CN112905262A - Configuration method and device of aerospace measurement and control system - Google Patents
Configuration method and device of aerospace measurement and control system Download PDFInfo
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Abstract
The application provides a method and a device for configuring a space measurement and control system, comprising the following steps: generating a control software system configuration file according to configuration data of the aerospace measurement and control system; generating a display control page according to a pre-established page template and the control software system configuration file; checking the correctness of the content to be checked in the display control page according to the pre-established correctness checking configuration data; and configuring the task of the aerospace measurement and control system according to the configuration file of the control software system and the display control page after the correctness check is completed. According to the method and the device, the task of the space measurement and control system can be automatically configured by utilizing the human-computer interaction interface based on the page template and the configuration rule.
Description
Technical Field
The application relates to the field of aerospace measurement and control, in particular to a configuration method and device of an aerospace measurement and control system.
Background
The space measurement and control system takes charge of measuring and controlling spacecrafts such as spacecrafts and satellites and processing parameters of the spacecrafts. The space flight measurement and control system is used as a man-machine interaction window of space flight tasks and measurement and control personnel, is responsible for mission of task data display and control command sending, and provides a basis for monitoring, commanding, scheduling, analyzing, deciding and controlling of the participants in the tasks. The system is a necessary platform for timely mastering task execution conditions, implementing commands and decisions and sending control commands, and is the core concerned by the whole aerospace measurement and control system. With the rapid development of the aerospace industry in China, the aerospace task in the future has the characteristics of intensive measurement and control task, frequent change of demand and short preparation period; meanwhile, spaceflight measurement and control personnel have the characteristics of various posts, rich requirements and complex interaction.
In order to meet the task and application requirements, an extensible software platform facing data service and application requirements is designed on the basis of a software architecture of a platform and a plug-in the prior art, and a general interface control and unified description method of multitask data is provided, but the method has the following defects:
1. the display operation and control starting and running are bound by a large number of configurations, such as task configuration, target configuration, communication configuration, subscription configuration, interface configuration, station-measuring equipment configuration, global segment configuration, host configuration, communication configuration and the like, and the probability of errors of manually bound and compiled configuration data is high.
2. Binding information errors are easily caused in part of pages due to interface changes, misoperation and the like, such as bound interface numbers, parameter codes, parameter types and the like, and the errors are difficult to be found in a manual confirmation mode.
3. A large amount of static information such as task constants, theoretical values, opposite-checking names and the like are distributed in the page, and the page is not easy to maintain uniformly, such as the radius of the earth, the theoretical value of the parameters of the separation points, the theoretical value of the time of the arrow remote key events and the like. The static information is scattered in hundreds of pages, and if the pages need to be traversed one by one, the workload is large, and the situations of wrong change and missed change sometimes occur.
4. And the binding operation of partial pages is complex, the workload is large, and errors are easy to occur.
Disclosure of Invention
Aiming at the problems in the prior art, the application provides a method and a device for configuring an aerospace measurement and control system, which can automatically configure tasks of the aerospace measurement and control system by using a human-computer interaction interface based on a page template and a configuration rule.
In order to solve the technical problem, the application provides the following technical scheme:
in a first aspect, the present application provides a method for configuring an aerospace measurement and control system, including:
generating a control software system configuration file according to configuration data of the aerospace measurement and control system;
generating a display control page according to a pre-established page template and the control software system configuration file;
checking the correctness of the content to be checked in the display control page according to the pre-established correctness checking configuration data;
and configuring the task of the aerospace measurement and control system according to the configuration file of the control software system and the display control page after the correctness check is completed.
Further, the generating a display control page according to the pre-established page template and the control software system configuration file includes:
creating a page frame according to the acquired page layout information;
creating a plug-in entity according to the acquired plug-in information;
establishing an incidence relation between the display component and the data source according to the acquired interface binding information;
generating data processing information according to the calculation script information in the page template and the operation logic between the multi-source data in the configuration file;
generating a judgment condition of data validity according to the condition script information in the page template and the data source use constraint condition in the configuration file;
generating a corresponding relation between data and a display result according to the checking script information in the page template and the data checking description in the configuration file;
and generating the display control page according to the page frame, the plug-in entity, the incidence relation, the data processing information, the judgment condition and the corresponding relation.
Further, the checking the correctness of the content to be checked in the display control page according to the pre-established correctness checking configuration data includes:
generating a page data check rule according to the configuration file; the page data checking rule comprises a checking sequence and a correct answer;
and checking the correctness of the content to be checked in the display control page according to the checking sequence and the correct answer to obtain a checking result.
Further, the task of configuring the space measurement and control system according to the configuration file of the control software system and the display control page after the correctness check is completed includes:
performing task information management and user management according to the control software system configuration file;
generating a display control mode according to the display control page after the correctness check is finished;
and configuring the tasks of the aerospace measurement and control system according to the task information management result, the user management result and the display control mode.
In a second aspect, the present application provides an aerospace measurement and control system configuration device, including:
the configuration file generating unit is used for generating a configuration file of the control software system according to the configuration data of the aerospace measurement and control system;
the control page generating unit is used for generating a display control page according to a pre-established page template and the control software system configuration file;
the correctness checking unit is used for checking the correctness of the content to be checked in the display control page according to the preset correctness checking configuration data;
and the task configuration unit is used for configuring the tasks of the aerospace measurement and control system according to the configuration file of the control software system and the display control page after the correctness check is finished.
