and PID regulator is used for fine tuning.When coarse adjustment
Bypass PID regulator.
In order to realize good man-machine interface interaction, further include in the device：Message input device.Message input device packet
It includes：Touching display screen and/or keyboard and mouse；Message input device is connect with built-in industrial computer 11；Built-in industrial electricity
Embedded ring moulds TT＆C software system 111 in brain 11 obtains operational order input by user by message input device, and
Operational order is sent to RTU modules 12.Further by RTU modules 12 and embedded ring moulds TT＆C software system 111, realize
Control to small space environment simulation facility 13.
In addition, further including in above-mentioned apparatus：Cooperate with PC machine.Collaboration PC machine is connect with built-in industrial computer 11；Cooperate with PC
Machine obtains monitoring data by ICP/IP protocol, from embedded ring moulds TT＆C software system 111；And/or collaboration PC machine passes through
ICP/IP protocol sends control instruction, so that embedded ring moulds TT＆C software system to embedded ring moulds TT＆C software system 111
111, according to control instruction, control small-sized environment simulation facility and execute corresponding operating.
It is analyzed by the requirement of hardware and software function to environment simulation facility, embedded ring moulds TT＆C software system 111 is pushed up
Layer data flow graph is as shown in Figure 3.Three entities with the software interactive are user respectively, RTU modules 12, cooperate with PC machine.User
It is inputted and is instructed to software systems by touch screen or key mouse, information is obtained from screen, file.RTU modules 12 pass through RS485/232
Bus obtains operational order from embedded ring moulds TT＆C software system 111, and to its feedback states, data and answer signal.Association
With upper PC machine by obtaining state from embedded ring moulds TT＆C software system 111 with ICP/IP protocol and data can monitor simultaneously
Various data modes also can send control instruction, indirect control small space ring moulds to embedded ring moulds TT＆C software system 111
The various actions of equipment 13.
Embedded ring moulds TT＆C software system 111 includes：Data resolution module, data processing module and instruction send mould
Block；Data resolution module is connect with RTU modules 12, instruction sending module, data processing module respectively；Data resolution module receives
RTU data transmitted by RTU modules 12, and RTU data are parsed, judged according to the data after parsing, if parsing
Data afterwards are feedback signal ACK, then are handled by instruction sending module, if the data after parsing are monitoring data,
Monitoring data are analyzed and handled by data processing module.
The mode of above-mentioned analysis and processing includes：In Refresh Data, data storage, data write-in daily record, data alarm extremely
One item missing.
Flow chart of data processing from RTU modules 12 is as shown in figure 4, first carry out the RTU data transmitted by RTU modules 12
Parsing, then judges the data after parsing, if the state of equipment and measurement data content then transfer to data processing mould
Processing is further processed in block, if being destined to the response feedback signal ACK of equipment, transfers to send instruction module place to go
Reason.If send instruction module does not receive ack signal before the deadline, need to command retransmission just now.At data
The processing link of reason module mainly completes 4 tasks：
(1) Refresh Data, such as：Refresh the data and curve on screen；
(2) data store, such as：Necessary data are stored in database；
(3) daily record is written in data, such as：Daily record is written into key operation and node data；
(4) data are alarmed, such as：Alert process is carried out to error condition and the data that transfinite.
Embedded ring moulds TT＆C software system 111 further includes as a preferred implementation manner,：Software configuration module.It is soft
The content that part configuration module is configured includes：At least one of interface information file, device parameter file, process scripts file；
Structure, scale and technological process of the software configuration module for customized small space environment simulation facility 13 again.
Specifically, as shown in figure 5, operational order frame, device address and the initiation parameter of different content, automated procedure
It controls the data such as script to preserve in a hard disk with file mode, be called by corresponding data processing module.
