CN112699035B - Multi-partition airborne application software association index testing method and device - Google Patents
Multi-partition airborne application software association index testing method and device Download PDFInfo
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Abstract
The invention belongs to the field of airborne software testing. The invention provides a multi-partition airborne application software association index testing method and device, which improve the testing efficiency of large-scale complex comprehensive multi-partition airborne application software. The method comprises the following steps: step (1) establishing a multi-partition airborne application software test information index according to test requirements; step (2), forming a configuration file of a test task as a test input according to test basic information, test items, test cases and test environments contained in the test information index; step (3), uniformly arranging and scheduling test tasks through a test engine to perform software test; step (4), updating the test result and the test problem in the test information index through the latest software test result; step (5) testing different partition software sub-configuration items through longitudinal testing inside the partition; and (6) completing configuration items or system tests of a multi-partition system level through multi-partition transverse tests.
Description
Technical Field
The invention belongs to the field of airborne software testing.
Background
The integrated modularization (Integrated Modular Avionics, IMA for short) of the airborne electronic system enables a set of airborne computer physical platform to bear multiple application fields, multiple systems and different task types, and becomes a necessary development trend. In order to solve the problem of fault isolation and information security caused by IMA, the existing high-security airborne operating systems all adopt a partition mechanism to provide inter-partition isolation and inter-partition communication capability, and typical partition operating systems, such as Wind River VxWorks AE653 and the proprietary property antenna system acouos 653 of China.
In contrast to conventional federated avionics architecture (FAA, federated Avionics Architectures), it is required that each avionics module must share a single set of computing resources and communication interfaces, whereas IMA architecture can run one or more avionics modules on a common computing resource. Under the development background of IMA and high-security partition onboard operating systems and the quality requirements of reliability, security and high standards, new challenges are presented to software testing.
At present, the test work of the multi-partition large-scale complex integrated system on-board software of IMA is mainly based on independent software configuration items under the FAA architecture, and a test method with pertinence and comprehensiveness is not designed aiming at the characteristics of the software according to a conventional test flow (such as unit test, component test, configuration item test and system test) and a conventional test method (such as equivalence class, boundary value and coverage rate, etc.), so that knowledge experience is difficult to solidify, and the test capability of the software is formed.
Disclosure of Invention
The invention aims to: the invention provides a multi-partition airborne application software association index testing method and device, which improve the testing efficiency of large-scale complex comprehensive multi-partition airborne application software.
The technical scheme is as follows:
a multi-partition airborne application software association index testing method comprises the following steps:
step (1) establishing a multi-partition airborne application software test information index according to test requirements;
step (2), forming a configuration file of a test task as a test input according to test basic information, test items, test cases and test environments contained in the test information index;
step (3), uniformly arranging and scheduling test tasks through a test engine to perform software test;
step (4), updating the test result and the test problem in the test information index through the latest software test result;
step (5) testing different partition software sub-configuration items through longitudinal testing inside the partition;
and (6) completing configuration items or system tests of a multi-partition system level through multi-partition transverse tests.
The multi-partition on-board application software test information index of the step (1) comprises the following steps:
testing basic information, including: software identification, software name, version to be tested, basic version, importance level, test level, coverage requirement, software and document to be tested and requirement items;
a unit/component test item comprising: software identification, test version, source file identification, function identification to be tested, function name to be tested, requirement tracking, test type and change type;
a configuration item/system test item comprising: software identification, test version, test item identification, test item name, requirement tracking, test type and change type;
a test environment, comprising: test environment name, test environment identification, application software to be tested, application software version to be tested, environment configuration-software item, environment configuration-hardware resource and test environment related document;
a test case, comprising: test item identification, test case name, test case description, design method, premise and constraint, test input, expected result, evaluation standard, and operation process;
test results, comprising: test item identification, test case-total number, test case-passing number, test case-failing number, test case-non-executing number, coverage, actual test result, problem identification;
testing problems, including: problem identification, software name, software version, discovery date, reporting date, problem provenance, test type, problem nature-category, problem nature-level, problem tracking, problem description, tester advice, development unit opinion, problem closure.