Further, the control page generating unit includes:
the page frame creating module is used for creating a page frame according to the acquired page layout information;
the plug-in entity creating module is used for creating a plug-in entity according to the acquired plug-in information;
the incidence relation establishing module is used for establishing the incidence relation between the display component and the data source according to the acquired interface binding information;
the data processing information generating module is used for generating data processing information according to the calculation script information in the page template and the operation logic between the multi-source data in the configuration file;
the judgment condition generation module is used for generating a judgment condition of data effectiveness according to the condition script information in the page template and the data source use constraint condition in the configuration file;
the corresponding relation determining module is used for generating the corresponding relation between the data and the display result according to the checking script information in the page template and the data checking description in the configuration file;
and the control page generating module is used for generating the display control page according to the page frame, the plug-in entity, the incidence relation, the data processing information, the judgment condition and the corresponding relation.
Further, the correctness checking unit includes:
the check rule generating module is used for generating a page data check rule according to the configuration file; the page data checking rule comprises a checking sequence and a correct answer;
and the checking result generating module is used for checking the correctness of the content to be checked in the display control page according to the checking sequence and the correct answer to obtain a checking result.
Further, the task configuration unit includes:
the information user management module is used for managing task information and managing users according to the configuration file of the control software system;
the control mode generating module is used for generating a display control mode according to the display control page after the correctness check is finished;
and the task configuration module is used for configuring the tasks of the aerospace measurement and control system according to the task information management result, the user management result and the display control mode.
In a third aspect, the present application provides an electronic device, which includes a memory, a processor, and a computer program stored in the memory and executable on the processor, where the processor implements the steps of the configuration method of the space measurement and control system when executing the program.
In a fourth aspect, the present application provides a computer-readable storage medium having stored thereon a computer program which, when being executed by a processor, carries out the steps of the method for configuring an aerospace measurement and control system.
Aiming at the problems in the prior art, the configuration method and the configuration device for the space flight measurement and control system can design a uniform configuration description mode for the space flight measurement and control system, and automatically generate a universal display and control page based on a uniform configuration file and a page template; the configuration of the human-computer interaction interface can be automatically completed according to the task description configuration file; the automatic checking of the page correctness can be efficiently and accurately finished according to the task and the interface configuration file; the task of the space measurement and control system can be automatically configured by utilizing a human-computer interaction interface based on a page template and a configuration rule.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to the drawings without creative efforts.
FIG. 1 is a flow chart of a configuration method of an aerospace measurement and control system in an embodiment of the present application;
FIG. 2 is a flowchart illustrating the generation of a display manipulation page in an embodiment of the present application;
FIG. 3 is a flow chart of correctness checking in the embodiment of the present application;
FIG. 4 is a flowchart of a task for configuring an aerospace measurement and control system in an embodiment of the present application;
FIG. 5 is a structural diagram of a configuration device of a space flight measurement and control system in an embodiment of the present application;
FIG. 6 is a block diagram of a control page generating unit in the embodiment of the present application;
FIG. 7 is a block diagram of a correctness checking unit in the embodiment of the present application;
FIG. 8 is a block diagram of a task configuration unit according to an embodiment of the present application;
fig. 9 is a schematic structural diagram of an electronic device in an embodiment of the present application;
FIG. 10 is a diagram illustrating an embodiment of generating a configuration file for a managed software system;
fig. 11 is one of schematic diagrams of generating a display manipulation page in an embodiment of the present application;
FIG. 12 is a second schematic diagram illustrating a generation of a display control page according to an embodiment of the present application;
FIG. 13 is a diagram illustrating a correctness check performed in an embodiment of the present application;
FIG. 14 is a schematic diagram illustrating a task of configuring an aerospace measurement and control system according to an embodiment of the present application;
fig. 15 is a second schematic diagram illustrating a task of configuring an aerospace measurement and control system in an embodiment of the present application.
Detailed Description
The technical solutions in the embodiments of the present application will be clearly and completely described below with reference to the drawings in the embodiments of the present application, and it is obvious that the described embodiments are only a part of the embodiments of the present application, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present application.
Referring to fig. 1, in order to automatically configure a task of an aerospace measurement and control system by using a human-computer interaction interface based on a page template and a configuration rule, the application provides a configuration method of the aerospace measurement and control system, which includes:
s101: generating a control software system configuration file according to configuration data of the aerospace measurement and control system;
it can be understood that, in order to solve the problems existing in the prior art, the application designs and implements a configuration method of an aerospace measurement and control system, which is implemented based on an aerospace measurement and control task human-computer interaction interface automatic configuration system (hereinafter, may be referred to as "system").
Referring to fig. 10, in generating the operating software system configuration file according to the configuration data of the space measurement and control system, a formatted system configuration file may be defined using extensible markup language (XML), which includes but is not limited to the following information: the system comprises a task configuration file, a target configuration file, a communication configuration file, a subscription configuration file, an interface configuration file, a station measuring equipment configuration file, a global section configuration file, a host configuration file, a communication configuration file, a B code configuration file, an uplink control configuration file and a remote measuring key event configuration file.
Based on a uniform binding database, the method can customize and generate a system configuration file group with a fixed format, and release the system configuration file group to a corresponding directory in the system according to needs, so that control software running on the system can be started and run, and support is provided for automatically generating pages and automatically completing measurement and control task general attribute configuration. The method can effectively solve the problem that errors are easy to occur when the configuration file is bound and compiled manually in the prior art.
