Integrated commanding and monitoring system for intelligent launching site

Abstract

The invention discloses an integrated commanding and monitoring system for an intelligent launching site, and aims to construct a highly-automatic integrated intelligent monitoring system for construction requirements of the intelligent launching site so as to improve the testing and launching efficiency, safety and reliability of a spaceflight launching site. The research blank can be filled up through the patent. According to the scheme provided by the invention, new technologies are respectively provided aiming at the three prominent problems, so that theoretical support and practical guidance are provided for the development of the intelligent launching site in the future; in the future, along with the emergence of more innovative technologies and ideas, the technical route and scheme of the intelligent launching site are continuously improved on the basis of the patent, and a wider development prospect is achieved.

Description

Technical Field

[0001] The present invention relates to the technical field of space launch site command information, and in particular to an integrated command and monitoring system for a smart launch site. Background Art

[0002] With the rapid development of the global aerospace industry, the demand for intelligent management of launch sites is growing. At present, the focus is mainly on building an information system to manage the test data of traditional launch sites and empowering traditional launch sites with digital twin technology. The main problems are as follows: lack of virtualized resource sharing technology, the amount of data accumulated by the launch site during launch and testing is increasing, reaching a massive amount, which causes the monitoring, processing, and query systems of traditional launch sites to run slowly or even be unable to process; lack of data-driven monitoring technology, the solidified time drive has been difficult to adapt to the display requirements of multiple models of rockets and different launch processes, and the evolution of automation has made the update of the process often accompanied by complex and diverse process criteria and instruction actions; lack of configuration interface interactive customization technology, the fixed interface parameter display requirements brought by traditional fixed task requirements have been difficult to meet the new requirements of flexible customization of multi-model switching, and with the improvement of informationization and monitoring levels, the number of monitored parameters has increased day by day, which has led to a sharp increase in the demand for binding the types of parameters displayed on the interface, and a convenient and draggable interface parameter binding mode is urgently needed to support the display requirements of a large number of parameters and diverse parameters. Summary of the invention

[0003] The present invention provides an integrated command and monitoring system for a smart launch site, with the aim of constructing a highly automated integrated intelligent monitoring system for the construction needs of a smart launch site, so as to improve the measurement and launch efficiency and safety and reliability of the space launch site. This patent will fill the above research gaps. The solution provided by the present invention proposes new technologies for the above three outstanding problems, in order to provide theoretical support and practical guidance for the development of future smart launch sites; in the future, with the emergence of more innovative technologies and concepts, smart launch sites will continue to improve their technical routes and solutions based on this patent, ushering in a broader development prospect.

[0004] First, an integrated command and monitoring system for a smart launch site is provided, including:

[0005] Interface forwarding module, responsible for receiving and forwarding launch site system data;

[0006] The data processing and storage middle platform is responsible for storing and managing the launch site system data and providing a unified data calling interface for business applications;

[0007] The BS business module controls user access to the main business modules according to user permissions through a unified integrated portal, including an integrated command and display module, a health management module, an integrated operation and maintenance module, a launch mission control module, and a launch mission system control platform. It interacts with the data processing and storage middle platform to obtain data resources, presents them to users through a unified integrated portal, and realizes module definition seats;

[0008] Special business modules, including the test, launch, command and display modules, are independent of the management and control of the unified integrated portal.

[0009] In combination with the first aspect, in certain implementations of the first aspect, the launch site data elements are divided into frequent acquisition data and fixed input data according to the acquisition form, the frequent acquisition data is time series data, and the fixed input data includes structured data and unstructured data; the data processing and storage middle platform design database includes:

[0010] Cache database to achieve memory storage of high-frequency call data and improve access efficiency;

[0011] Historical database, to realize the storage and management of time series data;

[0012] Metadatabase, which uses relational database to store structured data;

[0013] File system, which enables storage of unstructured data.