Problem nature-category includes: program/document/design/other issues;
problem nature-class includes: level 1/level 2/level 3/level 4/level 5.
The step (1) comprises:
(11) The testing basic information represents basic information of a software configuration item to be tested, and establishes association with other items through a software identifier and key fields of a version to be tested;
(12) Establishing a demand tracking relationship in the test process through the demand items;
(13) Identifying unit/component test or configuration item/system test by test level; wherein the object of the unit/component test is a function item in the software source code, and the object of the configuration item/system test item is an entire software configuration item;
(14) The test type is used for distinguishing dynamic test or static examination and analysis, and a test method of static examination and analysis is used for obtaining a test result, so that a test case does not need to be loaded;
(15) The test cases are closely related to the test environment, and the test method using the dynamic test needs to inject the test cases into the tested software through the test environment and acquire the test result.
The step (4) comprises: the test results record the execution of the test cases, as well as the results of static inspection and analysis, and all information for failed test items is recorded in the test questions.
The step (5) comprises: input testing, intra-partition task scheduling testing, application function testing and output testing of each partition application software.
The step (6) comprises: and performing inter-partition data communication test, multi-partition task scheduling test, external interface test and health monitoring and management test on the complete system test formed by the multiple partitions.
Further comprises:
and (7) manually customizing the concerned test record data based on the test information index according to the condition of software testing, so as to generate multiple test views of different test measurement angles.
A multi-partition on-board application software association index testing device, comprising:
the index establishing unit (1) establishes a multi-partition airborne application software test information index according to test requirements;
the configuration file unit (2) forms a configuration file of a test task as a test input according to the test basic information, the test items, the test cases and the test environments contained in the test information index;
the software testing unit (3) uniformly arranges and schedules testing tasks through the testing engine to perform software testing;
an updating unit (4) for updating the test result and the test problem in the test information index by the latest software test result;
the different partition software testing units (5) complete testing of different partition software sub-configuration items through longitudinal testing inside the partition;
a multi-partition system test unit (6) for completing multi-partition system level configuration items or system tests through multi-partition transverse tests.
The beneficial effects are that:
according to the invention, the multi-dimensional information association is carried out on the test requirements, the test case data sets (comprising units, components, configuration items and systems), the test environment configuration, the test problem sets of different versions of the software configuration items, the test method and the test process, the tracking and management of software defects are established, the test capability of multi-partition airborne application software is formed, the test efficiency of large-scale complex comprehensive multi-partition airborne application software can be remarkably improved, the test cost is reduced, and the management and control capability of the test process and the comprehensiveness of the test are improved.
Drawings
FIG. 1 is a schematic diagram of an on-board application software architecture of a multi-partition system according to the present invention.
FIG. 2 is a diagram illustrating the correlation index test according to the present invention.
FIG. 3 is a schematic diagram of the testing process of the present invention.
Fig. 4 is a schematic view of the structure of the device of the present invention.
Detailed Description
The multi-partition system onboard application software architecture is shown in fig. 1. The system consists of an application layer, a Partition operating system (Partition OS), a core operating system layer (CoreOS), a configurable component, a Module Support Layer (MSL), a processor module and an interface module. The Arinc653 library is implemented in the partitionOS, and basic resources and management are provided for the running of the application task. CoreOS provides a basic environment for partition operation, including loading, booting, reconfiguration of partitions, partition scheduling and communication, and the like.
The application layer is composed of multiple partitions, and functions of various professional application fields are realized by application software of different partitions. The partition technology well realizes space-time isolation of the system, the partitions are not mutually influenced and independently run, and the running of the partitions is required to meet the requirements of time and space. Direct communication between partitions is not allowed and must be communicated through ports controlled by the operating system.