Taking the configuration information of the station instrumentation as an example, the method described in the present application may derive the bound station instrumentation information from the uniformly bound database to form a system configuration file described in the following format, where the station instrumentation information includes: the system comprises a station name, a station code, a station type, a station code number, a station address coordinate, a station capability, a control capability, a support task code, a support target code and the like.
S102: generating a display control page according to a pre-established page template and the control software system configuration file;
it can be understood that the system designs a uniform system configuration description mode, and all system configuration files are exported from a uniformly bound database; and automatically generating a universal display control page based on the uniformly described system configuration file and the page template.
S103: checking the correctness of the content to be checked in the display control page according to the pre-established correctness checking configuration data;
s104: and configuring the task of the aerospace measurement and control system according to the configuration file of the control software system and the display control page after the correctness check is completed.
It can be understood that after the display control page is generated, the generated display control page can be further subjected to correctness check, so that the configuration of the human-computer interaction interface is completed, and the subsequent task of configuring the aerospace measurement and control system is facilitated.
As can be seen from the above description, the configuration method of the space flight measurement and control system provided by the application can design a uniform configuration description mode for the space flight measurement and control system, and automatically generate a universal display and control page based on a uniform configuration file and a page template; the configuration of the human-computer interaction interface can be automatically completed according to the task description configuration file; the automatic checking of the page correctness can be efficiently and accurately finished according to the task and the interface configuration file; the task of the space measurement and control system can be automatically configured by utilizing a human-computer interaction interface based on a page template and a configuration rule.
Referring to fig. 2, generating a display control page according to a pre-established page template and the control software system configuration file includes:
s201: creating a page frame according to the acquired page layout information;
it is to be understood that, referring to fig. 11 and 12, the page layout information includes content defining elements, layouts, color schemes, fonts, descriptions, and the like contained in the page.
S202: creating a plug-in entity according to the acquired plug-in information;
it is understood that, referring to fig. 11 and 12, the plug-in information includes proprietary attributes defining all plug-ins (e.g., whether the table supports the trace display, whether the curve supports the auto-refresh, whether the file supports the auto-download, etc.), the number of basic units in the plug-in (e.g., several rows and columns of the table, several curves, etc.), the signaling relationship and response logic between the plug-ins, etc.
S203: establishing an incidence relation between the display component and the data source according to the acquired interface binding information;
it is understood that, referring to fig. 11 and 12, the interface binding information includes data sources in the definition plug-in, and the method described herein can find and establish an association between the display component and the data sources.
S204: generating data processing information according to the calculation script information in the page template and the operation logic between the multi-source data in the configuration file;
it is to be understood that, referring to fig. 11 and 12, calculating script information includes describing the operational logic between data sources and implementing the secondary processing of multi-source data. The secondary processing is to use a script editing mode to complete mathematical (addition, subtraction, multiplication, division, trigonometric function, exponent, logarithm, and the like) and logical (and, or, not) operations between multi-source data, dimension conversion, state judgment, and the like of the multi-source data.
S205: generating a judgment condition of data validity according to the condition script information in the page template and the data source use constraint condition in the configuration file;
it is to be understood that, referring to fig. 11 and 12, the conditional script information includes usage constraints describing the data sources to implement the decision selection of data validity. For example, a user can set an effective mark in the spacecraft attitude data as a constraint condition, and when the effective mark is 1, the attitude data is analyzed and displayed in real time; when the valid flag is 0, the data is discarded and not processed.
S206: generating a corresponding relation between data and a display result according to the checking script information in the page template and the data checking description in the configuration file;
it is to be understood that, referring to fig. 11 and 12, the query script information includes a correspondence between description data and a display result. For example, the types of various types of data downloaded by the spacecraft are represented by numerical codes (such as 639587416, 231564752 and the like), and have no readability and understandability. For user convenience, the checking script can be defined as follows: 639587416 spacecraft attitude data, 231564752: and the software automatically completes the conversion from numbers to Chinese according to the checking script so as to provide interactive information which is convenient for a user to understand.
S207: and generating the display control page according to the page frame, the plug-in entity, the incidence relation, the data processing information, the judgment condition and the corresponding relation.
It is understood that, in an embodiment, the page layout information is static information in the template, the plug-in information, the interface binding information, the calculation script information, the condition script information, and the check script information are dynamic information in the template. When a page is generated using the page template, the static information remains unchanged and the dynamic information is dynamically created based on the configuration file. The page module can effectively avoid the problem that a large amount of constant information is difficult to maintain in a unified mode manually, and the problems that page binding operation is complex, workload is large and mistakes are easy to make are pertinently solved.
Specifically, the flow of page automatic generation is shown in fig. 12:
firstly, starting an automatic generation process of a display control page;
secondly, loading layout information in the page template, completing the setting of contents including elements, layout, color matching, fonts, description and the like in the page, and creating a page frame;
loading plug-in information in the page template, and creating all plug-in entities according to the description about the plug-in proprietary attribute, the number of basic units and the signal transmission relationship in the configuration file;
loading interface binding information in the page template, and establishing an association relation between the display component and the data source according to the description about the data interface in the configuration file;
loading the calculation script information in the page template, and finishing the definition of the secondary processing of the data according to the description of the mutual operation logic of the multi-source data in the configuration file;
loading condition script information in the page template, and finishing judgment, selection and definition of data effectiveness according to the description about the data source use constraint condition in the configuration file;
loading the checking script information in the page template, and finishing the definition of the corresponding relation between the data and the display result according to the description about data checking in the configuration file;
generating and storing a display control page;
ninthly, ending the automatic generation flow of the page.
