CN102722437A - Spacecraft test system and spacecraft test method based on assemblies and scripts - Google Patents
Spacecraft test system and spacecraft test method based on assemblies and scripts Download PDFInfo
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Abstract
The invention discloses a spacecraft test system based on assemblies and scripts. The spacecraft test system based on the assemblies and the scripts comprises a test case editing environment module and a test case executing environment module, wherein the test case editing environment module comprises a test assembly library, a script function library and a test case imaging interface; the test assembly library comprises test assemblies; the script function library comprises script functions; the test case imaging interface arranges the test assemblies, the script functions and/ or script placeholders by dragging according to a test case, sets parameters of the arranged test assemblies and edits scripts for the script placeholders so as to form the test case; and the test case executing environment module analyses the test case so as to form an executable sequence of the test case and executes the test case sequence in the testing process to finish the test. The invention also discloses a corresponding spacecraft test method. The test scripts and the test assemblies are combined to realize automatic test on a spacecraft.
Description
Technical field
The invention belongs to the spacecraft field tests, relate to a kind of spacecraft test macro and method based on assembly and script.
Background technology
The spacecraft model needs a large amount of test jobs in development process, automatization testing technique is by extensive employing.Existing automatization testing technique can be divided into based on script with based on the visualization component dual mode.The script grammer is flexible, and representation function is strong, but ease for use and intuitive are relatively poor, and inconvenience is safeguarded; The visualization component simple, intuitive, the test case editor that can realize What You See Is What You Get, but the testing process that assembly comprised solidifies, and systemic-function receives the restriction of Component Gallery scale, and very flexible is difficult for expansion.The spacecraft test event is numerous, logic is complicated and changeable, edits and safeguard substantive test script difficulty, and the visualization component that solidifies is difficult for satisfying new testing requirement.
Automatization test system (publication number is 10184711A) discloses a kind of automatization test system of supporting the different scripts that different automatized script language are realized.This system only supports the test case editor of script mode.
A kind of satellite automated test method (application number is CN201010597273.0) based on the test atom discloses a kind of method of carrying out the test case design based on the minimum test cell assembly of combination.Through the editing component attribute test case parameters is customized, finally generate test case script sequence.The execution flow process of each atom is solidified in this method, only can customize intraatomic parameter, lacks dirigibility.
Automatic test script implementation method and device (publication number is 101141319) based on the feature operation encapsulation are decomposed into the basic operation unit function and set up the basic operation unit function library by feature operation through extracting the test operation object; Basic operation unit function to same feature operation makes up, and with all basic operation unit function parameters of this feature operation as the feature operation function parameters, set up the feature operation function library; Be combined to form automatic test script to the feature operation function according to test case towards test case.This method and apparatus has improved the versatility of test case script, but script inadequately intuitively, easy care not.
A kind of satellite automated test frame system (publication number is 101216712) discloses a kind of based on the satellite automated test frame of instruction with criterion, and its test case adopts instruction sequence to describe, and the criterion separate, stored that and instruction is related is irrelevant with concrete use-case.But this method can not be described complicated flow process and data processing and analysis logic.
Summary of the invention
Technology of the present invention is dealt with problems and is: to the deficiency of prior art, a kind of spacecraft test macro and method of testing based on assembly and script is provided, with the test script formation test case that combines with test suite, realized the automatic test to spacecraft.
Technical solution of the present invention is:
Spacecraft test macro based on assembly and script according to the invention is supported in the test case and adds visual testing assembly and test script simultaneously.For test logic commonly used, adopt the mode that pulls assembly, editing component parameter to describe; For testing requirement special, that logic is complicated, adopt the mode of compile script to describe.Assembly, script may be combined in the same test case, thereby describe test case complicated and changeable.At last, through execution environment module of the present invention, automatically perform test case.
Said automatization test system comprises: test case editing environment module and test case execution environment module.
Said test case editing environment module comprises test suite storehouse, script function storehouse, test case graphic interface, and wherein, said test suite storehouse comprises test suite; Said script function storehouse comprises script function;
Said test case graphic interface is arranged described test suite, script function and/or script placeholder according to test case through pulling; And the said test suite of arranging carried out the parameter setting and said script placeholder is carried out the script editor, form test case;
Said test case execution environment module is resolved said test case, forms the test case sequence; And in test process, said test case sequence is carried out complete test.