The invention carries out information association on key fields in basic test information, test items (including unit/component test, configuration item/system test), test environment, test cases and test results, and forms a test knowledge base, as shown in figure 2. In the actual software testing process, by loading the information related to each other, test item management, test quality management, software defect and test problem tracking, unit/component/configuration item/system level testing can be realized.
The composition elements of the association index test mainly consist of the following data sets, including:
testing basic information, including: software identification, software name, version to be tested, basic version, importance level, test level, coverage requirement, software to be tested, document and requirement item.
A unit/component test item comprising: software identification, test version, source file identification, function identification to be tested, function name to be tested, requirement tracking, test type and change type.
A configuration item/system test item comprising: software identification, test version, test item identification, test item name, requirement tracking, test type, change type.
A test environment, comprising: test environment name, test environment identification, application software to be tested, application software version to be tested, environment configuration-software item, environment configuration-hardware resource and test environment related document.
A test case, comprising: test item identification, test case name, test case description, design method, premise and constraint, test input, expected result, evaluation criteria, and operation process.
Test results, comprising: test item identification, test case-total number, test case-pass number, test case-fail number, test case-un-executed number, coverage, actual test result, problem identification.
Testing problems, including: problem identification, software name, software version, discovery date, reporting date, problem provenance, test type, problem nature-category (program problem/document problem/design problem/other problem), problem nature-level (level 1/level 2/level 3/level 4/level 5), problem tracking, problem description, tester advice, development unit opinion, problem closure.
The association method comprises the following steps:
the test basic information represents basic information of a software configuration item to be tested, and the software identification and the key field of the version to be tested are associated with other items. The requirement items are used for establishing a requirement tracking relation in the test process. By test level identification unit/component testing or configuration item/system testing.
Determining test items by test level, comprising: unit/component testing and configuration item/system testing, the test item covers the test requirements entirely. Wherein the object of the unit/component test is a function item in the software source code and the object of the configuration item/system test item is the entire software configuration item. And the test type is used for distinguishing dynamic test or static examination and analysis, and a test method of static examination and analysis is used for obtaining a test result, so that a test case does not need to be loaded.
The test cases are closely related to the test environment, and the test method using the dynamic test needs to inject the test cases into the tested software through the test environment and acquire the test result.
The test results record the execution of the test cases, as well as the results of static inspection and analysis, and all information for failed test items is recorded in the test questions.
The complete test process is based on test information retrieval, and the test information index comprises: the test system comprises a test requirement set, a test case, a test environment configuration and a test result, wherein the test requirement set comprises: test planning, test quality requirements, software development documents, and software code. The testing process covers the unit, component, configuration item and system testing requirements entirely. The complete test process based on the comprehensive index of test information is shown in fig. 3, and comprises the following steps:
generating a test information set, a test project set, a test case set and a test environment set according to the test requirement set, and forming a configuration file of a test task as test input;
uniformly arranging and scheduling test tasks through a test engine, analyzing test results, and updating test result data in a test information index through test result analysis data;
testing of different partition software sub-configuration items is completed through longitudinal testing inside the partition. The input test, the task scheduling test, the application function test and the output test contained in the intra-partition test belong to the unit or component test;
the configuration items or system tests of the multi-partition system level are completed through multi-partition transverse tests, wherein main test items comprise: inter-partition data communication test, multi-partition task scheduling test, external interface test and health monitoring and management test;
according to the software test situation, based on the test information index, a user can customize the concerned test record data so as to generate multiple test views with different test measurement angles.
Example 1
A multi-partition airborne application software association index testing method comprises the following steps:
step (1) establishing a multi-partition airborne application software test information index according to test requirements;
step (2), forming a configuration file of a test task as a test input according to test basic information, test items, test cases and test environments contained in the test information index;
step (3), uniformly arranging and scheduling test tasks through a test engine to perform software test;
step (4), updating the test result and the test problem in the test information index through the latest software test result;
step (5) testing different partition software sub-configuration items through longitudinal testing inside the partition;
and (6) completing configuration items or system tests of a multi-partition system level through multi-partition transverse tests.