In the present embodiment, software configuration function may be implemented by software configuration module, using software configuration that can be customized
Mode, by manufacturer user using software configuration function to a certain degree with customized small space environment simulation facility 13 again in range
Structure, scale and technological process, expand software to the accommodation of hardware, reduce the skill set requirements of manufacturer staff,
Improve 13 production of small space environment simulation facility, debugging efficiency.
Identification information on software interface, the information such as dbase, Subscriber Unit, logo are by data file
Dynamic generation, it is only necessary to which software interface information can be changed by changing data file.Instruct content frame, device address, device parameter,
Sensor parameters, calibration coefficient, number of sensors, number of devices, timing, process flow operation script etc. are preserved by file,
Only need to change file without changing program code, you can complete the change of control mode, control content and control flow.
Its flow is as shown in Figure 6.
In the present embodiment, the operating mode of embedded ring moulds TT＆C software system 111 includes：Debugging module, Working mould
Formula both of which, to adapt to the application of manufacturer and user flexibility.Debugging mode has higher permission and operating flexibility, and
It can check initial data and intermediate result, facilitate the work such as calibration, test, the parameter testing of manufacture link.
The function module of embedded Webserver includes as a preferred implementation manner,：Procedure module, monitoring modular,
At least one of journal module, debugging module, setup module, user management module, help module.Shown in Fig. 7,
Procedure module includes：At least one of automatic overall process unit, vacuum process unit, pyroprocess unit, chilling process unit；
Monitoring modular includes：At least one of flow monitoring unit, Condition Monitoring Unit, temperature monitoring unit；Journal module includes：Day
Will checks unit；Debugging module includes：Port numbering and weights setting unit, port diagnostic threshold setting unit, pid parameter are whole
At least one of fixed and download unit；Setup module includes：Communication port setting unit, data periodic unit, software interface are ordered
At least one of unit processed, hardware adaptive mechanism setting unit, process scripts dispensing unit；User management module includes：Account and
At least one of Password Management unit, rights management unit.
In addition, further including in the space environment control device that the present embodiment is provided：Warning device.Warning device and insertion
Formula industrial computer 11 connects；Warning device receives the alarm command transmitted by embedded ring moulds TT＆C software system 111, and according to
Alarm command is alarmed.
When embedded ring moulds TT＆C software system 111 is according to monitoring data, judges corrupt data or be more than predetermined threshold value
When range, alarm command is sent to warning device, warning device is alarmed according to alarm command, such as：Audible alarm, light
Alarm, audio alert etc., do not limit herein.
In Space environment simulation facility control device provided in an embodiment of the present invention, including built-in industrial computer 11, RTU moulds
Block 12, wherein embedded ring moulds TT＆C software system 111 is equipped in built-in industrial computer 11；RTU modules 12 and small size air
Between environment simulation facility 13 connect；RTU modules 12 are connect by RS485/232 buses with built-in industrial computer 11；RTU modules 12 connect
The operational order transmitted by embedded ring moulds TT＆C software system 111 is received, and soft to embedded ring moulds observing and controlling according to operational order
111 feedback monitoring data of part system, to realize the TT＆C task of small space environment simulation facility 13.Spatial loop provided by the present invention
Mould plant control unit, using embedded system technology, it is one that human-computer interaction interface, key control unit and environment simulation facility, which are melted,
Body constructs a kind of localization touch screen man-machine interactive operation mode, and more meet user makes custom.Using RTU+ embedded systems
The mode of+real time operating system+special-purpose software can be well solved PC machine platform and general engineering in a manner of local manipulation
Configuration software enhances compact, localization and the convenience of operation of equipment, is conducive in terms of space environment observing and controlling the problem of
The overall cost of environment simulation facility is reduced, system reliability is improved.
