CN105487975A - Self organization method for spacecraft test software processes - Google Patents
Self organization method for spacecraft test software processes Download PDFInfo
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- CN105487975A CN105487975A CN201510843472.8A CN201510843472A CN105487975A CN 105487975 A CN105487975 A CN 105487975A CN 201510843472 A CN201510843472 A CN 201510843472A CN 105487975 A CN105487975 A CN 105487975A
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- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F11/00—Error detection; Error correction; Monitoring
- G06F11/36—Preventing errors by testing or debugging software
- G06F11/3668—Software testing
- G06F11/3672—Test management
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- Computer Hardware Design (AREA)
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Abstract
The invention provides a self organization method for spacecraft test software processes. The self organization method comprises the following steps: (1) setting a configuration file: abstractly writing the correlativity of a test process and processes in the configuration file; (2) generating the test process: reading the configuration file when loading a core layer of the test software, and generating a process list according to the information of the configuration file; (3) generating a process panel: generating the process panel by an interface layer according to the process list; and (4) executing the test: a user operates the interface layer, and the interface layer dispatches an operation function of a corresponding operation process of the core layer according to the information of the process list and displays a dispatch result on the process panel. By adopting the self organization method provided by the invention, the interaction relation of the processes is realized, whether necessary conditions of a certain process are satisfied can be automatically judged, the processes can be defined in the configuration file, and the self organization of the processes can be realized by modifying the configuration file.
Description
Technical field
The present invention relates to a kind of spacecraft-testing software flow self-organizing method, belong to spacecraft-testing technology.
Background technology
Spacecraft changes frequent in the development stage, the adjustment comprising test event, flow process related to.If according to this redjustment and modification software, revise, verify that workload is large, and easily cause state of the art chaotic, not manageable problem.
Summary of the invention
For solving the problems of the technologies described above, the invention provides a kind of spacecraft-testing software flow self-organizing method, this spacecraft-testing software flow self-organizing method achieves the mutual interactively of flow process, whether the necessary condition of a certain flow process of energy automatic discrimination meets, and by amendment configuration file, can the self-organization of realization flow.
The present invention is achieved by the following technical programs.
A kind of spacecraft-testing software flow self-organizing method provided by the invention, comprises the steps:
1. configuration file is set: write in configuration file by abstract for the correlationship between testing process and each flow process;
2. testing process is generated: when the core layer of testing software loads, read configuration file, and according to the list of profile information product process;
3. product process panel: contact bed is according to flow process list product process panel;
4. perform test: user interface layer, contact bed calls the handling function of core layer respective operations flow process according to flow process list information, and will call result and be presented on flow process panel.
Described step 2. in, core layer is loaded as dynamic load.
Described step 4. in, the handling function that contact bed calls core layer calls for dynamically reading.
In described core layer, operation information corresponding for each testing process is stored as testing process node, and be whole process module by testing process ID list storage, read by reading whole process module information the testing process nodal information needing to call when flow process panel calls.
On-board test flow nodes executive condition is gone back in described whole process module, first judge when whole process module is read and calls whether testing process node executive condition is satisfied, the complete call when condition is satisfied again, returns miscue information in the unsatisfied situation of condition.
Whether beneficial effect of the present invention is: achieve the interactively that flow process is mutual, can the necessary condition of automatic discrimination a certain flow process meet, by flow definition in configuration file, by amendment configuration file, and can the self-organization of realization flow.
Accompanying drawing explanation
Fig. 1 is schematic flow sheet of the present invention;
Fig. 2 is the model schematic of flow process panel in Fig. 1.
Embodiment
Further describe technical scheme of the present invention below, but described in claimed scope is not limited to.
A kind of spacecraft-testing software flow self-organizing method as shown in Figure 1, comprises the steps:
1. configuration file is set: write in configuration file by abstract for the correlationship between testing process and each flow process;
2. testing process is generated: when the core layer of testing software loads, read configuration file, and according to the list of profile information product process;
3. product process panel: contact bed is according to flow process list product process panel;
4. perform test: user interface layer, contact bed calls the handling function of core layer respective operations flow process according to flow process list information, and will call result and be presented on flow process panel.
Described step 2. in, core layer is loaded as dynamic load.
Described step 4. in, the handling function that contact bed calls core layer calls for dynamically reading.
As shown in Figure 2, in described core layer, operation information corresponding for each testing process is stored as testing process node, and be whole process module by testing process ID list storage, read by reading whole process module information the testing process nodal information needing to call when flow process panel calls.
Specifically, On-board test flow nodes executive condition is gone back in described whole process module, first judge when whole process module is read and calls whether testing process node executive condition is satisfied, the complete call when condition is satisfied again, returns miscue information in the unsatisfied situation of condition.
Thus, testing process and correlationship thereof carry out abstract by the present invention, and are stored in configuration file.Read configuration file during test of missile Bootload, generate testing process by configuration file, testing process title is associated with concrete test operation, the self-organization of realization flow.
Claims (5)
1. a spacecraft-testing software flow self-organizing method, is characterized in that: comprise the steps:
1. configuration file is set: write in configuration file by abstract for the correlationship between testing process and each flow process;
2. testing process is generated: when the core layer of testing software loads, read configuration file, and according to the list of profile information product process;
3. product process panel: contact bed is according to flow process list product process panel;
4. perform test: user interface layer, contact bed calls the handling function of core layer respective operations flow process according to flow process list information, and will call result and be presented on flow process panel.
2. spacecraft-testing software flow self-organizing method as claimed in claim 1, is characterized in that: described step 2. in, core layer is loaded as dynamic load.
3. spacecraft-testing software flow self-organizing method as claimed in claim 1, is characterized in that: described step 4. in, the handling function that contact bed calls core layer calls for dynamically reading.
4. spacecraft-testing software flow self-organizing method as claimed in claim 1, it is characterized in that: in described core layer, operation information corresponding for each testing process is stored as testing process node, and be whole process module by testing process ID list storage, read by reading whole process module information the testing process nodal information needing to call when flow process panel calls.
5. spacecraft-testing software flow self-organizing method as claimed in claim 4, it is characterized in that: in described whole process module, go back On-board test flow nodes executive condition, first judge when whole process module is read and calls whether testing process node executive condition is satisfied, the complete call when condition is satisfied again, returns miscue information in the unsatisfied situation of condition.
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| Application Number | Priority Date | Filing Date | Title |
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| CN201510843472.8A CN105487975A (en) | 2015-11-27 | 2015-11-27 | Self organization method for spacecraft test software processes |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201510843472.8A CN105487975A (en) | 2015-11-27 | 2015-11-27 | Self organization method for spacecraft test software processes |
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| CN105487975A true CN105487975A (en) | 2016-04-13 |
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| CN201510843472.8A Pending CN105487975A (en) | 2015-11-27 | 2015-11-27 | Self organization method for spacecraft test software processes |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116501650A (en) * | 2023-06-27 | 2023-07-28 | 航天科工火箭技术有限公司 | Method, device and medium for executing carrier rocket measurement and control flow engine |
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2015
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Patent Citations (7)
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| CN101162426A (en) * | 2007-11-15 | 2008-04-16 | 中兴通讯股份有限公司 | Example design test method for testing based on data driving and automatically testing platform |
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Application publication date: 20160413 |