In an embodiment, taking a "monitoring page for exchanging station information" as an example, when a page is automatically generated, first, the layout information in the template of the "monitoring page for exchanging station information" is loaded, and the setting of contents including elements, layout, color matching, fonts, description and the like in the page is completed (corresponding to the first step and the second step); secondly, loading plug-in information in the page template, and creating a control table plug-in entity (corresponding to the third step) by combining a configuration file of 'configuration information of the station measuring equipment'; thirdly, loading interface binding information in the page template, and establishing an association relation (corresponding to the fourth step) between the 'control form plug-in' and the 'station measurement information exchange state' by combining the 'interface information' configuration file; fourthly, loading the script information (corresponding to the fifth, sixth and seventh) such as calculation, condition, checking and the like in the page template; finally, a station survey information exchange monitoring page is generated and saved to a specified path (corresponding to the above item).
From the above description, the configuration method of the space flight measurement and control system provided by the application generates the display control page according to the pre-established page template and the configuration file of the control software system.
Referring to fig. 3, the correctness checking of the contents to be checked in the display manipulation page according to the pre-established correctness checking configuration data includes:
s301: generating a page data check rule according to the configuration file; the page data checking rule comprises a checking sequence and a correct answer;
s302: and checking the correctness of the content to be checked in the display control page according to the checking sequence and the correct answer to obtain a checking result.
It will be appreciated that in one embodiment, the correctness checking of the selected display manipulation page (or group of pages) needs to be done in accordance with the system configuration file. The method can efficiently and accurately complete the checking of the page correctness, and effectively solves the problem that the binding information in partial pages caused by interface change, misoperation and other reasons is difficult to identify through a traditional manual confirmation mode. Referring to fig. 13, the work flow is as follows:
firstly, starting an automatic page checking process;
selecting the content to be checked described by using the XML format by the user, wherein the step comprises the following steps: task codes, object codes, interface type codes, parameter names, parameter types, display formats, checking scripts, condition scripts, station survey information, B code format numbers, system binding constants and the like;
thirdly, generating page file checking rules according to the configuration file group, wherein the checking rules comprise checking sequence and 'correct answer';
selecting the page (or page group) to be detected by the user;
circularly carrying out matching type inspection and reporting the inspection condition in real time;
if the user interrupts the check or finishes all the page check work, generating a check report;
and seventhly, finishing the automatic page checking process.
In one embodiment, taking the example of "monitoring page for exchanging station information", when the page is automatically checked, the content to be checked described in XML format is selected first, including: task code, object code, interface type code, parameter name, parameter type, display format, checking script, condition script and the elements contained in the station-measuring information exchange monitoring page (corresponding to the first and the second); secondly, generating page file checking rules aiming at a configuration file group (comprising task configuration, target configuration, interface configuration and station testing equipment configuration) according to the page, wherein the page file checking rules comprise checking sequences (station testing binding sequences) and correct answers (corresponding to the third step and the fourth step); thirdly, circularly carrying out matching type check on the station-measuring information exchange monitoring page selected by the user, and reporting the check condition in real time (corresponding to the fifth step); finally generating a check report (corresponding to the sixth and the seventh).
From the above description, the configuration method of the space flight measurement and control system provided by the application can perform correctness check on the content to be checked in the display control page according to the preset correctness check configuration data.
Referring to fig. 4, the task of configuring the space measurement and control system according to the configuration file of the control software system and the display control page after the correctness check is completed includes:
s401: performing task information management and user management according to the configuration file of the control software system;
s402: generating a display control mode according to the display control page after the correctness check is completed;
s403: and configuring the tasks of the aerospace measurement and control system according to the task information management result, the user management result and the display control mode.
It can be understood that a large number of same or similar task configurations are included between different space flight measurement and control tasks and between different measurement and control targets of the same space flight measurement and control task. Such as a display control mode, a task information management unit, a user management unit, a page group and the like, wherein the page group comprises: the system comprises an information exchange page group, an uplink control page group, a remote measurement monitoring page group, a track control page group, a measurement and control plan page group, a measurement and control forecast page group, a measurement and control network page group, a key arc section (a transmitting section, a rendezvous and docking section, a power descending section, a return section and the like) page group, a public display page group and the like. The display control mode, the task information management unit, the user management unit and the like can be automatically generated according to the task configuration file. On the basis, according to the dependency relationship, the configuration and the deployment of the independent task units can be automatically completed, the loading operation of a human-computer interaction interface is provided, and the task joint debugging and the task execution are supported. The method can automatically complete the configuration and deployment of the task unit, and pointedly solve the problem that the existing page editing platform can not effectively reuse the existing page and bring a large amount of repetitive work to system users, thereby effectively improving the preparation efficiency of the space measurement and control task.
Specifically, referring to fig. 14 and 15, the structure of the system is as follows: firstly, a configuration file automatic generation module completes the generation of a software system configuration file group; secondly, a page automatic generation module generates a display control page group according to the configuration file and the page template; thirdly, the page correctness check is finished by the automatic page check module according to the configuration file and the content to be checked; and finally, completing the configuration and deployment of the independent task unit by a human-computer interaction interface automatic configuration module.