The Space environment simulation facility control device that the embodiment of the present invention is provided is collection process control, database, a multimachine
Strongly professional, the comprehensive soft project that complexity is high of group-net communication, software and hardware one, specific features are as follows：
(1) industry control class hardware is related：For industrial control condition, monitoring, control object are that complicated, diversified hardware is set
Standby, embedded OS and embedded software program.Developer is needed both to be familiar with knowledge and the communication of Industry Control neighborhood
Specification will also be proficient in embedded hardware and software design technology.Have to the level of developer, technology, experience, background of hardware higher
It is required that.
(2) real-time and reliability requirement：Software architecture, module encapsulation, algorithm performance, testing standard, in mechanism for correcting errors
It is intended to meet the requirement of higher reliability and real-time.
(3) scale can be set：To adapt to the ring moulds object of different characteristic, software has a degree of structure, scale, boundary
Function can be arranged in face.
(4) host computer cooperates with：For human-computer interaction flexible expansion, there is upper collaboration machine to participate in the requirement of control, two sets soft
Part coordinated operation needs design collaboration working specification.
(5) specificity is strong：It is exclusively used in the narrow Space environment simulation facility in field, no Open Source Code is used for reference without similar system.
The Space environment simulation facility control device that the embodiment of the present invention is provided has the following advantages：
(1) embedded system and open, inexpensive 12 technology of RTU modules is used to realize that the observing and controlling of small space ring moulds is appointed
Business；
(2) observing and controlling flow can be changed；
(3) open process scripts；
(4) device structure, scale and process control are unrelated with code；
(5) device attribute and energy consumption statistic；
(6) host computer cooperates with.
The implementation of the software and hardware integrated system can effectively reduce the cost of small space environment simulation facility 13, improve space environment
The globality and compact of equipment promote observation and control technology level, improve the usage experience of user.Enterprise can be made to be further formed certainly
There is intellectual property, march toward product supply model from system integration pattern, guide and give side reform in industry altogether, promotes enterprise to become and go
Industry is leading.
Embodiment two：
The embodiment of the present invention provides a kind of Space environment simulation facility control system, and shown in Figure 8, which includes：Intelligence
Terminal 21 and the Space environment simulation facility control device 22 as described in embodiment one.
Wherein, intelligent terminal 21 is communicated to connect with the built-in industrial computer 221 in Space environment simulation facility control device 22；
Intelligent terminal 21 receives the monitoring data transmitted by built-in industrial computer 221, so that staff refers to.
Above-mentioned intelligent terminal 21 includes：Smart mobile phone, iPad, laptop etc..By intelligent terminal 21 with it is embedded
The remote monitoring to small space environment simulation facility is realized in data interaction between industrial computer.
Include the spatial loop as described in embodiment one in the Space environment simulation facility control system that the embodiment of the present invention is provided
Therefore mould plant control unit equally may be implemented with aforesaid space environment simulation facility control device technical characteristic having the same
Above-mentioned function.The specific work process of this system is referring to above-mentioned apparatus embodiment, and details are not described herein.
What flow chart and block diagram in attached drawing showed apparatus according to the invention embodiment and computer program product can
The architecture, function and operation that can be realized.In this regard, each box in flowchart or block diagram can represent a mould
A part for block, program segment or code, the part of the module, section or code include one or more for realizing rule
The executable instruction of fixed logic function.It should also be noted that in some implementations as replacements, the function of being marked in box
It can also occur in a different order than that indicated in the drawings.For example, two continuous boxes can essentially be substantially in parallel
It executes, they can also be executed in the opposite order sometimes, this is depended on the functions involved.It is also noted that block diagram and/
Or the combination of each box in flow chart and the box in block diagram and or flow chart, can use execute as defined in function or
The dedicated hardware based system of action is realized, or can be realized using a combination of dedicated hardware and computer instructions.
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 the description present invention and simplify description, do not indicate or imply the indicated device or element must have a particular orientation,
With specific azimuth configuration and operation, therefore it is not considered as limiting the invention.In addition, term " first ", " second ",
" third " is used for description purposes only, and is not understood to indicate or imply relative importance.