[0014] In conjunction with the first aspect, in certain implementations of the first aspect, the main body of the launch site data element is time series data, which is recorded in the form of table-codes, and the table number division is based on the GJB 7337 protocol file. The data includes data of the rocket system, satellite system, refueling system, and launch pad system in units of test tasks, and also includes water, electricity, and meteorological data;

[0015] Among them, the table numbers are classified according to the model-issue-test task level and stored according to table-code; the data corresponding to the table numbers are stored according to table-code;

[0016] One of the properties of data storage is whether the data is stored on site in units of model-launch-test task. It is set by operating the relational database through the data processing and storage middle platform.

[0017] In conjunction with the first aspect, in certain implementations of the first aspect, the system implements multi-task parallel command and monitoring to meet the following requirements:

[0018] The interface forwarding module serves as the interface for the integrated command and monitoring system to interact with the outside world. One set of interface forwarding modules corresponds to one test task. When the interface forwarding module is started, it interacts with the data processing and storage center to obtain the model-launch-test task identifier of the data it receives. After receiving the data, the identifier is assigned to the data and sent to the data processing and storage center to realize the data storage of the test task. Multiple sets of interface forwarding modules are replicated and deployed through the container cloud platform or virtual cloud platform, one set of interface forwarding modules is used to receive data that is not related to the launch site and the model-launch-test task, and other interface forwarding modules receive data of different test tasks respectively. The model-launch-test task corresponding to each interface forwarding module is edited through the data processing and storage center operation database.

[0019] When users use the unified integrated portal module to access the business module, they select Model-Times-Test Task after logging in to access the corresponding test task information;

[0020] Special business applications are divided into two categories; one is to obtain data directly through the interface forwarding module, and soft-bind it to the specific interface forwarding; the other is to obtain data through the data processing and storage middle platform. After startup, select model-issue-test task, and access the unified interface of the data processing and storage middle platform to obtain the corresponding data.

[0021] In conjunction with the first aspect, in some implementations of the first aspect, the system includes:

[0022] Parameter attribute maintenance: used to maintain the hierarchical relationship and content of model-issue-system-parameter table-parameter definition, providing support for the system to receive, process and display data of different test tasks;

[0023] Test task maintenance: used to add, delete, modify, check and associate models, releases, test tasks and process time periods. At the same time, configure the corresponding interface forwarding module under the test task to build the association relationship between model-release-test task-interface forwarding module;

[0024] User-facing interface: provides one-, two-, and four-screen display templates. On each screen, select display controls for data tables, curve graphs, and timing diagrams. After selecting a control, select the parameter to be monitored according to the parameter table-code.

[0025] Interface for large-screen display: Provides a canvas and display controls for data tables, instruction append tables, curve charts, indicator lights, dashboards, process charts, text, and decorations. Freely drag, drag, and zoom on the canvas. After the display controls are bound to data sets, a large-screen page for data monitoring is constructed.

[0026] Data interpretation: parameter interpretation method, judgment criteria, judgment stage, fault level, alarm information, and related plans.

[0027] In conjunction with the first aspect, in certain implementations of the first aspect, the process of the system controlling the launch site mission satisfies:

[0028] The launch site mission control is divided according to the time scale, including the launch site refueling and launch mission process control and the launch site full-process mission control. The launch site refueling and launch mission process control is aimed at status monitoring and command at different stages of the refueling and launch process, which is test data monitoring based on the test process. The launch site full-process mission control includes various tests and transportation of rockets and satellites after entering the site, and is mainly a process orchestration based on launch site resources.

[0029] In conjunction with the first aspect, in certain implementations of the first aspect, the launch site refueling launch mission process control includes:

[0030] Information display automation: The information display of the large screen includes the test process screen, parameter element screen and camera video based on the module interface; for the module interface screen, the system large screen display interface is based on the configured process period. Under each configured process period, several large screen display interfaces are set. These interfaces support two display logics: patrol display and parameter trigger display. The process stage is controlled by process instructions, and the test instructions under the process stage control page display to realize data-driven module large screen interface display content; the overall display of the large screen is used as a template, and the parameter trigger switching and patrol display mode are realized by splicing the controller and the supporting modules. The two data-driven logics are nested to realize the automatic display script arrangement of the launch site large screen;

[0031] Automated abnormal diagnosis: Based on the parameter interpretation method, judgment criteria, judgment stage, fault level, alarm information, and associated plans, the system can realize automatic background interpretation, alarm, and auxiliary decision-making push based on the test stage;

[0032] Process-driven automation: The test and launch command display module issues process instructions and supports automatic mode, compressed mode and manual mode. In automatic mode, the corresponding process instructions are automatically issued based on the launch countdown. In compressed mode, after manually clicking the process instruction button, the estimated ignition time and countdown correspond to the process instruction. In manual mode, after manually clicking the process instruction button, only the process instruction is issued without changing the estimated ignition time and countdown.