The multi-partition on-board application software test information index of the step (1) comprises the following steps:
the step (1) comprises:
(11) The testing basic information represents basic information of a software configuration item to be tested, and establishes association with other items through a software identifier and key fields of a version to be tested;
(12) Establishing a demand tracking relationship in the test process through the demand items;
(13) Identifying unit/component test or configuration item/system test by test level; wherein the object of the unit/component test is a function item in the software source code, and the object of the configuration item/system test item is an entire software configuration item;
(14) The test type is used for distinguishing dynamic test or static examination and analysis, and a test method of static examination and analysis is used for obtaining a test result, so that a test case does not need to be loaded;
(15) The test cases are closely related to the test environment, and the test method using the dynamic test needs to inject the test cases into the tested software through the test environment and acquire the test result.
The step (4) comprises: the test results record the execution of the test cases, as well as the results of static inspection and analysis, and all information for failed test items is recorded in the test questions.
The step (5) comprises: input testing, intra-partition task scheduling testing, application function testing and output testing of each partition application software.
The step (6) comprises: and performing inter-partition data communication test, multi-partition task scheduling test, external interface test and health monitoring and management test on the complete system test formed by the multiple partitions.
And (7) manually customizing the concerned test record data based on the test information index according to the condition of software testing, so as to generate multiple test views of different test measurement angles.
A corresponding multi-partition airborne application software association index testing device, as shown in figure 4, comprises:
the index establishing unit 1 establishes a multi-partition airborne application software test information index according to test requirements;
a configuration file unit 2, which forms a configuration file of a test task as a test input according to the test basic information, the test items, the test cases and the test environment contained in the test information index;
the software testing unit 3 uniformly arranges and schedules testing tasks through a testing engine to perform software testing;
an updating unit 4 for updating the test result and the test problem in the test information index by the latest software test result;
the different partition software testing unit 5 is used for completing the testing of different partition software sub-configuration items through the longitudinal testing in the partition; the specific flow is seen in a test method of multi-partition airborne software (patent application number: 201911363531.6).
The multi-partition system test unit 6 completes the configuration item or the system test of the multi-partition system level through multi-partition transverse test. A testing method of multi-partition on-board software (patent application number: 201911363531.6).
Example 2
Taking an electromechanical core processor (EMP) of an Electromechanical Management System (EMS) of a type of aircraft as an example. The EMP on-board software is multi-partition on-board application software based on Wind River VxWorks AE653 operating system. The method mainly comprises the following steps: 1. data acquisition and state monitoring are carried out on the electromechanical control system; 2. comprehensively processing fault alarms of an electromechanical control system; 3, executing control and management functions of part of electromechanical control systems; 4, managing data transmission between electromechanical control systems; 5. displaying configuration information, current state, parameters, prompt, alarm information and other contents of each electromechanical control system on an avionics system display by utilizing a virtual instrument technology; 6. and the electromechanical control system has the functions of storing and displaying fault data, BIT and other maintenance and management.
The application function of the EMP is jointly completed by the following multi-partition onboard application software:
bus partition application software;
fuel partition application software;
the hydraulic partition should be software;
the cabin door partitioning application software,
fireproof partition application software;
power partition application software;
the partition application software is controlled in a ring manner;
landing gear partition software;
using electrical partition application software;
partition application software is maintained.
For EMP on-board application software, the invention is implemented by the following two steps:
step one: the association information shown in fig. 2 is established for each of the 10 partitioned application software of the EMP on-board application software, and is used for independent testing of each partitioned application software.
Step two: the characteristics of EMP airborne application software are analyzed, and 10 partition application software composed of the EMP airborne application software have some common test requirements, and mainly comprise: heartbeat test, 2 redundancy voting test, 3 redundancy voting test, 4 redundancy voting test, bus health test, inter-partition communication test, etc. The associated information of each requirement shown in fig. 2 is established for the common test requirements, and the information can effectively improve the test item multiplexing capability of the multi-partition software.
