CN107819507A - The collocation method and method of testing of a kind of multi-level test system for satellite TT＆C system - Google Patents
The collocation method and method of testing of a kind of multi-level test system for satellite TT＆C system Download PDFInfo
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- CN107819507A CN107819507A CN201711171382.4A CN201711171382A CN107819507A CN 107819507 A CN107819507 A CN 107819507A CN 201711171382 A CN201711171382 A CN 201711171382A CN 107819507 A CN107819507 A CN 107819507A
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- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04B—TRANSMISSION
- H04B7/00—Radio transmission systems, i.e. using radiation field
- H04B7/14—Relay systems
- H04B7/15—Active relay systems
- H04B7/185—Space-based or airborne stations; Stations for satellite systems
- H04B7/1851—Systems using a satellite or space-based relay
- H04B7/18519—Operations control, administration or maintenance
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- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04L—TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
- H04L41/00—Arrangements for maintenance, administration or management of data switching networks, e.g. of packet switching networks
- H04L41/08—Configuration management of networks or network elements
- H04L41/0803—Configuration setting
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- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04L—TRANSMISSION OF DIGITAL INFORMATION, e.g. TELEGRAPHIC COMMUNICATION
- H04L43/00—Arrangements for monitoring or testing data switching networks
- H04L43/50—Testing arrangements
Abstract
The invention discloses a kind of collocation method and method of testing of the multi-level test system for satellite TT＆C system, contain enforceable human-computer interaction system parameter calibration, the tri-layer software and hardware composition strictly divided, the information management monitoring mechanism of the double clients of two levels, and real time data inquiry and interpretation mode, the also export comprising test data bag.The present invention has good versatility and good portability, can apply to the test system of the aerospace product of standardization type spectrum, there is provided flexible and efficient test Solution, to meet reliability demand that satellite system is constantly lifted.
Description
Technical field
The present invention relates to the multi-level testing field of Satellite TT product, and in particular to a kind of for satellite TT＆C system
The collocation method and method of testing of multi-level test system.
Background technology
At present, the development of China's spacecraft enters a new period.With to the dual of product delivery cycle and quality
It is required that Satellite Product progressively turns to universal goods shelf type spectrum unit from customization unit.Especially in recent years, the networking satellite such as Big Dipper
Batch high quality requirement for delivery so that there is serious conflict in test coverage completeness and the delivery cycle of unit.For
Adapt to the new development feature of Satellite Product and change, matching versatility automatization test system should be formed, with it is more, fast,
Completion test assignment that is good, saving.
At present, system level testing equipment is changed into centralized management system, the integrated journey of equipment by past dispersion
Degree generally improves.TT＆C system test system common at present is integrated with low frequency, base band and radio frequency, but level on hardware
The test for changing automation is not yet used widely.It is primarily due to the highly reliable particularity of Satellite Product so that surveys
Self-defined the manual test demand and automatic test demand of test system exist simultaneously, are sent and artificial interpretation from traditional-handwork
The conversion ratio that implementation process goes to automated execution is not high, takes considerable time, and is readily incorporated mistake.
Type spectrum observing and controlling unit meets generalization, the design requirement of standardization, and its test system also possesses generalization, automation
Ability, but the reliance security of satellite borne equipment requires high, and the interpretation requirement of real-time of test data is high, to test system
Propose higher requirement.
At present, the test system of TT＆C system typically completes low frequency interface configuration, system configuration by interface configuration interface
TT ＆ C architecture definition is completed at interface, and the traversal of test scene is carried out one by one after then carrying out manual configuration to various parameters again.Before
Two Step Times are shorter but complex and need operating personnel to confirm that last process is then to ensure the validity of test
Mainly repeatable operation, takes that longer, record data is more and operational error easily occurs, realizes that automatic test can be with
Greatly improve testing efficiency.
The solution of the present invention is to change regarding to the issue above to what the existing method of testing for satellite TT＆C system was carried out
Enter.
The content of the invention
In order to overcome deficiency of the prior art, the present invention provides a kind of multi-level test system for satellite TT＆C system
The collocation method and method of testing of system, substantially increase the testing efficiency of TT＆C system.
In order to reach foregoing invention purpose, technical scheme is as follows used by solving its technical problem：
The invention discloses a kind of collocation method of the multi-level test system for satellite TT＆C system, do not possessing height
In the case of level software and hardware, comprise the following steps：
Step A1：Start low level software and hardware, hardware system completes self-test, startup of server work；
Step A2：Start middle-level software and hardware, the configuration of low layer interface between software and hardware and Working mould are completed in client-server
Formula configures；
Step A3：Test traversal is carried out to each test scene under mode of operation manually.
