CN201974675U - Centralized monitoring system applicable to parallel test for multiple spacecrafts - Google Patents
Centralized monitoring system applicable to parallel test for multiple spacecrafts Download PDFInfo
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- CN201974675U CN201974675U CN 201020671321 CN201020671321U CN201974675U CN 201974675 U CN201974675 U CN 201974675U CN 201020671321 CN201020671321 CN 201020671321 CN 201020671321 U CN201020671321 U CN 201020671321U CN 201974675 U CN201974675 U CN 201974675U
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Abstract
The utility model discloses a centralized monitoring system applicable to parallel test for multiple spacecrafts, which comprises tested satellites, measuring and controlling systems, power supply and distribution systems, control systems, a master control server and testing computers. One tested satellite, one measuring and controlling system, one power supply and distribution system and one control system form a tested spacecraft unit, the master control server is arranged between the tested spacecraft unit and each testing computer and used for receiving and processing remote metering source codes and uplinking routes of remote control commands, each testing computer is used for completing testing process control and data monitoring for the tested spacecraft unit corresponding to one tested spacecraft unit. Since the master control server is added between a front measured object and a testing device, test for multiple satellites can be realized by one testing device, and parallel test for multiple satellites can be completed by one group of staff. Accordingly, resources for test are saved and testing efficiency is improved.
Description
Technical field
The utility model relates to a kind of centralized monitoring system that is applicable to many spacecrafts concurrent testing, is mainly used in parallel batch of Navsat and produces the Centralized Monitoring of test.
Background technology
A corresponding cover ground checkout equipment and a collection of tester of next satellite of single star test pattern, increase along with space launch mission, when needs are tested simultaneously to multi-satellite, if adopt existing test mode, the test of each satellite all needs a cover ground testing system and a tester, then need to drop into more costs, cause the testing apparatus utilization factor low.Therefore must adopt a kind of new method for managing and monitoring to organize whole test system and testing process, reduce human cost thereby improve plant factor.
The utility model content
Technology of the present utility model is dealt with problems and is: overcome the deficiencies in the prior art, a kind of centralized monitoring system that is applicable to many spacecrafts concurrent testing is provided, saved test resource, improved testing efficiency.
Technical solution of the present utility model is: a kind of centralized monitoring system that is applicable to many spacecrafts concurrent testing, comprise tested satellite, TT﹠C system, power supply-distribution system, control system, overhead control server and test computer are formed, every tested satellite, a TT﹠C system, a power supply-distribution system and a bench control system are formed one group of tested spacecraft unit, TT﹠C system is uploaded remote signal to tested satellite, receive the telesignalisation that passes under the tested satellite, power supply-distribution system provides power supply for tested satellite, control system is controlled tested satellite action, the overhead control server is arranged between tested spacecraft unit and the test computer, the overhead control server is finished the reception and the processing of remote measurement source code, the route of up telecommand, the corresponding one group of tested spacecraft unit of each test computer is finished tested spacecraft unit is carried out testing process control and data monitoring.
The utility model beneficial effect compared with prior art is: the utility model increases the overhead control server between front end measurand and testing apparatus, realized utilizing a cover testing apparatus to finish the test of multi-satellite, one cover personnel finish many stars concurrent testing, thereby saved test resource, improved test and imitated.
Description of drawings
Fig. 1 is that system of the present utility model forms structural drawing.
Embodiment
For being suitable for the Centralized Monitoring management of many spacecrafts concurrent testing, the utility model proposes a kind of new test pattern, this test pattern is divided into three levels to ground checkout equipment from structure: measurand, overhead control server and testing apparatus.Divide timing at test network, will test front-end equipment and testing apparatus and be divided into two test network segments, avoid the network management confusion.
As shown in Figure 1, concrete composition of the present utility model and network structure are as follows: monitoring management system is divided into three parts, is respectively prefix area, service area and operational applications district, and placing measurand in the prefix area is satellite and uphole equipment; Place the overhead control server in the service area; Operational applications is placed ground checkout equipment in the district, planning according to integration test, the armamentarium of service area is placed in the data machine room, the equipment in prefix area and operational applications district is placed between test, during large-scale experiment, prefix area equipment can change factory with satellite, and operational applications district equipment can keep motionless, and measurand is carried out unified management and control by the overhead control server.
The prefix area mainly comprises the special test equipment of contacting directly with satellite, as ground observing and controlling system, ground power supply and distribution system, the ground control system of present each model satellite.Every tested satellite, TT﹠C system, power supply-distribution system and a bench control system are formed one group of tested spacecraft unit, TT﹠C system is uploaded remote signal to tested satellite, receive the telesignalisation that passes under the tested satellite, power supply-distribution system provides power supply for tested satellite, and control system applies the action of control program control satellite to tested satellite.
Service area is the core space of satellite comprehensive testing turn-key system, is whole ISP, mainly finishes the reception and the processing of remote measurement source code, the route of up telecommand.The principle of work of overhead control server is: in test network, definition also realizes a sets of data interaction protocol, the integrated management, the telemetry that realize test data, test instruction and subsystem data are distributed to each subsystem by the master control server, reach the effect that each subsystem test data are effectively shared.The overhead control server adopts HP server or IBM server, adopts LINUX or UNIX operating system.