[0033] In conjunction with the first aspect, in certain implementations of the first aspect, the full-process mission control of the launch site includes:

[0034] Mission process node configuration: According to different models, through configuration, select the process category, set the preconditions for process execution and the functions used for calculation, the output instructions for process execution, adjust the process sequence, complete the process settings and output the process file, drive the completion of the mission node based on the launch site test data, and provide timing requirements for intelligent test and automatic test;

[0035] Launch process control: Execute the full process scheduling from mission entry to mission launch, and intelligently arrange the parallel work progress of multiple tasks according to the window dates and key nodes of different models. It supports scheduling based on the entry date and scheduling based on the launch date, and supports normal launch processes, expedited launch processes, and emergency launch processes. It generates and pushes electronic work scheduling sheets every day.

[0036] Launch resource control: Based on the launch process, launch resources are automatically arranged, including test personnel, ground support, workshops, equipment, vehicles, canteen support, and fire protection, and personnel in place, work conditions, warehouse materials and other resources are uniformly allocated and managed;

[0037] Launch window control: Automatically select the transition and launch window by comprehensively evaluating the environment, weather, and mission requirements. When the factors affecting the window change, the launch process and resource allocation are automatically re-arranged;

[0038] Key point quality control: It has the key node control function, and determines whether to enter the next process based on the work progress, test results and resource preparation of the next stage of the current key stage; it also has the risk point identification function, identifies the risks of manpower, progress and resources, automatically evaluates the risk level and results, and provides solutions;

[0039] Emergency status control: If an emergency abnormal situation involving safety such as product failure, gas or liquid leakage, or launch delay occurs, the system will automatically and accurately mobilize resources from all parties according to the pre-made plan to complete subsequent disposal measures and work arrangements.

[0040] In combination with the first aspect, in some implementations of the first aspect, the system is centrally deployed on a server cluster; based on the container and virtualization technology of k8s and kvm, the server resources are integrated and managed to build a computing resource pool.

[0041] In a second aspect, a launch platform is provided, comprising an integrated command and monitoring system as described in any one of the implementations of the first aspect above.

[0042] Compared with the prior art, the solution provided by the present invention includes at least the following beneficial technical effects:

[0043] 1) The method provided by the present invention adopts a technology that combines container cloud and virtual cloud technologies. Through an interface forwarding, a data middle platform, and a login portal, a comprehensive situation display function of the integration of all-factor data of the launch site rocket and satellite test launch process is realized; the problem of data islands caused by complicated processing methods and different styles due to differentiated business requirements of various systems in traditional launch sites is solved, and the problems of incomplete presentation of launch site status information, mismatch between test passwords and process monitoring, and untimely switching of monitoring data are solved.

[0044] 2) The present invention designs a universal launch site command and monitoring platform with interface configuration capability, which solves the problem that the information page needs to modify the software code or configuration file, and the configuration is cumbersome, time-consuming and non-visual. It realizes flexible and fast configuration and customized information push for different positions and different processes, and supports parallel monitoring of no less than 4 launch tasks. It solves the problem that the current launch site needs to independently develop different command and monitoring platforms for different models and different tasks, and cannot realize rapid software deployment and flexible definition of seats.

[0045] 3) The present invention proposes a set of intelligent monitoring systems for launch sites that integrate mission control, equipment monitoring, health assessment, and comprehensive operation and maintenance. Aiming at the high-density launch missions and massive resources of the launch site, the system conducts unified management, allocation, and scheduling of launch missions, and unified management and monitoring of equipment status, presenting the launch site situation in an all-round and multi-angle manner, and improving the digitalization, automation, and intelligence capabilities of the launch site. This solves the problem of low automation in mission control at traditional launch sites. BRIEF DESCRIPTION OF THE DRAWINGS

[0046] Figure 1A This is a schematic diagram of the command and monitoring system architecture and information flow.