The present invention discloses a kind of collocation method of the multi-level test system for satellite TT＆C system in addition, is possessing
In the case of high-level software and hardware, comprise the following steps：
Step B1：Start low level software and hardware, hardware system completes self-test, startup of server work；
Step B2：Start middle-level software and hardware, the configuration of low layer interface between software and hardware and Working mould are completed in client-server
Formula configures；
Step B3：Start high-level software and hardware, corresponding configuration file is loaded according to the configuration of middle-level software and hardware, started
Client；
Step B4：Carry out systematic parameter and force demarcation flow, and force to record null value, line loss, mode of operation；
Step B5：Test course is selected, starts automatic test；
Step B6：Data base administration is carried out in test process in real time, test can export as tabular packet after terminating.
The invention also discloses a kind of method of testing of the multi-level test system for satellite TT＆C system, including it is following
Testing procedure：
Step C1：Automatization test system is divided into 3 levels from physics and software view, high-level software and hardware enters
Row automatic flow controls to be recorded with test result data；Middle-level software and hardware carries out configuration control to test equipment and equipment under test
System and real time graphical show and recorded；Low level software and hardware completes the direct control of interface, base band and radio frequency, and anti-to upper strata
Feedforward information；
Step C2：In order to take into account the automatic test traveled through entirely and conventional manual test demand simultaneously, double visitors are devised
The mechanism of information feedback of family end pattern：In the case where not being equipped with high-level software and hardware, middle-level software and hardware structure client/clothes
The test system for device pattern of being engaged in, low level software and hardware is controlled, complete manual test；Under conditions of high-level software and hardware is equipped with,
Client in high-level software and hardware is controlled to server, but server info feeds back to high-rise and middle level client simultaneously
End so that high level and the respective state of display that can be simultaneously independent in the human-computer interaction interface in middle level, be easy to different levels
The non-interfering monitoring test process of tester；
Step C3：In order to prevent tester from carrying out invalid test in the case of no completion system calibrating, automation is surveyed
Test system Qiang Zhiyaoqius the calibration that system null value, up line loss are completed according to man-machine interface before activation；
Step C4：Data query in high-level software and hardware works independently with scenery control, and inquiry operation does not influence automatically
Change the operation of test；
Step C5：High-level software and hardware carries out real-time judge and overproof mark according to default indication range to test result
Know, be stored in database, improve the analysis efficiency of interpretation personnel；
Step C6：In order to prevent automatic test device under test from causing latent lesion, automatic test does not change to be measured
Equipment working state, only carries out test traversal under specified unit operating mode, and the switching of Devices to test operating mode and automatic test are gone through
Journey configuration is manually operated by tester；
Step C7：Low level software and hardware configuration file is divided into two aspects, respectively interface configuration file and program
Control file so that can carry out generalization test using the unit of different interface shape and TT ＆ C architecture.
Further, in step C2, double client-side information interactions is further comprised, specifically include following step
Suddenly：
Step C21：High-level software and hardware shows the testing progress of current test course, and test result is recorded,
Provide sentence read result；
Step C22：Middle-level software and hardware is acquired and shown to whole states of test equipment and Devices to test, is easy to
Tester carries out analysis judgement to details；
Step C23：High-level software and hardware is controlled by client to middle-level client software at work, middle level
Secondary client is acquired afterwards to low layer operation result while feeds back to higher-layer client and middle level client software；
Step C24：Higher-layer client and the work of the data query of middle level client user interface are not interfere with each other, but in high level
Client implementation controls the stage, and middle level client only works as status display, misaligns stratum server and be controlled, avoid sending out
Raw control hazard.
Further, in step C7, the interface configuration file is used to be responsible for unit instruction, low frequency interface access tune
Reason.
Further, in step C7, described program control file is used to be responsible for TT ＆ C architecture, frequency configuration.
The present invention is allowed to compared with prior art, have the following advantages that and actively imitate due to using above technical scheme
Fruit：
The present invention has good versatility and good portability, can apply to standardize the aerospace production of type spectrum
The test system of product, there is provided flexible and efficient test Solution, to meet reliability demand that satellite system is constantly lifted.
