Space launch control task automation platform and method

Abstract

This invention provides an automated command platform and method for aerospace launch telemetry, tracking, and command (TT&C) missions, belonging to the field of aerospace TT&C technology. It includes a TT&C command module and a rapid TT&C mission evaluation module. The TT&C command module is equipped with a first data transceiver engine, which sends TT&C commands to each participating unit in the TT&C system, driving the TT&C system to execute TT&C integration or operational missions. It also obtains the next TT&C command based on the evaluation results transmitted by the rapid TT&C mission evaluation module. The rapid TT&C mission evaluation module is equipped with a second data transceiver engine, which acquires mission data sent by each parameter unit of the TT&C system, evaluates the mission data according to the TT&C commands, obtains the evaluation results, and transmits the evaluation results to the TT&C command module. This invention flattens the command chain, reduces manual intervention, and improves the efficiency and automation level of TT&C mission execution.

Description

Technical Field

[0001] This invention relates to the field of aerospace telemetry and control technology, and more specifically, to an automated command platform and method for aerospace launch telemetry and control missions. Background Technology

[0002] Space launch tracking and control (TT&C) is a crucial link in ensuring the safe flight and precise orbit insertion of launch vehicles and payloads. In the existing organization and implementation of space launch TT&C missions, system engineers primarily rely on observing display software parameters, personally supervising at TT&C sites, and communicating by telephone to oversee the mission process. TT&C command and control organizes and distributes mission plans through written mission documents, and coordinates the scheduling of various TT&C resources via voice dispatch. This model relies heavily on human intervention.

[0003] Specifically, such as Figure 1 As shown, the existing command system for space launch telemetry, tracking, and command (TT&C) missions typically employs a three-tiered architecture: Chief TT&C Commander → Station Commander → On-site Commander / Operator. The station-level command acts as a "second-hand information relay," facilitating communication between higher and lower levels. Due to a lack of information-based command tools, commands are transmitted level by level via voice or paper documents, resulting in problems such as untimely transmission, susceptibility to errors, and difficulty in traceability. Furthermore, the diverse range of TT&C equipment (including launch control consoles, external ballistic measurement systems, telemetry and remote control systems, and TT&C center systems) necessitates manual scheduling for coordination between these devices, leading to a lengthy overall command chain and low efficiency in mission organization and implementation.

[0004] On the other hand, the quality assessment of telemetry and control missions mainly relies on post-mission manual interpretation or semi-automatic analysis. Assessment rules are scattered across the experience of various technical experts, lacking a unified digital representation; the assessment granularity is limited, making it difficult to conduct multi-level, real-time automated evaluations of joint commissioning projects, single joint commissioning sessions, mission phases, actual missions, and the overall mission. More importantly, the planning, command, anomaly handling, and mission assessment processes are disconnected—assessment results cannot be promptly fed back to the command center to drive the automatic generation of subsequent instructions, and the command center cannot dynamically adjust mission procedures based on real-time assessment conclusions.

[0005] The existing telemetry, tracking, and command (TT&C) model, characterized by high labor costs and low levels of information technology, is no longer adequate for future mission requirements. In recent years, while some patents and documents have proposed methods for commanding and scheduling aerospace test missions (e.g., scheduling missions in hierarchical levels, with higher-level command stations sending instructions to lower-level stations, and lower-level stations reporting fault modes and searching knowledge bases for fault handling), these solutions still retain a multi-level command architecture and fail to achieve a flattened command chain. Furthermore, other patents disclose evaluation methods for aerospace TT&C missions, but these lack a closed-loop linkage mechanism between evaluation and command; the evaluation results are only used for post-event reference and cannot drive the command process in real time.