Claims (8)
1. The multi-partition airborne application software association index testing method is characterized by comprising the following steps of:
step (1) establishing a multi-partition airborne application software test information index according to test requirements;
step (2), forming a configuration file of a test task as a test input according to test basic information, test items, test cases and test environments contained in the test information index;
step (3), uniformly arranging and scheduling test tasks through a test engine to perform software test;
step (4), updating the test result and the test problem in the test information index through the latest software test result;
step (5) testing different partition software sub-configuration items through longitudinal testing inside the partition;
step (6) completing configuration items or system tests of a multi-partition system level through multi-partition transverse tests;
the step (1) comprises:
(11) The testing basic information represents basic information of a software configuration item to be tested, and establishes association with other items through a software identifier and key fields of a version to be tested;
(12) Establishing a demand tracking relationship in the test process through the demand items;
(13) Identifying unit/component test or configuration item/system test by test level; wherein the object of the unit/component test is a function item in the software source code, and the object of the configuration item/system test item is an entire software configuration item;
(14) The test type is used for distinguishing dynamic test or static examination and analysis, and a test method of static examination and analysis is used for obtaining a test result, so that a test case does not need to be loaded;
(15) The test cases are closely related to the test environment, and the test method using the dynamic test needs to inject the test cases into the tested software through the test environment and acquire the test result.
2. The multi-partition on-board application software association index test method of claim 1, wherein the multi-partition on-board application software test information index of step (1) comprises:
testing basic information, including: software identification, software name, version to be tested, basic version, importance level, test level, coverage requirement, software and document to be tested and requirement items;
a unit/component test item comprising: software identification, test version, source file identification, function identification to be tested, function name to be tested, requirement tracking, test type and change type;
a configuration item/system test item comprising: software identification, test version, test item identification, test item name, requirement tracking, test type and change type;
a test environment, comprising: test environment name, test environment identification, application software to be tested, application software version to be tested, environment configuration-software item, environment configuration-hardware resource and test environment related document;
a test case, comprising: test item identification, test case name, test case description, design method, premise and constraint, test input, expected result, evaluation standard, and operation process;
test results, comprising: test item identification, test case-total number, test case-passing number, test case-failing number, test case-non-executing number, coverage, actual test result, problem identification;
testing problems, including: problem identification, software name, software version, discovery date, reporting date, problem provenance, test type, problem nature-category, problem nature-level, problem tracking, problem description, tester advice, development unit opinion, problem closure.
3. A multi-partition on-board application software association index test method as claimed in claim 2,
problem nature-category includes: program/document/design/other issues;
problem nature-class includes: level 1/level 2/level 3/level 4/level 5.
4. The multi-partition on-board application software association index test method of claim 1, wherein step (4) comprises: the test results record the execution of the test cases, as well as the results of static inspection and analysis, and all information for failed test items is recorded in the test questions.
5. The multi-partition on-board application software association index test method of claim 1, wherein step (5) comprises: input testing, intra-partition task scheduling testing, application function testing and output testing of each partition application software.
6. The multi-partition on-board application software association index test method of claim 1, wherein step (6) comprises: and performing inter-partition data communication test, multi-partition task scheduling test, external interface test and health monitoring and management test on the complete system test formed by the multiple partitions.
7. The multi-partition on-board application software association index test method of claim 1, further comprising:
and (7) manually customizing the concerned test record data based on the test information index according to the condition of software testing, so as to generate multiple test views of different test measurement angles.