Brief description of the drawings
In order to illustrate the technical solution of the embodiments of the present invention more clearly, required use in being described below to embodiment
Accompanying drawing be briefly described.It is clear that drawings in the following description are only some embodiments of the present invention, for ability
For field technique personnel, on the premise of not paying creative work, other accompanying drawings can also be obtained according to these accompanying drawings.It is attached
In figure：
Fig. 1 is the test system division figure of the present invention；
Fig. 2 is that a kind of first pass of the collocation method of multi-level test system for satellite TT＆C system of the invention shows
It is intended to；
Fig. 3 is that a kind of second procedure of the collocation method of multi-level test system for satellite TT＆C system of the invention is shown
It is intended to；
Fig. 4 is a kind of flow signal of the method for testing of multi-level test system for satellite TT＆C system of the invention
Figure；
Fig. 5 is the double client-side information flow graphs of double level of the present invention；
Fig. 6 be a kind of multi-level test system for satellite TT＆C system of the invention method of testing in step C2 letter
Cease interaction flow schematic diagram.
Embodiment
Below with reference to the accompanying drawing of the present invention, clear, complete description is carried out to the technical scheme in the embodiment of the present invention
And discussion, it is clear that as described herein is only a part of example of the present invention, is not whole examples, based on the present invention
In embodiment, the every other implementation that those of ordinary skill in the art are obtained on the premise of creative work is not made
Example, belongs to protection scope of the present invention.
It is well known that crucial subsystem of the TT＆C system as satellite, it tests intensity and test coverage for a long time
Greatly paid close attention to.It is increasingly complicated with the use environment of TT＆C system, to the test condition traversal and data of TT＆C system
The shortcomings that record completeness requires also more and more higher, and manually efficiency is low, error rate is high present in test also gradually protrudes.
With differentiation of the satellite fields product from customed product to type spectrum goods shelf productses, in order to meet that standardization and efficient test will
Ask, the actual test demand of present patent application combination TT＆C system, devise a kind of multi-level survey for satellite TT＆C system
Test system, enforceable human-computer interaction system parameter calibration is specifically contained, the tri-layer software and hardware composition strictly divided, two layers
The information management monitoring mechanism of secondary double clients, and real time data inquiry and interpretation mode, also leading comprising test data bag
Go out.The function of the test system defines the intensive test for being both easy to the standard testing stage, is also applied for the independent survey of development stage
Examination.The invention is not only applicable to the test of TT＆C system, is applied equally well to the survey of TT＆C system core singleness control answering machine
Examination.
Embodiment one
Fig. 1 schemes for the system division of the present invention, the testing requirement of the invention according to TT＆C system, and three levels of completion are
System division, and be respectively configured in the test starting stage.As shown in Fig. 2 the invention discloses one kind to be directed to Satellite TT system
The collocation method of the multi-level test system of system, in the case where not possessing high-level software and hardware, test system can independently be entered
Row manual test, its system configuration process comprise the following steps：
Step A1：Start low level software and hardware, hardware system completes self-test, startup of server work；
Step A2：Start middle-level software and hardware, the configuration of low layer interface between software and hardware and Working mould are completed in client-server
Formula configures；
Step A3：Test traversal is carried out to each test scene under mode of operation manually.
Embodiment two
As shown in figure 3, the present invention discloses a kind of configuration of the multi-level test system for satellite TT＆C system in addition
Method, in the case where possessing high-level software and hardware, whole test system configurations process comprises the following steps：
Step B1：Start low level software and hardware, hardware system completes self-test, startup of server work；
Step B2：Start middle-level software and hardware, the configuration of low layer interface between software and hardware and Working mould are completed in client-server
Formula configures；
Step B3：Start high-level software and hardware, corresponding configuration file is loaded according to the configuration of middle-level software and hardware, started
Client；
Step B4：Carry out systematic parameter and force demarcation flow, and force to record null value, line loss, mode of operation；
Step B5：Test course is selected, starts automatic test；
Step B6：Data base administration is carried out in test process in real time, test can export as tabular packet after terminating.
Wherein, high-level software and hardware is completely independent work with middle-level software and hardware, conveniently adapts to different test requests, because
It is the standardized test traveled through entirely for automatic test course, it is time-consuming longer, only carried out in the standard testing stage, debugging stage etc.
Development stage stills need manual test；Interface define it is constant on the premise of, each level software and hardware can with independent maintenance and upgrading,
Substantially increase the flexibility of test system.
