CN107272451A - Vacuum test control system and method - Google Patents
Vacuum test control system and method Download PDFInfo
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- CN107272451A CN107272451A CN201610218092.XA CN201610218092A CN107272451A CN 107272451 A CN107272451 A CN 107272451A CN 201610218092 A CN201610218092 A CN 201610218092A CN 107272451 A CN107272451 A CN 107272451A
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- data
- vacuum test
- power supply
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- temperature
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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
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- General Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- Automation & Control Theory (AREA)
- Testing And Monitoring For Control Systems (AREA)
Abstract
The invention discloses a kind of vacuum test control system and method, the system imports library module, programmable power supply channel including temperature data and sets up module, programmable power supply control module, data outputting module, graphical real-time monitoring module in real time.The system and method transmits vacuum test data by programmable power supply, temperature acquisition, Ethernet, being capable of output data in time, data constantly property is improved, using Graph analysis method, analysis vacuum test data validity, integrality, tightness and prediction space environment situation can be carried out.
Description
Technical field
The present invention relates to programmable power supply control, temperature data acquisition, Ethernet transmission, more particularly to a kind of vacuum examination
Test control system and method.
Background technology
China still lags behind foreign countries in terms of vacuum environment construction, and autonomous large-scale vacuum environment experiment is not set up also
System.Vacuum environment application aspect be also limited only to Satellite Product, space window etc. it is limited in terms of.With industry certainly
Dynamicization is progressively accelerated development with information-based, and the application field of vacuum environment is more and more wider, basic with Satellite Product, with reference to
Technology of Internet of things, sets up complete vacuum test monitoring system and would be particularly applicable to the not enough present situation of China's spacecraft development.
With the arrival of information age, increasing rapidly for global spacecraft demand will realize spacecraft rapid growth,
Vacuum test is essential research technique.
The content of the invention
The technical problems to be solved by the invention are to provide a kind of vacuum test control system and method, and it can be defeated in time
Go out data, improve data constantly property, using Graph analysis method, can carry out analysis vacuum test data validity,
Integrality, tightness and prediction space environment situation.
The present invention is to solve above-mentioned technical problem by following technical proposals：A kind of vacuum test control system, it is special
Levy and be, it includes：
Temperature data imports library module in real time, gathers, arranges in real time for setting up temperature data；
Programmable power supply channel sets up module, for setting up multiple power supply channels；
Programmable power supply control module, for according to self-defined experiment process, to programmable power supply control；
Temperature current voltage data output module, for setting up data output interface；
Graphical real-time monitoring module, for graphical analyze data content.
Preferably, the temperature data imports library module and gathers, imports including temperature data format protocol, in real time in real time
Database.
Preferably, the programmable power supply channel, which sets up module, includes power supply title, channel status.
Preferably, the programmable power supply control module uses following control mode：Current control, voltage control, temperature
Control, temperature control current mode.
Preferably, the temperature current voltage data output module includes temperature output interface, current output interface, electricity
Press output interface.
Preferably, the graphical real-time monitoring module is using following graphical monitor mode in real time：Temperature data figure
Change analysis, current data is graphically analyzed, voltage data is graphically analyzed.
The present invention also provides a kind of vacuum test control method, it is characterised in that it comprises the following steps：
Step one, data acquisition, is controlled vacuum test data receiver, transmission, storage and programmable power supply procedural style；
Step 2, temperature data is imported in real time；
Step 3, sets up how program control Resource Channel；
Step 4, sets vacuum test mode；
Step 5, the controlling test mode set according to step 4 performs vacuum test；
Step 6, the data to vacuum test are monitored in real time；
Step 7, vacuum test data output pattern analysis；
Step 8, terminates.
The positive effect of the present invention is：The present invention is transmitted true by programmable power supply, temperature acquisition, Ethernet
Empty test data, can output data in time, improve data constantly property, using Graph analysis method, can be divided
Analyse vacuum test data validity, integrality, tightness and prediction space environment situation.