[0047] Figure 1B This is a schematic diagram of the command and monitoring system architecture and information flow.

[0048] Figure 2 For configuration flow chart.

[0049] Figure 3 This is the information flow diagram for task control. DETAILED DESCRIPTION

[0050] The present invention is further described in detail below with reference to the accompanying drawings and specific embodiments.

[0051] like Figure 1A and 1BAs shown, the present invention provides an integrated command and monitoring system for smart launch sites. The main body of the integrated command and monitoring system can be a software service, which is centrally deployed on a server cluster; based on containers and virtualization technologies such as k8s and kvm, server resources are integrated and managed to build a computing resource pool, providing a basic operating environment for the integrated command and monitoring system software, while supporting the expansion of subsequent computing resources.

[0052] The integrated command and monitoring system provided by the present invention includes: an interface forwarding module, a data processing and storage middle station, a BS business module and a special business module. The interface forwarding module is responsible for receiving and forwarding the launch site system data. The data processing and storage middle station is responsible for storing and managing the launch site system data, and providing a unified data call interface for business applications. The BS business module controls the user's access to the main business modules according to the user's authority through a unified integrated portal (a system entrance for users), including an integrated command and display module, a health management module, a comprehensive operation and maintenance module, a launch mission management and control module, a launch mission system management and control platform, etc., interacts with the data processing and storage middle station to obtain data resources, and presents them to users through a unified integrated portal to realize module definition seats. Special business modules, such as the test and launch command display module, etc., are independent of the management and control of the unified integrated portal because the business needs to specify seats or have special requirements such as hot standby redundancy and high-performance graphical processing.

[0053] The design plan for data fusion of all elements of the rocket and satellite test launch process at the launch site is as follows.

[0054] 1) Launch site data elements can be divided into frequent acquisition data and fixed input data according to the collection form. The former is time series data, and the latter includes structured data, unstructured data, etc. The database designed for data processing and storage center includes: cache database, which realizes memory storage of high-frequency call data and improves access efficiency; historical database, which realizes time series data storage and management; metadata database, which uses relational database to realize structured data storage; file system, which realizes unstructured data storage.

[0055] 2) The main data elements of the launch site are time series data, which are recorded in the form of table-code. The table number division is based on the GJB 7337 protocol file. The data includes data on rocket systems, satellite systems, refueling systems, launch pad systems, etc. in units of test missions, as well as long-term data such as hydropower and meteorology. For the former, they are classified according to the model-launch-test mission level and stored according to table-code. For the latter, they are directly stored according to table-code. For data based on test missions, different test missions usually share table numbers. Therefore, after marking the model-launch-test mission, the data of different test missions can be distinguished, realizing data fusion storage.

[0056] 3) Whether the data is stored on-site in units of model-launch-test task is one of the attributes of the data, which can be set by operating the relational database through the data processing and storage middle platform.

[0057] By designing two modes of storage according to model-launch-test task classification, the repeated storage of long-term collected data that is not related to model-launch-test task is avoided. Based on the characteristics of time series data, both storage modes store the timestamp of the data, which can be used to associate the two types of data and realize joint analysis and display of the two types of data.

[0058] The design scheme of the integrated command and monitoring system to realize multi-task parallel command and monitoring is as follows.

[0059] 1) The interface forwarding module serves as the interface for the integrated command and monitoring system to interact with the outside world. One set of interface forwarding modules corresponds to one test task. When the interface forwarding module is started, it interacts with the data processing and storage center to obtain the model-launch-test task identification of the data it receives. After receiving the data, it assigns the identification to the data and sends it to the data processing and storage center to realize the data storage of the test task. Through the container cloud platform or virtual cloud platform, multiple sets of interface forwarding modules can be quickly copied and deployed to realize multi-task parallel reception. In actual applications, one set of interface forwarding modules is used to receive data that is not related to the launch site and the model-launch-test task, and other interface forwarding modules receive data from different test tasks respectively.