Embodiment three
As shown in figure 4, the invention also discloses a kind of test side of the multi-level test system for satellite TT＆C system
Method, including following testing procedure：
Step C1：Automatization test system is divided into 3 levels from physics and software view, high-level software and hardware enters
Row automatic flow controls and test result data record (containing data base administration)；Middle-level software and hardware is to test equipment and is tested
Equipment carries out configuration control and real time graphical shows and recorded；Low level software and hardware completes the direct of interface, base band and radio frequency
Control (containing TT ＆ C architecture, signal intensity etc.), and to upper strata feedback information；
Step C2：In order to take into account the automatic test traveled through entirely and conventional manual test demand simultaneously, double visitors are devised
The mechanism of information feedback of family end pattern：In the case where not being equipped with high-level software and hardware, middle-level software and hardware structure client/clothes
The test system for device pattern of being engaged in, low level software and hardware is controlled, complete manual test；Under conditions of high-level software and hardware is equipped with,
Client in high-level software and hardware is controlled to server, but server info feeds back to high-rise and middle level client simultaneously
End so that high level and the respective state of display that can be simultaneously independent in the human-computer interaction interface in middle level, be easy to different levels
The non-interfering monitoring test process of tester；
Step C3：In order to prevent tester from carrying out invalid test in the case of no completion system calibrating, automation is surveyed
Test system Qiang Zhiyaoqius the calibration that system null value, up line loss are completed according to man-machine interface before activation；
Step C4：Data query in high-level software and hardware works independently with scenery control, and inquiry operation does not influence automatically
Change the operation of test；
Step C5：High-level software and hardware carries out real-time judge and overproof mark according to default indication range to test result
Know, be stored in database, improve the analysis efficiency of interpretation personnel；
Step C6：In order to prevent automatic test device under test from causing latent lesion, automatic test does not change to be measured
Equipment working state, only carries out test traversal under specified unit operating mode, and the switching of Devices to test operating mode and automatic test are gone through
Journey configuration is manually operated by tester；
Step C7：Low level software and hardware configuration file is divided into two aspects, respectively interface configuration file and program
Control file so that can carry out generalization test using the unit of different interface shape and TT ＆ C architecture.
Fig. 5 is the double client-side information flow graphs of double level of the present invention, and the present invention is according to the automatic test need of TT＆C system
Ask, test relevant information is fed back and recorded in two aspects, as shown in fig. 6, whole information interactive process, including it is following
Step：
Step C21：High-level software and hardware shows the testing progress of current test course, and test result is recorded,
Provide sentence read result；
Step C22：Middle-level software and hardware is acquired and shown to whole states of test equipment and Devices to test, is easy to
Tester carries out analysis judgement to details；
Step C23：High-level software and hardware is controlled by client to middle-level client software at work, middle level
Secondary client is acquired afterwards to low layer operation result while feeds back to higher-layer client and middle level client software；
Step C24：Higher-layer client and the work of the data query of middle level client user interface are not interfere with each other, but in high level
Client implementation controls the stage, and middle level client only works as status display, misaligns stratum server and be controlled, avoid sending out
Raw control hazard.
Further, in step C7, the interface configuration file is used to be responsible for unit instruction, low frequency interface access tune
Reason.
Further, in step C7, described program control file is used to be responsible for TT ＆ C architecture, frequency configuration.
The present invention is allowed to compared with prior art, have the following advantages that and actively imitate due to using above technical scheme
Fruit：
The present invention has good versatility and good portability, can apply to standardize the aerospace production of type spectrum
The test system of product, there is provided flexible and efficient test Solution, to meet reliability demand that satellite system is constantly lifted.
The foregoing is only a preferred embodiment of the present invention, but protection scope of the present invention be not limited thereto,
Any one skilled in the art the invention discloses technical scope in, the change or replacement that can readily occur in,
It should all be included within the scope of the present invention.Therefore, protection scope of the present invention should be with scope of the claims
It is defined.
Claims (6)
1. the collocation method of a kind of multi-level test system for satellite TT＆C system, it is characterised in that do not possessing high level
In the case of secondary software and hardware, comprise the following steps：
Step A1：Start low level software and hardware, hardware system completes self-test, startup of server work；
Step A2：Start middle-level software and hardware, complete the configuration of low layer interface between software and hardware in client-server and mode of operation is matched somebody with somebody
Put；
Step A3：Test traversal is carried out to each test scene under mode of operation manually.