Brief description of the drawings
Fig. 1 is the composition schematic diagram of vacuum test control system of the present invention.
Fig. 2 is the schematic flow sheet of vacuum test control system method of the present invention.
Embodiment
Present pre-ferred embodiments are provided below in conjunction with the accompanying drawings, to describe technical scheme in detail.
Fig. 1 is the composition schematic diagram of vacuum test control system of the present invention.As shown in figure 1, vacuum test control of the present invention
System processed mainly includes：
Temperature data imports library module 110 in real time, gathers, arranges in real time for setting up temperature data；
Programmable power supply channel sets up module 120, for setting up multiple power supply channels；
Programmable power supply control module 130, for according to self-defined experiment process, to programmable power supply control；
Temperature current voltage data output module 140, for setting up data output interface；
Graphical real-time monitoring module 150, for graphical analyze data content.
Wherein, the temperature data imports library module and is gathered including temperature data format protocol, in real time, imports number in real time
According to storehouse, Information Security is good, strong in real time.The programmable power supply channel, which sets up module, includes power supply title, channel status.
The programmable power supply control module uses following control mode：Current control, voltage control, temperature control, temperature control current
Mode, embodies Suresh Kumar control.The temperature current voltage data output module includes temperature output interface, electric current
Output interface, voltage output interface.The graphical real-time monitoring module is using following graphical monitor mode in real time：
Temperature data is graphically analyzed, current data is graphically analyzed, voltage data is graphically analyzed, visual good.
As shown in Fig. 2 vacuum test control method of the present invention is mainly included the following steps that：
Step one, data acquisition, is controlled vacuum test data receiver, transmission, storage and programmable power supply procedural style；
Step 2, temperature data is imported in real time；
Step 3, sets up how program control Resource Channel；
Step 4, set vacuum test mode, have current control, voltage control, temperature control vacuum test mode,；
Step 5, the controlling test mode set according to step 4 performs vacuum test；
Step 6, the data to vacuum test are monitored in real time；
Step 7, vacuum test data output pattern analysis, by pattern analysis data, there is curve map, column diagram point
Analyse vacuum test data；
Step 8, terminates.
The step 2 includes temperature data format protocol, in real time collection, imports database.The step 3 includes electricity
The foundation of source name, channel status.The step 4 includes current control, voltage control, temperature control, temperature control current
Mode.The step 7 is graphically analyzed including temperature data, current data is graphically analyzed, voltage data graphically divides
Analysis.
To sum up, the present invention is not required to vacuum test data type first, it is to avoid polymorphic type many data managements, using program control
Power supply, ethernet communication channel and Data Input Interface service, the method for output interface service, are substantially increased
Stability, reliability, the accuracy of data, and effectively reduce cost payout；Meanwhile, the present invention also enters to data value
Row is shown in time, graphical analyze data so that vacuum test data application is more flexible.For the later stage every profession and trade it is true
Empty test data application, spacecraft vacuum test have established good basis.
The specific embodiment of the present invention is described above.It is to be appreciated that the invention is not limited in upper
Particular implementation is stated, those skilled in the art can make various deformations or amendments within the scope of the claims,
This has no effect on the substantive content of the present invention.
Claims (7)
1. a kind of vacuum test control system, it is characterised in that it includes：
Temperature data imports library module in real time, gathers, arranges in real time for setting up temperature data；
Programmable power supply channel sets up module, for setting up multiple power supply channels；
Programmable power supply control module, for according to self-defined experiment process, to programmable power supply control；
Temperature current voltage data output module, for setting up data output interface；
Graphical real-time monitoring module, for graphical analyze data content.
2. vacuum test control system as claimed in claim 1, it is characterised in that the temperature data is imported in real time
Library module includes temperature data format protocol, in real time collection, imports database.
3. vacuum test control system as claimed in claim 1, it is characterised in that the programmable power supply channel is set up
Module includes power supply title, channel status.