Taking the automatic configuration of the "station-finding information exchange monitoring page" as an example: after the space flight measurement and control task is issued, firstly, a configuration file automatic generation module completes generation of configuration files such as task configuration, target configuration, interface configuration, station measurement equipment configuration and the like; secondly, a page automatic generation module generates an observation station information exchange monitoring page according to the configuration file group and the observation station information exchange monitoring page template; thirdly, the page correctness check is finished by the automatic page check module according to the configuration file and the content to be checked; and finally, the human-computer interaction interface automatic configuration module completes the deployment of configuration files such as task configuration, target configuration, interface configuration, survey station equipment configuration and the like in the independent task unit and a survey station information exchange monitoring page.
From the above description, the configuration method of the space flight measurement and control system provided by the application can configure the task of the space flight measurement and control system according to the configuration file of the control software system and the display control page after the correctness check is completed.
In an embodiment, the automatic configuration system for the man-machine interaction interface of the space measurement and control task can be applied to a space station task and a star detection task. The system is provided with a uniformly bound database, a configuration file automatic generation plug-in and a display control client deployment page automatic check plug-in are deployed in the database, and by utilizing the plug-ins, the system can independently deploy a page automatic generation executable program and a man-machine interaction interface automatic configuration executable program, so that the one-click export of the man-machine interaction interface configuration file, the automatic generation of a basic display control page, the automatic check of a whole set of man-machine interaction pages and the efficient configuration and deployment of the man-machine interaction system executable independent task units are realized in the preparation process of the space measurement and control task. In the task preparation process of the space station measurement and control system, the time consumption for accurately generating the human-computer interaction interface configuration file is less than 5 minutes, the time consumption for automatically and accurately generating 102 basic display control pages is less than 2 minutes, the time consumption for automatically checking 316 complete sets of human-computer interaction pages is less than 5 minutes, and the time consumption for accurately configuring and deploying the task units of the space station of the human-computer interaction system is less than 1 minute. In the task preparation process of the mars detection and control system, the time for accurately generating the human-computer interaction interface configuration file is less than 4 minutes, the time for automatically and accurately generating 117 basic display control pages is less than 2 minutes, the time for automatically checking 345 complete sets of human-computer interaction pages is less than 6 minutes, and the time for accurately configuring and deploying task units of the space station of the human-computer interaction system is less than 1 minute. To sum up, the system can realize task configuration and preparation time of 10 minutes magnitude, obviously reduces task preparation workload, ensures the correctness of task configuration and deployment, and effectively improves the preparation efficiency of aerospace measurement and control tasks.
The method and the system on which the method is implemented have the following advantages:
1. the method is realized based on a uniformly bound database, can customize and generate a system configuration file group with a fixed format, and release the system configuration file group to a corresponding directory in the system according to needs, so that control software running on the system can be started and run, and support is provided for automatically generating pages and automatically completing measurement and control task general attribute configuration. The method can effectively solve the problem that errors are easy to occur when the configuration file is bound and compiled manually in the prior art.
2. The method described herein uses an extensible markup language (XML) to define a formatted page file template that enables dynamic creation of a page file (or group of files) in conjunction with a task configuration file. The problems of complex page binding operation, large workload and easy error are effectively solved; meanwhile, the problem that a large amount of static information (such as task constants, theoretical values, opposite searching names and the like) scattered in the page needs to be manually maintained is solved, and the page manufacturing efficiency is remarkably improved.
3. The method uses a dynamically generated page file check rule to perform matching check on the page (or page group) aiming at the content to be checked described by formatting. The method can effectively find the problem that binding information in partial pages has errors (such as binding interface number errors, parameter code number errors, parameter type errors and the like) due to interface change, misoperation and the like, and remarkably improves the reliability and safety of the whole system.
4. According to the method, the configuration and the deployment of the independent task units are automatically completed according to the dependency relationship by combining with the automatically generated page groups according to the task configuration file, the loading and the operation of a human-computer interaction interface are provided, a one-key task assembly scheme is realized, the workload of binding configuration, page making and task setting of operators in the task preparation process is greatly reduced, meanwhile, the risk caused by manual operation errors is effectively avoided, and the task preparation efficiency is greatly improved.
Based on the same inventive concept, the embodiment of the present application further provides a configuration device of an aerospace measurement and control system, which can be used for implementing the method described in the above embodiment, as described in the following embodiments. Because the principle of solving the problems of the configuration device of the aerospace measurement and control system is similar to that of the configuration method of the aerospace measurement and control system, the implementation of the configuration device of the aerospace measurement and control system can refer to the implementation of a software performance reference determination method, and repeated parts are not repeated. As used hereinafter, the term "unit" or "module" may be a combination of software and/or hardware that implements a predetermined function. While the system described in the embodiments below is preferably implemented in software, implementations in hardware, or a combination of software and hardware are also possible and contemplated.
Referring to fig. 5, in order to automatically configure a task of an aerospace measurement and control system by using a human-computer interaction interface based on a page template and a configuration rule, the application provides a configuration device of the aerospace measurement and control system, which includes:
the configuration file generating unit 501 is configured to generate a configuration file of the control software system according to configuration data of the space measurement and control system;
a control page generating unit 502, configured to generate a display control page according to a pre-established page template and the control software system configuration file;
the correctness checking unit 503 is configured to perform correctness checking on the to-be-checked content in the display control page according to the pre-established correctness checking configuration data;
and a task configuration unit 504, configured to configure a task of the space measurement and control system according to the configuration file of the control software system and the display control page after the correctness check is completed.