The operational applications district is the main man-machine interaction district of Centralized Monitoring management system, and corresponding work is finished in the various services that the overhead control server provides in the equipment utilization service area in this zone.Equipment in the operational applications district mainly is made up of general purpose PC, and different integration test application software is installed on the different machines to finish corresponding work.The satellite comprehensive testing application software be data show software, basic data management software, data query analysis software, test console etc.
The utility model not detailed description is a technology as well known to those skilled in the art.
Claims (1)
1. centralized monitoring system that is applicable to many spacecrafts concurrent testing, it is characterized in that: comprise tested satellite, TT﹠C system, power supply-distribution system, control system, overhead control server and test computer are formed, every tested satellite, a TT﹠C system, a power supply-distribution system and a bench control system are formed one group of tested spacecraft unit, TT﹠C system is uploaded remote signal to tested satellite, receive the telesignalisation that passes under the tested satellite, power supply-distribution system provides power supply for tested satellite, control system is controlled tested satellite action, the overhead control server is arranged between tested spacecraft unit and the test computer, the overhead control server is finished the reception and the processing of remote measurement source code, the route of up telecommand, the corresponding one group of tested spacecraft unit of each test computer is finished tested spacecraft unit is carried out testing process control and data monitoring.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201020671321 CN201974675U (en) | 2010-12-10 | 2010-12-10 | Centralized monitoring system applicable to parallel test for multiple spacecrafts |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201020671321 CN201974675U (en) | 2010-12-10 | 2010-12-10 | Centralized monitoring system applicable to parallel test for multiple spacecrafts |
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| CN201974675U true CN201974675U (en) | 2011-09-14 |
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| CN 201020671321 Expired - Lifetime CN201974675U (en) | 2010-12-10 | 2010-12-10 | Centralized monitoring system applicable to parallel test for multiple spacecrafts |
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Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103795593A (en) * | 2014-01-24 | 2014-05-14 | 武汉大学 | Testing system and method of uplink of high-speed communication processor of spaceship |
| CN106292636A (en) * | 2016-08-30 | 2017-01-04 | 北京宇航系统工程研究所 | A kind of integrated ground observing and controlling system |
| CN107884007A (en) * | 2017-10-25 | 2018-04-06 | 北京空间技术研制试验中心 | Manned spacecraft remote test system |
| CN107991902A (en) * | 2017-12-07 | 2018-05-04 | 北京空间技术研制试验中心 | A kind of modeling of electric power system of spacecraft and emulation mode |
| CN108287484A (en) * | 2018-02-05 | 2018-07-17 | 中国科学院光电技术研究所 | A method of being directed to the quick architecture testing system of aerospace system single machine test |
| CN112015166A (en) * | 2020-08-31 | 2020-12-01 | 湖北航天技术研究院总体设计所 | Portable survey and control equipment suitable for spacecraft |
| CN114024883A (en) * | 2021-11-05 | 2022-02-08 | 江西洪都航空工业集团有限责任公司 | Method, device and system for open-loop parallel testing of multiple products of data chain |
-
2010
- 2010-12-10 CN CN 201020671321 patent/CN201974675U/en not_active Expired - Lifetime
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103795593A (en) * | 2014-01-24 | 2014-05-14 | 武汉大学 | Testing system and method of uplink of high-speed communication processor of spaceship |
| CN103795593B (en) * | 2014-01-24 | 2017-07-11 | 武汉大学 | A kind of method of testing of airship high-speed communication processor up-link |
| CN106292636A (en) * | 2016-08-30 | 2017-01-04 | 北京宇航系统工程研究所 | A kind of integrated ground observing and controlling system |
| CN106292636B (en) * | 2016-08-30 | 2019-12-20 | 北京宇航系统工程研究所 | Integrated ground measurement and control system |
| CN107884007A (en) * | 2017-10-25 | 2018-04-06 | 北京空间技术研制试验中心 | Manned spacecraft remote test system |
| CN107991902A (en) * | 2017-12-07 | 2018-05-04 | 北京空间技术研制试验中心 | A kind of modeling of electric power system of spacecraft and emulation mode |
| CN108287484A (en) * | 2018-02-05 | 2018-07-17 | 中国科学院光电技术研究所 | A method of being directed to the quick architecture testing system of aerospace system single machine test |
| CN112015166A (en) * | 2020-08-31 | 2020-12-01 | 湖北航天技术研究院总体设计所 | Portable survey and control equipment suitable for spacecraft |
| CN114024883A (en) * | 2021-11-05 | 2022-02-08 | 江西洪都航空工业集团有限责任公司 | Method, device and system for open-loop parallel testing of multiple products of data chain |
| CN114024883B (en) * | 2021-11-05 | 2023-11-17 | 江西洪都航空工业集团有限责任公司 | Method, device and system for open-loop parallel testing of multiple products of data link |
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Legal Events
| Date | Code | Title | Description |
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| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CX01 | Expiry of patent term | ||
| CX01 | Expiry of patent term |
Granted publication date: 20110914 |