4. vacuum test control system as claimed in claim 1, it is characterised in that the programmable power supply control module
Using following control mode：Current control, voltage control, temperature control, temperature control current mode.
5. vacuum test control system as claimed in claim 1, it is characterised in that the temperature current voltage data
Output module includes temperature output interface, current output interface, voltage output interface.
6. vacuum test control system as claimed in claim 1, it is characterised in that the graphical monitoring mould in real time
Block is using following graphical monitor mode in real time：Temperature data is graphically analyzed, current data is graphically analyzed, voltage number
According to graphical analysis.
7. a kind of vacuum test control method, it is characterised in that it comprises the following steps：
Step one, data acquisition, is controlled vacuum test data receiver, transmission, storage and programmable power supply procedural style；
Step 2, temperature data is imported in real time；
Step 3, sets up how program control Resource Channel；
Step 4, sets vacuum test mode；
Step 5, the controlling test mode set according to step 4 performs vacuum test；
Step 6, the data to vacuum test are monitored in real time；
Step 7, vacuum test data output pattern analysis；
Step 8, terminates.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610218092.XA CN107272451A (en) | 2016-04-08 | 2016-04-08 | Vacuum test control system and method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610218092.XA CN107272451A (en) | 2016-04-08 | 2016-04-08 | Vacuum test control system and method |
Publications (1)
| Publication Number | Publication Date |
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| CN107272451A true CN107272451A (en) | 2017-10-20 |
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| CN201610218092.XA Pending CN107272451A (en) | 2016-04-08 | 2016-04-08 | Vacuum test control system and method |
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Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101770225A (en) * | 2008-12-29 | 2010-07-07 | 北京卫星环境工程研究所 | Centralized monitoring system for multiple sets of spacecraft thermal-vacuum environment simulating equipment |
| CN101769825A (en) * | 2008-12-29 | 2010-07-07 | 北京卫星环境工程研究所 | Tracking temperature control device for spacecraft thermal vacuum test |
| CN104483993A (en) * | 2014-11-07 | 2015-04-01 | 北京卫星环境工程研究所 | Temperature automatic control system and control method of alternating thermal load test-pieces under space environment |
| CN104731131A (en) * | 2014-11-14 | 2015-06-24 | 中国科学院力学研究所 | Spacecraft thermal vacuum testing temperature control method |
| RU2564056C1 (en) * | 2014-05-30 | 2015-09-27 | Акционерное общество "Военно-промышленная корпорация "Научно-производственное объединение машиностроения" (АО "ВПК "НПО машиностроения") | Method of heat-vacuum test of spacecraft |
-
2016
- 2016-04-08 CN CN201610218092.XA patent/CN107272451A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101770225A (en) * | 2008-12-29 | 2010-07-07 | 北京卫星环境工程研究所 | Centralized monitoring system for multiple sets of spacecraft thermal-vacuum environment simulating equipment |
| CN101769825A (en) * | 2008-12-29 | 2010-07-07 | 北京卫星环境工程研究所 | Tracking temperature control device for spacecraft thermal vacuum test |
| RU2564056C1 (en) * | 2014-05-30 | 2015-09-27 | Акционерное общество "Военно-промышленная корпорация "Научно-производственное объединение машиностроения" (АО "ВПК "НПО машиностроения") | Method of heat-vacuum test of spacecraft |
| CN104483993A (en) * | 2014-11-07 | 2015-04-01 | 北京卫星环境工程研究所 | Temperature automatic control system and control method of alternating thermal load test-pieces under space environment |
| CN104731131A (en) * | 2014-11-14 | 2015-06-24 | 中国科学院力学研究所 | Spacecraft thermal vacuum testing temperature control method |
Non-Patent Citations (2)
| Title |
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| 冯尧等: "航天器真空热试验测控系统软件结构设计与建模", 《航天器环境工程》 * |
| 裴一飞等: ""嫦娥一号"卫星真空热试验中的技术关键", 《航天器环境工程》 * |
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Application publication date: 20171020 |