Method of testing according to the invention may further comprise the steps:
In test case image conversion interface, arrange test suite, script function and/or script placeholder according to test purpose through pulling;
The logical relation of adjusting said test suite, script function and/or script placeholder according to testing process forms the test case framework;
Parameter to said test suite is provided with, and adds script function code formation test case and storage in said script placeholder position;
In said test case execution environment, extract said test case, and resolve to the test case sequence;
Said test case sequence is carried out the test of driving execution to spacecraft.
Further, said test suite comprises Service Component, flow process assembly and from package assembling, said Service Component is used for the packaging and testing business; Said flow process assembly is used to realize branch and flow process control; Saidly be packaged with one group of Service Component and/or flow process assembly from package assembling, the multiplexing function after can realizing encapsulating.
Further; Said test case execution environment module is when carrying out said test case sequence; Through setting up each test suite of thread execution and/or script function; And be that said test suite and/or script function provide detecting information issuing interface and test result to submit interface to, said test suite and script function are shared the global variable in the test case sequence implementation.
The present invention compared with prior art has following advantage:
The present invention has realized realizing the editor of test case through pulling test case and script placeholder.Through pulling test suite and script and it being carried out permutation and combination, can fast construction test case framework.On test case frame foundation; Further test suite and script function are edited; Can realize accurate description to test case; Thereby the mode that can utilize test suite and script function to mix is described the required test case of spacecraft, and implementation and can adapt to the design of spacecraft test case complicated and changeable simply, fast, flexibly.
Simultaneously; When test case is carried out; To carry out serializing by the test case that test suite and script function are formed through the test case execution environment, and the test case sequence after the serializing will be automatically performed, in the process of implementation; Test case and script function are carried out unified management, and make test case and script function share global variable.
Description of drawings
Fig. 1 is a synoptic diagram of the present invention;
Fig. 2 is a process flow diagram of the present invention.
Embodiment
Just combine accompanying drawing that the present invention is done further introduction below.
As shown in Figure 1, be structure principle chart of the present invention.System is connected in the satellite test network, when test case is finally carried out with instruction type control front end hardware testing apparatus, and the test data returned of receiving equipment.System is divided into test case editing environment and execution environment two parts.
The use-case editing environment comprises test suite storehouse, script function storehouse, test case graphic interface, component parameter editing interface and 5 modules of script editing interface.The test suite storehouse provides the visual testing assembly that a cover is graphical, can pull, and assembly specifically is divided into Service Component, flow process assembly and from three kinds of package assemblings.
Wherein, Service Component is realized the basic operation encapsulation to the spacecraft test service; The flow process assembly is realized branch, circulation process control; By User Defined, realize multiplexing function from package assembling with one group of Service Component and/or the further encapsulation of flow process assembly;
Blank script is provided in the script function storehouse, encapsulates script and script function certainly.Blank script does not contain any scripted code, encapsulates certainly that script is then edited and preserved by the user, reusable one section ripe shell script.The script function storehouse for editor's test script provide abundant, towards the common mathematical function of spacecraft test.The test case graphic interface shows with patterned way, supports directly to pull from test suite storehouse and script function storehouse, row portion test suite and script placeholder.Component parameter editing interface and script editing interface are respectively applied for editor's test suite parameter and compile script code.Test case deposits test case library in.
The use-case execution environment can be with test case from test case library reading assembly sequence and be translated as the script sequence, gives to carry out driven by engine and carry out.According to the use-case flow process, carry out the actuating logic that each assembly or script inner packet install respectively during execution.Assembly and script are shared the test data that equipment under test passes down.Test case execution environment module is in charge of the thread life cycle of each test suite and script, and public test process information display interface and test result memory interface is provided for test suite and script.Test case is presented as when carrying out to spacecraft, uphole equipment at last sends instruction, and reception, processing test data deposit test result in the test result storehouse.
As shown in Figure 2, flow process of the present invention is following:
(1) beginning;
(2) in the test case editing environment, pull test suite and script placeholder to the test case graphic interface;
(3) adjustment assembly and the script placeholder position relation (unnecessary operations) in test case forms the test case framework;
(4) editor's test suite parameter, write the test case script, accomplish customization of test case parameter and logic realization;
(5) generate test case and be saved to test case library;
(6) in test execution environments,, it is resolved to the test script sequence from test case library read test use-case.The script sequence is the flow process description script of whole cycle tests, does not relate to the test suite in concrete each step or the inside actuating logic of test script;
(7) by the execution of test case execution environment module drive test case sequence.When whenever implementing pacing examination assembly or script function, create a new thread, carry out the inner logic of test suite or script function for the test suite or the script function of current step;
(8) by carrying out each pacing examination assembly or the inner actuating logic of test script in the flow process, read test data from the test data shared drive, and the global variable shared of access test assembly, script;
(9) common interface that provided of test suite, script calls test case execution environment module, in the monitoring panel of test case execution environment module, issue test process information separately.