Referring to fig. 6, the manipulation page generation unit 502 includes:
a page frame creating module 601, configured to create a page frame according to the obtained page layout information;
a plug-in entity creating module 602, configured to create a plug-in entity according to the acquired plug-in information;
an association relationship establishing module 603, configured to establish an association relationship between the display component and the data source according to the obtained interface binding information;
a data processing information generating module 604, configured to generate data processing information according to computation script information in the page template and an operation logic between multi-source data in the configuration file;
a judgment condition generating module 605, configured to generate a judgment condition of data validity according to the condition script information in the page template and the data source usage constraint condition in the configuration file;
a correspondence determining module 606, configured to generate a correspondence between data and a display result according to the checking script information in the page template and the data checking description in the configuration file;
the control page generating module 607 is configured to generate the display control page according to the page frame, the plug-in entity, the association relationship, the data processing information, the determination condition, and the corresponding relationship.
Referring to fig. 7, the correctness checking unit 503 includes:
a check rule generating module 701, configured to generate a page data check rule according to the configuration file; the page data checking rule comprises a checking sequence and a correct answer;
and the inspection result generating module 702 is configured to perform correctness inspection on the to-be-inspected content in the display control page according to the inspection sequence and the correct answer to obtain an inspection result.
Referring to fig. 8, the task configuration unit 504 includes:
an information user management module 801, configured to perform task information management and user management according to the configuration file of the operating software system;
a control mode generating module 802, configured to generate a display control mode according to the display control page after the correctness check is completed;
and the task configuration module 803 is configured to configure a task of the space measurement and control system according to the task information management result, the user management result and the display control mode.
In order to automatically configure a task of an aerospace measurement and control system by using a human-computer interaction interface based on a page template and a configuration rule in a hardware level, the application provides an embodiment of an electronic device for implementing all or part of contents in a configuration method of the aerospace measurement and control system, and the electronic device specifically includes the following contents:
a Processor (Processor), a Memory (Memory), a communication Interface (Communications Interface) and a bus; the processor, the memory and the communication interface complete mutual communication through the bus; the communication interface is used for realizing information transmission between the configuration device of the aerospace measurement and control system and relevant equipment such as a core service system, a user terminal, a relevant database and the like; the logic controller may be a desktop computer, a tablet computer, a mobile terminal, and the like, but the embodiment is not limited thereto. In this embodiment, the logic controller may be implemented with reference to the embodiment of the space measurement and control system configuration method and the embodiment of the space measurement and control system configuration device in the embodiment, and the contents thereof are incorporated herein, and repeated descriptions are omitted.
It is understood that the user terminal may include a smart phone, a tablet electronic device, a network set-top box, a portable computer, a desktop computer, a Personal Digital Assistant (PDA), an in-vehicle device, a smart wearable device, and the like. Wherein, intelligence wearing equipment can include intelligent glasses, intelligent wrist-watch, intelligent bracelet etc..
In practical applications, part of the configuration method of the space flight measurement and control system may be executed on the electronic device side as described above, or all operations may be completed in the client device. The selection may be specifically performed according to the processing capability of the client device, the limitation of the user usage scenario, and the like. This is not a limitation of the present application. The client device may further include a processor if all operations are performed in the client device.
The client device may have a communication module (i.e., a communication unit), and may be in communication connection with a remote server to implement data transmission with the server. The server may include a server on the side of the task scheduling center, and in other implementation scenarios, the server may also include a server on an intermediate platform, for example, a server on a third-party server platform that is communicatively linked to the task scheduling center server. The server may include a single computer device, or may include a server cluster formed by a plurality of servers, or a server structure of a distributed apparatus.
Fig. 9 is a schematic block diagram of a system configuration of an electronic device 9600 according to an embodiment of the present application. As shown in fig. 9, the electronic device 9600 can include a central processor 9100 and a memory 9140; the memory 9140 is coupled to the central processor 9100. Notably, this fig. 9 is exemplary; other types of structures may also be used in addition to or in place of the structure to implement telecommunications or other functions.
In an embodiment, the functions of the configuration method of the space flight measurement and control system may be integrated into the central processor 9100. The central processor 9100 may be configured to control as follows:
s101: generating a control software system configuration file according to configuration data of the aerospace measurement and control system;
s102: generating a display control page according to a pre-established page template and the control software system configuration file;
s103: checking the correctness of the content to be checked in the display control page according to the pre-established correctness checking configuration data;
s104: and configuring the task of the aerospace measurement and control system according to the configuration file of the control software system and the display control page after the correctness check is completed.
As can be seen from the above description, the configuration method of the space flight measurement and control system provided by the application can design a uniform configuration description mode for the space flight measurement and control system, and automatically generate a universal display and control page based on a uniform configuration file and a page template; the configuration of the human-computer interaction interface can be automatically completed according to the task description configuration file; the automatic checking of the page correctness can be efficiently and accurately finished according to the task and the interface configuration file; the task of the space measurement and control system can be automatically configured by utilizing a human-computer interaction interface based on a page template and a configuration rule.
In another embodiment, the space flight measurement and control system configuration device may be configured separately from the central processor 9100, for example, the space flight measurement and control system configuration device of the data composite transmission device may be configured as a chip connected to the central processor 9100, and the function of the space flight measurement and control system configuration method is implemented by the control of the central processor.