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 division of logic function, formula that in actual implementation, there may be another division manner, in another example, multiple units or component 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 by some communication interfaces, device or unit it is indirect
Coupling or communication connection can be electrical, machinery or other forms.
The unit illustrated as separating component may or may not be physically separated, aobvious as unit
The component shown may or may not be physical unit, you can be located at a place, or may be distributed over multiple
In network element.Some or all of unit therein can be selected according to the actual needs to realize the mesh of this embodiment scheme
's.
In addition, each functional unit in each embodiment of the present invention can be integrated in a processing unit, it can also
It is that each unit physically exists alone, it can also be during two or more units be integrated in one unit.
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 read/write memory 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 step 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 disc or CD etc. are various can be with
Store the medium of program code.
Finally it should be noted that：Embodiment described above, only specific implementation mode 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, it will be understood by those of ordinary skill in the art that：Any one skilled in the art
In the technical scope disclosed by the present invention, it can still modify to the technical solution recorded in 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 the protection in the present 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 Space environment simulation facility control device, which is characterized in that including：Built-in industrial computer, RTU modules；
Embedded ring moulds TT＆C software system is installed in the built-in industrial computer；
The RTU modules are connect with small space environment simulation facility；
The RTU modules are connect by RS485/232 buses with the built-in industrial computer；
The RTU modules receive the operational order transmitted by the embedded ring moulds TT＆C software system, and according to the operation
It instructs to the embedded ring moulds TT＆C software system feedback monitoring data, to realize the observing and controlling of the small space environment simulation facility
Task.
2. Space environment simulation facility control device according to claim 1, which is characterized in that further include：Message input device；
Described information input unit includes：Touching display screen and/or keyboard and mouse；
Described information input unit is connect with the built-in industrial computer；
The embedded ring moulds TT＆C software system in the built-in industrial computer is obtained by described information input unit
Operational order input by user is taken, and the operational order is sent to the RTU modules.
3. Space environment simulation facility control device according to claim 1, which is characterized in that further include：Cooperate with PC machine；
The collaboration PC machine is connect with the built-in industrial computer；
The collaboration PC machine obtains the monitoring data by ICP/IP protocol, from the embedded ring moulds TT＆C software system；
And/or
The collaboration PC machine sends control instruction by the ICP/IP protocol, to the embedded ring moulds TT＆C software system,
So that the embedded ring moulds TT＆C software system, according to the control instruction, the control small-sized environment simulation facility executes corresponding behaviour
Make.
4. Space environment simulation facility control device according to claim 1, which is characterized in that the embedded ring moulds observing and controlling is soft
Part system includes：Data resolution module, data processing module and instruction sending module；
The data resolution module is connect with the RTU modules, described instruction sending module, the data processing module respectively；
The data resolution module receives the RTU data transmitted by the RTU modules, and is parsed to the RTU data, root
Judged according to the data after parsing, if the data after the parsing are feedback signal ACK, passes through described instruction sending module
Handled, if the data after the parsing be monitoring data, by the data processing module to the monitoring data into
Row analysis and processing.
5. Space environment simulation facility control device according to claim 4, which is characterized in that the mode of the analysis and processing
Including：Refresh Data, data storage, key operation and node data write-in daily record, alarm wrong data at least one
.
6. Space environment simulation facility control device according to claim 1, which is characterized in that the embedded ring moulds observing and controlling is soft
Part system further includes：Software configuration module；
The content that the software configuration module is configured includes：In interface information file, device parameter file, process scripts file
It is at least one；
Structure, scale and technological process of the software configuration module for the customized small space environment simulation facility again.
7. Space environment simulation facility control device according to claim 1, which is characterized in that the embedded ring moulds observing and controlling is soft
The operating mode of part system includes：Debugging module, operating mode.