[0060] 2) The model-issue-test task corresponding to each interface forwarding module can be edited through the data processing and storage middle platform operation database.

[0061] 3) When users use the unified integrated portal module to access major business applications, they need to select model-issue-test task after logging in, so that they can access the information of the test tasks that the user is concerned about.

[0062] 4) Special business applications are divided into two categories. One is to directly obtain data through the interface forwarding module, which is soft-bound to the specific interface forwarding (such as the test command display module); the other is to obtain data through the data processing and storage middle platform, which requires selecting the model-launch-test task after startup, and accessing the unified interface of the data processing and storage middle platform to obtain the corresponding data.

[0063] The solution to the problem of high degree of customization and poor functional flexibility of traditional launch site business modules is as follows.

[0064] 1) At the data level, through a unified integrated portal and a data processing and storage platform, the data elements of business applications are controlled from both top and bottom directions to achieve data independence under multi-task parallel working conditions.

[0065] 2) At the functional level, the user-oriented functions of the integrated command and monitoring system module are all configurable, as follows:

[0066] i. Parameter attribute maintenance: Supports users to maintain the hierarchical relationship and content of model-issue-system-parameter table-parameter definition, providing basic support for the system to receive, process and display data of different test tasks.

[0067] ii. Test task maintenance: supports users to add, delete, modify, check and associate models, releases, test tasks and process time periods. At the same time, users can configure the corresponding interface forwarding module under the test task to build the association relationship between model-release-test task-interface forwarding module.

[0068] iii. User-facing interface: This type of configuration is relatively fixed and the steps are simple. Several fixed display templates are provided, such as one-split screen, two-split screen, and four-split screen. On each split screen, you can select display controls such as data tables, curve charts, and timing charts. After selecting the control, you can select the parameter to be monitored according to the parameter table-code.

[0069] iv. Large-screen display interface: This type of interface is configured by the operation and maintenance personnel before the task, with flexible configuration and various display styles. It provides a canvas and several display controls such as data table, instruction append table, curve chart, indicator light, dashboard, process chart, text, decoration, etc., which can be freely dragged, dragged and scaled on the canvas. After the display control is bound to the data set, the data monitoring large-screen page can be constructed.

[0070] v. Data interpretation: Ability to configure parameter interpretation method, judgment criteria, judgment stage, fault level, alarm information, associated plans, etc.

[0071] The solution to the problem of low automation level of mission control in traditional launch sites is as follows.

[0072] 1) Launch site mission control is divided according to the time scale, including launch site refueling and launch mission process control and launch site full-process mission control. The former is aimed at status monitoring and command at different stages of the refueling and launch process, mainly for test data monitoring based on the test process; the latter includes various tests and transportation of rockets and satellites after entering the site, mainly for process orchestration based on launch site resources.

[0073] 2) Launch site refueling launch mission process control automation design:

[0074] i. Information display automation: The information display of the large-screen indicator includes the test process screen, parameter element screen and camera video based on the module interface. For the module interface screen, the system large-screen display interface is based on the configured process period. Under each configured process period, several large-screen display interfaces can be set. These interfaces support two display logics: patrol display and parameter trigger display (you can set whether to join the patrol after triggering). That is, the process instructions control the process stage, and the test instructions under the process stage control the page display, so as to realize the data-driven module large-screen interface display content. The overall display of the large-screen indicator (including the module interface and camera video) is used as a template. The parameter trigger switching and patrol display mode are realized by splicing the controller and the supporting modules. The two data-driven logics are nested, which can realize the automatic display script arrangement of the large screen of most launch sites.

[0075] ii. Automated abnormal diagnosis: Based on the parameter interpretation method, judgment criteria, judgment stage, fault level, alarm information, and related plans, it can realize automatic background interpretation, alarm and auxiliary decision push based on the test stage.