As shown in fig. 9, the electronic device 9600 may further include: a communication module 9110, an input unit 9120, an audio processor 9130, a display 9160, and a power supply 9170. It is noted that the electronic device 9600 also does not necessarily include all of the components shown in fig. 9; in addition, the electronic device 9600 may further include components not shown in fig. 9, which may be referred to in the prior art.
As shown in fig. 9, a central processor 9100, sometimes referred to as a controller or operational control, can include a microprocessor or other processor device and/or logic device, which central processor 9100 receives input and controls the operation of the various components of the electronic device 9600.
The memory 9140 can be, for example, one or more of a buffer, a flash memory, a hard drive, a removable media, a volatile memory, a non-volatile memory, or other suitable device. The information relating to the failure may be stored, and a program for executing the information may be stored. And the central processing unit 9100 can execute the program stored in the memory 9140 to realize information storage or processing, or the like.
The input unit 9120 provides input to the central processor 9100. The input unit 9120 is, for example, a key or a touch input device. Power supply 9170 is used to provide power to electronic device 9600. The display 9160 is used for displaying display objects such as images and characters. The display may be, for example, an LCD display, but is not limited thereto.
The memory 9140 can be a solid state memory, e.g., Read Only Memory (ROM), Random Access Memory (RAM), a SIM card, or the like. There may also be a memory that holds information even when power is off, can be selectively erased, and is provided with more data, an example of which is sometimes called an EPROM or the like. The memory 9140 could also be some other type of device. Memory 9140 includes a buffer memory 9141 (sometimes referred to as a buffer). The memory 9140 may include an application/function storage portion 9142, the application/function storage portion 9142 being used for storing application programs and function programs or for executing a flow of operations of the electronic device 9600 by the central processor 9100.
The memory 9140 can also include a data store 9143, the data store 9143 being used to store data, such as contacts, digital data, pictures, sounds, and/or any other data used by an electronic device. The driver storage portion 9144 of the memory 9140 may include various drivers for the electronic device for communication functions and/or for performing other functions of the electronic device (e.g., messaging applications, contact book applications, etc.).
The communication module 9110 is a transmitter/receiver 9110 that transmits and receives signals via an antenna 9111. The communication module (transmitter/receiver) 9110 is coupled to the central processor 9100 to provide input signals and receive output signals, which may be the same as in the case of a conventional mobile communication terminal.
Based on different communication technologies, a plurality of communication modules 9110, such as a cellular network module, a bluetooth module, and/or a wireless lan module, may be disposed in the same electronic device. The communication module (transmitter/receiver) 9110 is also coupled to a speaker 9131 and a microphone 9132 via an audio processor 9130 to provide audio output via the speaker 9131 and receive audio input from the microphone 9132, thereby implementing ordinary telecommunication functions. The audio processor 9130 may include any suitable buffers, decoders, amplifiers and so forth. In addition, the audio processor 9130 is also coupled to the central processor 9100, thereby enabling recording locally through the microphone 9132 and enabling locally stored sounds to be played through the speaker 9131.
An embodiment of the present application further provides a computer-readable storage medium capable of implementing all steps in the configuration method of an aerospace measurement and control system with a server or a client as an execution subject in the foregoing embodiment, where the computer-readable storage medium stores a computer program, and when the computer program is executed by a processor, all steps of the configuration method of an aerospace measurement and control system with a server or a client as an execution subject in the foregoing embodiment are implemented, for example, when the processor executes the computer program, the following steps are implemented:
s101: generating a control software system configuration file according to configuration data of the aerospace measurement and control system;
s102: generating a display control page according to a pre-established page template and the control software system configuration file;
s103: checking the correctness of the content to be checked in the display control page according to the pre-established correctness checking configuration data;
s104: and configuring the task of the aerospace measurement and control system according to the configuration file of the control software system and the display control page after the correctness check is completed.
As can be seen from the above description, the configuration method of the space flight measurement and control system provided by the application can design a uniform configuration description mode for the space flight measurement and control system, and automatically generate a universal display and control page based on a uniform configuration file and a page template; the configuration of the human-computer interaction interface can be automatically completed according to the task description configuration file; the automatic checking of the page correctness can be efficiently and accurately finished according to the task and the interface configuration file; the task of the space measurement and control system can be automatically configured by utilizing a human-computer interaction interface based on a page template and a configuration rule.
As will be appreciated by one skilled in the art, embodiments of the present invention may be provided as a method, apparatus, or computer program product. Accordingly, the present invention may take the form of an entirely hardware embodiment, an entirely software embodiment or an embodiment combining software and hardware aspects. Furthermore, the present invention may take the form of a computer program product embodied on one or more computer-usable storage media (including, but not limited to, disk storage, CD-ROM, optical storage, and the like) having computer-usable program code embodied therein.
The present invention is described with reference to flowchart illustrations and/or block diagrams of methods, apparatus (devices), and computer program products according to embodiments of the invention. It will be understood that each flow and/or block of the flow diagrams and/or block diagrams, and combinations of flows and/or blocks in the flow diagrams and/or block diagrams, can be implemented by computer program instructions. These computer program instructions may be provided to a processor of a general purpose computer, special purpose computer, embedded processor, or other programmable data processing apparatus to produce a machine, such that the instructions, which execute via the processor of the computer or other programmable data processing apparatus, create means for implementing the functions specified in the flowchart flow or flows and/or block diagram block or blocks.