8. Space environment simulation facility control device according to claim 1, which is characterized in that the embedded Webserver
Function module includes：Procedure module, journal module, debugging module, setup module, user management module, helps mould at monitoring modular
At least one of block；
The procedure module includes：In automatic overall process unit, vacuum process unit, pyroprocess unit, chilling process unit
At least one of；
The monitoring modular includes：At least one of flow monitoring unit, Condition Monitoring Unit, temperature monitoring unit；
The journal module includes：Unit is checked in daily record；
The debugging module includes：Port numbering is adjusted with weights setting unit, port diagnostic threshold setting unit, pid parameter
At least one of with download unit；
The setup module includes：Communication port setting unit, data periodic unit, the customized unit of software interface, hardware adapt to
At least one of property setting unit, process scripts dispensing unit；
The user management module includes：At least one of account and Password Management unit, rights management unit.
9. Space environment simulation facility control device according to claim 1, which is characterized in that further include：Warning device；
The warning device is connect with the built-in industrial computer；
The warning device receives the alarm command transmitted by the embedded ring moulds TT＆C software system, and according to the alarm
Instruction is alarmed.
10. a kind of Space environment simulation facility control system, which is characterized in that the system comprises：Intelligent terminal and such as claim
1-9 any one of them Space environment simulation facility control devices；
The intelligent terminal is connect with the built-in industrial compunlcation in the Space environment simulation facility control device；
The intelligent terminal receives the monitoring data transmitted by the built-in industrial computer, so that staff refers to.
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| CN201810133425.8A CN108363348B (en) | 2018-02-08 | 2018-02-08 | Space environment simulation facility control device and system |
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|---|---|---|---|
| CN201810133425.8A CN108363348B (en) | 2018-02-08 | 2018-02-08 | Space environment simulation facility control device and system |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109062298A (en) * | 2018-09-19 | 2018-12-21 | 西安微电子技术研究所 | A kind of space goes out cabin environmental monitoring and control device and its control method |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2695768Y (en) * | 2004-03-22 | 2005-04-27 | 克拉玛依金牛信泰工业控制有限公司 | Oil transfering station observing and controlling system for equilization transporting |
| CN201217613Y (en) * | 2007-07-26 | 2009-04-08 | 山东富友有限公司 | Security monitoring management system for tower crane |
| CN101945088A (en) * | 2010-01-08 | 2011-01-12 | 广州中浩控制技术有限公司 | Communication processing method of wide area data collection |
| CN103728949A (en) * | 2014-01-02 | 2014-04-16 | 贵州电网公司 | Integrated control device of hydroelectric generating set |
| CN104570768A (en) * | 2014-12-31 | 2015-04-29 | 浙江大学 | Information physics semi-physical simulation system based on Rt-Lab and OPNET |
-
2018
- 2018-02-08 CN CN201810133425.8A patent/CN108363348B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2695768Y (en) * | 2004-03-22 | 2005-04-27 | 克拉玛依金牛信泰工业控制有限公司 | Oil transfering station observing and controlling system for equilization transporting |
| CN201217613Y (en) * | 2007-07-26 | 2009-04-08 | 山东富友有限公司 | Security monitoring management system for tower crane |
| CN101945088A (en) * | 2010-01-08 | 2011-01-12 | 广州中浩控制技术有限公司 | Communication processing method of wide area data collection |
| CN103728949A (en) * | 2014-01-02 | 2014-04-16 | 贵州电网公司 | Integrated control device of hydroelectric generating set |
| CN104570768A (en) * | 2014-12-31 | 2015-04-29 | 浙江大学 | Information physics semi-physical simulation system based on Rt-Lab and OPNET |
Non-Patent Citations (1)
| Title |
|---|
| 刘畅，等: "基于SCADA及以太网的大型空间环境模拟器集中控制***", 《航天器环境工程》 * |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109062298A (en) * | 2018-09-19 | 2018-12-21 | 西安微电子技术研究所 | A kind of space goes out cabin environmental monitoring and control device and its control method |
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