(10) common interface that provided of test suite, script calls test case execution environment module will execution result be separately submitted to test case execution environment module and is shown.
(11) the unified test result of preserving of test case execution environment module is to the test result storehouse;
(12) finish.
The unspecified part of the present invention belongs to general knowledge as well known to those skilled in the art.
Claims (6)
1. spacecraft test macro based on assembly and script is characterized in that comprising: test case editing environment module and test case execution environment module,
Said test case editing environment module comprises test suite storehouse, script function storehouse, test case graphic interface, and wherein, said test suite storehouse comprises test suite; Said script function storehouse comprises script function;
Said test case graphic interface is arranged described test suite, script function and/or script placeholder according to test case through pulling; And the said test suite of arranging carried out the parameter setting and said script placeholder is carried out the script editor, form test case;
Said test case execution environment module is resolved said test case, forms the executable sequence of test case; And the executable sequence to said test case carries out complete test in test process.
2. a kind of spacecraft test macro based on assembly and script as claimed in claim 1 is characterized in that: said test suite comprises Service Component, flow process assembly and from package assembling, said Service Component is used for the packaging and testing business; Said flow process assembly is used to realize branch and circulation process control; Saidly be packaged with one group of Service Component and/or flow process assembly from package assembling, the multiplexing function after can realizing encapsulating.
3. according to claim 1 or claim 2 a kind of spacecraft test macro system based on assembly and script; It is characterized in that: said test case execution environment module is when carrying out said test case sequence; Through setting up each test suite of thread execution and/or script function; And be that said test suite and/or script function provide detecting information issuing interface and test result to submit interface to, said test suite and script function are shared the global variable in the test case sequence implementation.
4. method of testing that adopts the said a kind of spacecraft test macro based on assembly and script of claim 1 is characterized in that may further comprise the steps:
In test case image conversion interface, arrange test suite, script function and/or script placeholder according to test purpose through pulling;
The logical relation of adjusting said test suite, script function and/or script placeholder according to testing process forms the test case framework;
Parameter to said test suite is provided with, and adds script function code formation test case and storage in said script placeholder position;
In said test case execution environment, extract said test case, and resolve to the test case sequence;
Said test case sequence is carried out the test of driving execution to spacecraft.
5. method of testing as claimed in claim 4 is characterized in that: said test suite comprises Service Component, flow process assembly and from package assembling, said Service Component is used for the packaging and testing business; Said flow process assembly is used to realize branch and flow process control; Saidly be packaged with one group of Service Component and/or flow process assembly from package assembling, the multiplexing function after can realizing encapsulating.
6. like claim 4 or 5 described method of testings; It is characterized in that: said test case execution environment module is when carrying out said test case sequence; Through setting up each test suite of thread execution and/or script function; And be that said test suite and/or script function provide detecting information issuing interface and test result to submit interface to, said test suite and script function are shared the global variable in the test case sequence implementation.
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| CN103218292A (en) * | 2013-03-29 | 2013-07-24 | 北京控制工程研究所 | Automatic testing system for aerospace satellite-borne software |
| CN103218451A (en) * | 2013-04-27 | 2013-07-24 | 北京空间飞行器总体设计部 | Automatic spacecraft test data interpreting method |
| CN105988815A (en) * | 2015-03-04 | 2016-10-05 | 银联商务有限公司 | Business process development method and system |
| CN106294106A (en) * | 2015-05-27 | 2017-01-04 | 航天信息股份有限公司 | The method of testing of Web application system and device |
| WO2017017691A1 (en) * | 2015-07-27 | 2017-02-02 | Hewlett Packard Enterprise Development Lp | Testing computing devices |
| CN106547679A (en) * | 2015-09-17 | 2017-03-29 | 腾讯科技（深圳）有限公司 | The method and script management platform of script management |
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| CN106681921A (en) * | 2016-12-27 | 2017-05-17 | 腾讯科技（深圳）有限公司 | Method and device for achieving data parameterization |
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