2. the collocation method of a kind of multi-level test system for satellite TT＆C system, it is characterised in that high-level possessing
In the case of software and hardware, comprise the following steps：
Step B1：Start low level software and hardware, hardware system completes self-test, startup of server work；
Step B2：Start middle-level software and hardware, complete the configuration of low layer interface between software and hardware in client-server and mode of operation is matched somebody with somebody
Put；
Step B3：Start high-level software and hardware, corresponding configuration file is loaded according to the configuration of middle-level software and hardware, starts client
End；
Step B4：Carry out systematic parameter and force demarcation flow, and force to record null value, line loss, mode of operation；
Step B5：Test course is selected, starts automatic test；
Step B6：Data base administration is carried out in test process in real time, test can export as tabular packet after terminating.
3. the method for testing of a kind of multi-level test system for satellite TT＆C system, it is characterised in that including following test
Step：
Step C1：Automatization test system is divided into 3 levels from physics and software view, high-level software and hardware is carried out certainly
Dynamicization Row control records with test result data；Middle-level software and hardware to test equipment and equipment under test carry out configuration control and
Real time graphical shows and recorded；Low level software and hardware completes the direct control of interface, base band and radio frequency, and to upper strata feedback letter
Breath；
Step C2：In order to take into account the automatic test traveled through entirely and conventional manual test demand simultaneously, double clients are devised
The mechanism of information feedback of pattern：In the case where not being equipped with high-level software and hardware, middle-level software and hardware structure client/server
The test system of pattern, low level software and hardware is controlled, complete manual test；It is high-rise under conditions of high-level software and hardware is equipped with
Client in secondary software and hardware is controlled to server, but server info feeds back to high-rise and middle level client simultaneously, makes
The respective state of display that can be simultaneously independent in the high-rise and human-computer interaction interface in middle level is obtained, is easy to the tester of different levels
The non-interfering monitoring test process of member；
Step C3：In order to prevent tester from carrying out invalid test, automatic test system in the case of no completion system calibrating
System Qiang Zhiyaoqius the calibration that system null value, up line loss are completed according to man-machine interface before activation；
Step C4：Data query in high-level software and hardware works independently with scenery control, and inquiry operation does not influence automation and surveyed
The operation of examination；
Step C5：High-level software and hardware carries out real-time judge and overproof mark according to default indication range to test result, deposits
Enter database, improve the analysis efficiency of interpretation personnel；
Step C6：In order to prevent automatic test device under test from causing latent lesion, automatic test does not change Devices to test
Working condition, only carries out test traversal under specified unit operating mode, and the switching of Devices to test operating mode and automatic test course are matched somebody with somebody
Put manually operated by tester；
Step C7：Low level software and hardware configuration file is divided into two aspects, respectively interface configuration file and programme-control
File so that can carry out generalization test using the unit of different interface shape and TT ＆ C architecture.
4. a kind of method of testing of multi-level test system for satellite TT＆C system according to claim 3, it is special
Sign is, in step C2, further comprises double client-side information interactions, specifically includes following steps：
Step C21：High-level software and hardware shows the testing progress of current test course, and test result is recorded, and provides
Sentence read result；
Step C22：Middle-level software and hardware is acquired and shown to whole states of test equipment and Devices to test, is easy to test
Personnel carry out analysis judgement to details；
Step C23：High-level software and hardware is controlled by client to middle-level client software at work, middle-level visitor
Family end is acquired afterwards to low layer operation result while feeds back to higher-layer client and middle level client software；
Step C24：Higher-layer client and the work of the data query of middle level client user interface are not interfere with each other, but in high-rise client
End is implemented the control stage, and middle level client only works as status display, misaligns stratum server and is controlled, avoids controlling
System conflict.
5. a kind of method of testing of multi-level test system for satellite TT＆C system according to claim 3, it is special
Sign is, in step C7, the interface configuration file is used to be responsible for unit instruction, low frequency interface access conditioning.
6. a kind of method of testing of multi-level test system for satellite TT＆C system according to claim 3, it is special
Sign is, in step C7, described program control file is used to be responsible for TT ＆ C architecture, frequency configuration.
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| CN109992457A (en) * | 2019-03-11 | 2019-07-09 | 清华大学 | The test macro of stratification configurable type microsatellite |
| CN112577535A (en) * | 2019-09-27 | 2021-03-30 | 陕西星邑空间技术有限公司 | Data processing method, device and system |
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| CN106649112A (en) * | 2016-12-20 | 2017-05-10 | 中国电子科技集团公司第五十四研究所 | Platform plug-in technology oriented testing method |
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| CN112577535A (en) * | 2019-09-27 | 2021-03-30 | 陕西星邑空间技术有限公司 | Data processing method, device and system |
| CN112988218A (en) * | 2021-02-05 | 2021-06-18 | 上海航天卫星应用有限公司 | Configurable information flow management method and system |
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