[0076] iii. Process-driven automation: The test and launch command display module can issue process instructions (enter XX hours of preparation), supporting automatic mode, compressed mode and manual mode. In automatic mode, the corresponding process instructions can be automatically issued based on the launch countdown; in compressed mode, after manually clicking the process instruction button, the estimated ignition time and countdown correspond to the process instruction; in manual mode, after manually clicking the process instruction button, only the process instruction is issued, and the estimated ignition time and countdown are not changed. The above three modes support automatic process, manual process and compressed process during the test process.

[0077] 3) Launch site full-process mission control automation design:

[0078] i. Mission process node configuration: According to the characteristics of different models, you can select the process category through configuration, set the prerequisites for process execution and the functions used for calculation, the output instructions for process execution, adjust the process sequence, complete the process settings and output the process file. Drive the completion of the mission node based on the launch site test data and provide timing requirements for intelligent test and launch and automatic test and launch.

[0079] ii. Launch process control: Realize the whole process scheduling from the mission entry to the mission launch, and intelligently arrange the parallel work progress of multiple tasks according to the window dates and key nodes of different models. Support the arrangement based on the entry date and the arrangement based on the launch date. Support the normal launch process, expedited launch process (expedited progress) and emergency launch process (24 consecutive hours), and generate and push electronic work scheduling sheets every day.

[0080] iii. Launch resource control: Based on the launch process, the launch resources are automatically arranged, including test personnel, ground support, factory buildings, equipment, vehicles, canteen support, fire protection, etc., and the personnel position, work status, warehouse materials and other resource conditions can be uniformly allocated and managed.

[0081] iv. Launch window control: Automatically select the transition and launch window by comprehensively evaluating factors such as the environment, weather, and mission requirements. When factors affecting the window change, the launch process and resource allocation are automatically re-arranged.

[0082] v. Key point quality control: It has key node control function, and determines whether to enter the next process according to the work progress, test results and resource preparation of the next stage in the current key stage, such as the conditions for the transfer of the star cover assembly, the conditions for the transfer of the rocket, the conditions for refueling and launching, etc. It also has the function of risk point identification, identifies risks such as manpower, progress, and resources, automatically evaluates risk levels and results, and provides solutions.

[0083] vi. Emergency status control: If an emergency abnormal situation involving safety, such as product failure, gas or liquid leakage, or launch delay, occurs, the system can automatically and accurately mobilize resources from all parties according to the pre-made plan, and complete the subsequent disposal measures and work arrangements in a reasonable and efficient manner.

[0084] The present invention designs an integrated command and monitoring technology for smart launch site applications, which adopts a technology that combines container cloud and virtual cloud technology. Through an interface forwarding, a data middle platform, and a login portal, it has the data integration capability of no less than 10 systems and 1,000 elements during the launch site test launch process, and realizes comprehensive management and situation presentation of the data of the entire life cycle of the launch mission.

[0085] Based on the traditional launch site data monitoring, the present invention proposes an integrated monitoring method for equipment, process and data, breaks through key technologies such as data-driven system multi-dimensional visual monitoring and process timing monitoring, realizes automatic switching of large screens driven by data and processes, realizes unified alignment of monitoring elements and test and launch processes, and improves the automation level of launch site test and launch command. Information reception, processing and display are completed within 1s, the real-time processing capacity is greater than 100Mbps, and the amount of data recorded continuously at one time is not less than 100GB.

[0086] The present invention designs a universal launch site command and monitoring platform, which supports flexible configuration by user-configured drag and drop, without the need to modify module codes, thus lowering the threshold for user use; it has the ability to push customized information for specific positions and processes, can achieve rapid deployment for different models and different seats, and has the ability to simultaneously support parallel monitoring of no less than 4 launch missions.

[0087] The present invention designs a launch site mission intelligent monitoring platform that integrates launch mission management and control, equipment monitoring, health assessment, and comprehensive operation and maintenance. It is aimed at the high-density launch missions and massive resources of the launch site, and realizes unified management, allocation, and scheduling of no less than 50 high-density launch missions, and unified management and monitoring of the status of no less than 2,000 equipment. It presents the launch site situation in an all-round and multi-angle manner, realizes the closed-loop control of "situation monitoring-task scheduling-coordinated scheduling-status feedback", meets the needs of efficient collaborative operation and maintenance for the launch site test and launch process, and improves the digitalization, automation, and intelligence capabilities of the launch site.