These computer program instructions may also be stored in a computer-readable memory that can direct a computer or other programmable data processing apparatus to function in a particular manner, such that the instructions stored in the computer-readable memory produce an article of manufacture including instruction means which implement the function specified in the flowchart flow or flows and/or block diagram block or blocks.
These computer program instructions may also be loaded onto a computer or other programmable data processing apparatus to cause a series of operational steps to be performed on the computer or other programmable apparatus to produce a computer implemented process such that the instructions which execute on the computer or other programmable apparatus provide steps for implementing the functions specified in the flowchart flow or flows and/or block diagram block or blocks.
The principle and the implementation mode of the invention are explained by applying specific embodiments in the invention, and the description of the embodiments is only used for helping to understand the method and the core idea of the invention; meanwhile, for a person skilled in the art, according to the idea of the present invention, there may be variations in the specific embodiments and the application scope, and in summary, the content of the present specification should not be construed as a limitation to the present invention.
Claims (10)
1. A configuration method of a space flight measurement and control system is characterized by comprising the following steps:
generating a control software system configuration file according to configuration data of the aerospace measurement and control system;
generating a display control page according to a pre-established page template and the control software system configuration file;
checking the correctness of the content to be checked in the display control page according to the pre-established correctness checking configuration data;
and configuring the task of the aerospace measurement and control system according to the configuration file of the control software system and the display control page after the correctness check is completed.
2. The method according to claim 1, wherein the generating a display control page according to a pre-established page template and the control software system configuration file comprises:
creating a page frame according to the acquired page layout information;
creating a plug-in entity according to the acquired plug-in information;
establishing an incidence relation between the display component and the data source according to the acquired interface binding information;
generating data processing information according to the calculation script information in the page template and the operation logic between the multi-source data in the configuration file;
generating a judgment condition of data validity according to the condition script information in the page template and the data source use constraint condition in the configuration file;
generating a corresponding relation between data and a display result according to the checking script information in the page template and the data checking description in the configuration file;
and generating the display control page according to the page frame, the plug-in entity, the incidence relation, the data processing information, the judgment condition and the corresponding relation.
3. The configuration method of the aerospace measurement and control system according to claim 1, wherein the checking the correctness of the to-be-detected content in the display control page according to the pre-established correctness checking configuration data comprises:
generating a page data check rule according to the configuration file; the page data checking rule comprises a checking sequence and a correct answer;
and checking the correctness of the content to be checked in the display control page according to the checking sequence and the correct answer to obtain a checking result.
4. The configuration method of the aerospace measurement and control system according to claim 1, wherein the task of configuring the aerospace measurement and control system according to the configuration file of the control software system and the display control page after the correctness check is completed comprises the following steps:
performing task information management and user management according to the control software system configuration file;
generating a display control mode according to the display control page after the correctness check is finished;
and configuring the tasks of the aerospace measurement and control system according to the task information management result, the user management result and the display control mode.
5. A configuration device of an aerospace measurement and control system is characterized by comprising:
the configuration file generating unit is used for generating a configuration file of the control software system according to the configuration data of the aerospace measurement and control system;
the control page generating unit is used for generating a display control page according to a pre-established page template and the control software system configuration file;
the correctness checking unit is used for checking the correctness of the content to be checked in the display control page according to the preset correctness checking configuration data;
and the task configuration unit is used for configuring the tasks of the aerospace measurement and control system according to the configuration file of the control software system and the display control page after the correctness check is finished.
6. The configuration device of the aerospace measurement and control system according to claim 5, wherein the control page generating unit includes:
the page frame creating module is used for creating a page frame according to the acquired page layout information;
the plug-in entity creating module is used for creating a plug-in entity according to the acquired plug-in information;
the incidence relation establishing module is used for establishing the incidence relation between the display component and the data source according to the acquired interface binding information;
the data processing information generating module is used for generating data processing information according to the calculation script information in the page template and the operation logic between the multi-source data in the configuration file;
the judgment condition generation module is used for generating a judgment condition of data effectiveness according to the condition script information in the page template and the data source use constraint condition in the configuration file;
the corresponding relation determining module is used for generating the corresponding relation between the data and the display result according to the checking script information in the page template and the data checking description in the configuration file;
and the control page generating module is used for generating the display control page according to the page frame, the plug-in entity, the incidence relation, the data processing information, the judgment condition and the corresponding relation.
7. The configuration device of an aerospace measurement and control system according to claim 5, wherein the correctness checking unit comprises:
the check rule generating module is used for generating a page data check rule according to the configuration file; the page data checking rule comprises a checking sequence and a correct answer;
and the checking result generating module is used for checking the correctness of the content to be checked in the display control page according to the checking sequence and the correct answer to obtain a checking result.
8. The configuration device of the aerospace measurement and control system of claim 5, wherein the task configuration unit comprises:
the information user management module is used for managing task information and managing users according to the configuration file of the control software system;
the control mode generating module is used for generating a display control mode according to the display control page after the correctness check is finished;
and the task configuration module is used for configuring the tasks of the aerospace measurement and control system according to the task information management result, the user management result and the display control mode.
9. An electronic device comprising a memory, a processor and a computer program stored on the memory and executable on the processor, wherein the steps of the method of configuring an aerospace measurement and control system according to any one of claims 1 to 4 are performed by the processor when the program is executed.
10. A computer-readable storage medium, on which a computer program is stored, which, when being executed by a processor, carries out the steps of the method for configuring an aerospace measurement and control system according to any one of claims 1 to 4.
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