8. A multi-partition on-board application software association index testing device, comprising:
the index establishing unit (1) establishes a multi-partition airborne application software test information index according to test requirements; the process for establishing the multi-partition airborne application software test information index according to the test requirement comprises the following steps: (11) The testing basic information represents basic information of a software configuration item to be tested, and establishes association with other items through a software identifier and key fields of a version to be tested; (12) Establishing a demand tracking relationship in the test process through the demand items; (13) Identifying unit/component test or configuration item/system test by test level; wherein the object of the unit/component test is a function item in the software source code, and the object of the configuration item/system test item is an entire software configuration item; (14) The test type is used for distinguishing dynamic test or static examination and analysis, and a test method of static examination and analysis is used for obtaining a test result, so that a test case does not need to be loaded; (15) The test cases are closely related to the test environment, and the test method using dynamic test needs to inject the test cases into the tested software through the test environment and acquire the test result;
the configuration file unit (2) forms a configuration file of a test task as a test input according to the test basic information, the test items, the test cases and the test environments contained in the test information index;
the software testing unit (3) uniformly arranges and schedules testing tasks through the testing engine to perform software testing;
an updating unit (4) for updating the test result and the test problem in the test information index by the latest software test result;
the different partition software testing units (5) complete testing of different partition software sub-configuration items through longitudinal testing inside the partition;
a multi-partition system test unit (6) for completing multi-partition system level configuration items or system tests through multi-partition transverse tests.
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Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6332211B1 (en) * | 1998-12-28 | 2001-12-18 | International Business Machines Corporation | System and method for developing test cases using a test object library |
| WO2013087982A1 (en) * | 2011-12-16 | 2013-06-20 | Codenomicon Oy | Network- based testing and pubblication service |
| CN104978258A (en) * | 2014-04-01 | 2015-10-14 | 中国银联股份有限公司 | Software automation test method and system |
| CN108415845A (en) * | 2018-03-28 | 2018-08-17 | 北京达佳互联信息技术有限公司 | AB tests computational methods, device and the server of system index confidence interval |
| CN110083337A (en) * | 2019-04-03 | 2019-08-02 | 江苏梦立渊软件技术有限公司 | A kind of software development optimization method |
| GB201910775D0 (en) * | 2018-09-14 | 2019-09-11 | Sino Ic Tech Co Ltd | No Details |
| CN111124927A (en) * | 2019-12-25 | 2020-05-08 | 中国航空工业集团公司西安飞机设计研究所 | Test method of multi-partition airborne software |
| CN111767225A (en) * | 2020-06-29 | 2020-10-13 | 厦门力含信息技术服务有限公司 | Third-party software testing system and method in cloud computing environment |
-
2020
- 2020-12-29 CN CN202011612686.1A patent/CN112699035B/en active Active
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6332211B1 (en) * | 1998-12-28 | 2001-12-18 | International Business Machines Corporation | System and method for developing test cases using a test object library |
| WO2013087982A1 (en) * | 2011-12-16 | 2013-06-20 | Codenomicon Oy | Network- based testing and pubblication service |
| CN104978258A (en) * | 2014-04-01 | 2015-10-14 | 中国银联股份有限公司 | Software automation test method and system |
| CN108415845A (en) * | 2018-03-28 | 2018-08-17 | 北京达佳互联信息技术有限公司 | AB tests computational methods, device and the server of system index confidence interval |
| GB201910775D0 (en) * | 2018-09-14 | 2019-09-11 | Sino Ic Tech Co Ltd | No Details |
| CN110083337A (en) * | 2019-04-03 | 2019-08-02 | 江苏梦立渊软件技术有限公司 | A kind of software development optimization method |
| CN111124927A (en) * | 2019-12-25 | 2020-05-08 | 中国航空工业集团公司西安飞机设计研究所 | Test method of multi-partition airborne software |
| CN111767225A (en) * | 2020-06-29 | 2020-10-13 | 厦门力含信息技术服务有限公司 | Third-party software testing system and method in cloud computing environment |
Non-Patent Citations (3)
| Title |
|---|
| 基于Agent的智能化元搜索引擎个性化机制;李青山等;《中国科学:信息科学》;20150520(第05期);全文 * |
| 基于预测的输变电工程元数据分级索引算法;孙小虎;《计算机工程与设计》;20191130;全文 * |
| 无人机飞控软件测试方法研究;王泉等;《航空计算技术》;20080315(第02期);全文 * |
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