[0088] Although the present invention is disclosed as above in the form of a preferred embodiment, it is not intended to limit the present invention. Any person skilled in the art may make possible changes and modifications without departing from the spirit and scope of the present invention. Therefore, the scope of protection of the present invention shall be based on the scope defined by the claims of the present invention.

Claims

1. An integrated command and monitoring system for a smart launch site, characterized in that: include: Interface forwarding module, responsible for receiving and forwarding launch site system data; The data processing and storage middle platform is responsible for storing and managing the launch site system data and providing a unified data calling interface for business applications; The BS business module controls user access to the main business modules according to user permissions through a unified integrated portal, including an integrated command and display module, a health management module, an integrated operation and maintenance module, a launch mission control module, and a launch mission system control platform. It interacts with the data processing and storage middle platform to obtain data resources, presents them to users through a unified integrated portal, and realizes module definition seats; Special business modules, including the test, launch, command and display modules, are independent of the management and control of the unified integrated portal.

2. The integrated command and monitoring system according to claim 1 is characterized in that: The launch site data elements are divided into frequent acquisition data and fixed input data according to the acquisition form. Frequent acquisition data is time series data, and fixed input data includes structured data and unstructured data. The database design of the data processing and storage platform includes: Cache database to achieve memory storage of high-frequency call data and improve access efficiency; Historical database, to realize the storage and management of time series data; Metadatabase, which uses relational database to store structured data; File system, which enables storage of unstructured data.

3. The integrated command and monitoring system according to claim 2 is characterized in that: The main body of the launch site data elements is time series data, which is recorded in the form of table-code. The table number division is based on the GJB 7337 protocol document. The data includes data on the rocket system, satellite system, refueling system, and launch pad system in units of test missions, as well as water, electricity, and meteorological data. Among them, the table numbers are classified according to the model-issue-test task level and stored according to table-code; the data corresponding to the table numbers are stored according to table-code; One of the properties of data storage is whether the data is stored on site in units of model-launch-test task. It is set by operating the relational database through the data processing and storage middle platform.

4. The integrated command and monitoring system according to claim 3 is characterized in that: The system realizes multi-task parallel command and monitoring to meet the following requirements: The interface forwarding module serves as the interface for the integrated command and monitoring system to interact with the outside world. One set of interface forwarding modules corresponds to one test task. When the interface forwarding module is started, it interacts with the data processing and storage center to obtain the model-launch-test task identifier of the data it receives. After receiving the data, the identifier is assigned to the data and sent to the data processing and storage center to realize the data storage of the test task. Multiple sets of interface forwarding modules are replicated and deployed through the container cloud platform or virtual cloud platform, one set of interface forwarding modules is used to receive data that is not related to the launch site and the model-launch-test task, and other interface forwarding modules receive data of different test tasks respectively. The model-launch-test task corresponding to each interface forwarding module is edited through the data processing and storage center operation database. When users use the unified integrated portal module to access the business module, they select Model-Times-Test Task after logging in to access the corresponding test task information; Special business applications are divided into two categories; one is to obtain data directly through the interface forwarding module, and soft-bind it to the specific interface forwarding; the other is to obtain data through the data processing and storage middle platform. After startup, select model-issue-test task, and access the unified interface of the data processing and storage middle platform to obtain the corresponding data.

5. The integrated command and monitoring system according to claim 3 or 4, characterized in that: The system comprises: Parameter attribute maintenance: used to maintain the hierarchical relationship and content of model-issue-system-parameter table-parameter definition, providing support for the system to receive, process and display data of different test tasks; Test task maintenance: used to add, delete, modify, check and associate models, releases, test tasks and process time periods. At the same time, configure the corresponding interface forwarding module under the test task to build the association relationship between model-release-test task-interface forwarding module; User-facing interface: provides one-, two-, and four-screen display templates. On each screen, select display controls for data tables, curve graphs, and timing diagrams. After selecting a control, select the parameter to be monitored according to the parameter table-code. Interface for large-screen display: Provides a canvas and display controls for data tables, instruction append tables, curve charts, indicator lights, dashboards, process charts, text, and decorations. Freely drag, drag, and zoom on the canvas. After the display controls are bound to data sets, a large-screen page for data monitoring is constructed. Data interpretation: parameter interpretation method, judgment criteria, judgment stage, fault level, alarm information, and related plans.

6. The integrated command and monitoring system according to claim 5, characterized in that: The system's process of controlling the launch site mission meets the following requirements: The launch site mission control is divided according to the time scale, including the launch site refueling and launch mission process control and the launch site full-process mission control. The launch site refueling and launch mission process control is aimed at status monitoring and command at different stages of the refueling and launch process, which is test data monitoring based on the test process. The launch site full-process mission control includes various tests and transportation of rockets and satellites after entering the site, and is mainly a process orchestration based on launch site resources.

7. The integrated command and monitoring system according to claim 6, characterized in that: The launch site refueling launch mission process control includes: Information display automation: The information display of the large screen includes the test process screen, parameter element screen and camera video based on the module interface; for the module interface screen, the system large screen display interface is based on the configured process period. Under each configured process period, several large screen display interfaces are set. These interfaces support two display logics: patrol display and parameter trigger display. The process stage is controlled by process instructions, and the test instructions under the process stage control page display to realize data-driven module large screen interface display content; the overall display of the large screen is used as a template, and the parameter trigger switching and patrol display mode are realized by splicing the controller and the supporting modules. The two data-driven logics are nested to realize the automatic display script arrangement of the launch site large screen; Automated abnormal diagnosis: Based on the parameter interpretation method, judgment criteria, judgment stage, fault level, alarm information, and associated plans, the system can realize automatic background interpretation, alarm, and auxiliary decision-making push based on the test stage; Process-driven automation: The test and launch command display module issues process instructions and supports automatic mode, compressed mode and manual mode. In automatic mode, the corresponding process instructions are automatically issued based on the launch countdown. In compressed mode, after manually clicking the process instruction button, the estimated ignition time and countdown correspond to the process instruction. In manual mode, after manually clicking the process instruction button, only the process instruction is issued without changing the estimated ignition time and countdown.

8. The integrated command and monitoring system according to claim 6, characterized in that: The whole process of mission control at the launch site includes: Mission process node configuration: According to different models, through configuration, select the process category, set the preconditions for process execution and the functions used for calculation, the output instructions for process execution, adjust the process sequence, complete the process settings and output the process file, drive the completion of the mission node based on the launch site test data, and provide timing requirements for intelligent test and automatic test; Launch process control: Execute the full process scheduling from mission entry to mission launch, and intelligently arrange the parallel work progress of multiple tasks according to the window dates and key nodes of different models. It supports scheduling based on the entry date and scheduling based on the launch date, and supports normal launch processes, expedited launch processes, and emergency launch processes. It generates and pushes electronic work scheduling sheets every day. Launch resource control: Based on the launch process, launch resources are automatically arranged, including test personnel, ground support, workshops, equipment, vehicles, canteen support, and fire protection, and personnel in place, work conditions, warehouse materials and other resources are uniformly allocated and managed; Launch window control: Automatically select the transition and launch window by comprehensively evaluating the environment, weather, and mission requirements. When the factors affecting the window change, the launch process and resource allocation are automatically re-arranged; Key point quality control: It has the key node control function, and determines whether to enter the next process based on the work progress, test results and resource preparation of the next stage of the current key stage; it also has the risk point identification function, identifies the risks of manpower, progress and resources, automatically evaluates the risk level and results, and provides solutions; Emergency status control: If an emergency abnormal situation involving safety such as product failure, gas or liquid leakage, or launch delay occurs, the system will automatically and accurately mobilize resources from all parties according to the pre-made plan to complete subsequent disposal measures and work arrangements.

9. The integrated command and monitoring system according to any one of claims 1 to 8, characterized in that: The system is centrally deployed on a server cluster; based on the container and virtualization technology of k8s and kvm, server resources are integrated, managed and controlled to build a computing resource pool.

10. A launch platform, comprising the integrated command and monitoring system according to any one of claims 1 to 9.

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