[0006] Therefore, there is an urgent need in this field for a new type of automated command platform and method for aerospace launch telemetry and control missions that can achieve flattened command links, digitalized planning and scheduling, standardized handling of anomalies, and establish a closed-loop linkage between assessment and command, in order to solve the prominent problems in existing technologies such as high dependence on manual labor, untimely transmission of command information, and fragmentation of various links. Summary of the Invention

[0007] In view of this, and in response to the technical problems of high dependence on manual labor, untimely transmission of command information, and lack of evaluation-command linkage mechanism in the existing technology, the present invention provides an automated command platform and method for aerospace launch telemetry and control missions.

[0008] To achieve the above objectives, the present invention proposes an automated command platform for aerospace launch telemetry and control missions, comprising: The telemetry and control command module and the rapid assessment module for telemetry and control tasks; The measurement and control command module is equipped with a first data transceiver engine, which sends measurement and control commands to each participating unit in the measurement and control system to drive the measurement and control system to perform measurement and control joint debugging or actual combat tasks; and obtains the next measurement and control command based on the evaluation results transmitted by the measurement and control task rapid evaluation module. The rapid assessment module for measurement and control tasks is equipped with a second data transceiver engine. The second data transceiver engine acquires task data sent by each parameter unit of the measurement and control system, assesses the task data according to the measurement and control instructions, obtains the assessment result, and transmits the assessment result to the measurement and control command module.

[0009] Optionally, the measurement and control command module includes a planning and arrangement component, a planning and decomposition component, and an instruction generation component. The planning and arrangement component arranges the measurement and control task plan according to a macro-to-micro hierarchical structure; the planning and decomposition component decomposes the arranged measurement and control task plan to obtain a measurement and control instruction sequence; and the instruction generation component generates measurement and control instructions from the measurement and control instruction sequence.

[0010] Optionally, the planning and scheduling component can also acquire and generate a new measurement and control task plan based on the new work plan application, and determine the new measurement and control task plan.

[0011] Optionally, the measurement and control command module is further provided with an anomaly handling unit, wherein the first data transceiver engine receives the feedback information returned by each test unit, wherein the feedback information includes status information and test data; the anomaly handling unit evaluates the test unit according to the feedback information to obtain the operating status of the test unit; when an abnormal operating status occurs in the test unit, the abnormal operating status is handled by the pre-set handling measures in the anomaly case database.

[0012] Optionally, in the abnormal case database, the decision types in the handling measures include ignoring the abnormality and continuing execution as planned, waiting for the abnormality to be handled before continuing execution, removing the test unit that has experienced a major failure, repeating the previous joint debugging project, and terminating the entire system workflow.

[0013] Optionally, the rapid evaluation module for measurement and control tasks includes: an evaluation item library, an evaluation item component, and a responsibility chain processing component. The evaluation item library maintains a set of evaluation items for each participating unit. Each evaluation item includes a corresponding data source list and evaluation rules. The evaluation item component selects the corresponding evaluation item based on the measurement and control task scenario, and performs real-time evaluation of the task data using these evaluation items. The responsibility chain processing component performs hierarchical, top-down, layer-by-layer aggregation of the real-time evaluation results to obtain the evaluation results, which include measurement and control task evaluation conclusions and recommendations at different granularities.

[0014] Optionally, the plan decomposition component obtains the measurement and control instruction sequence and executes the measurement and control task, wherein the corresponding process includes: The project preparation instruction is sent to each participating unit through the plan decomposition component, and the preparation status and equipment status parameters returned by each participating unit are received. Capability assessment is performed based on the preparation status and equipment status parameters to obtain the execution capability assessment result. Based on the execution capability assessment result, the action execution instruction is sent to each participating unit through the plan decomposition component according to the specific execution process of the project. The action execution instruction is used to control each participating unit to complete the measurement and control project work, and the operating status of each participating unit is obtained and evaluated. According to the project execution duration of the measurement and control task plan, the project stop instruction is sent to each participating unit at the corresponding time node.

[0015] Optionally, a B / S architecture with front-end and back-end separation can be adopted, with the framework and components corresponding to the measurement and control command module and the rapid evaluation module of measurement and control tasks deployed in the B / S architecture.

[0016] Optionally, the structured evaluation rules are described using a JSON data structure.

[0017] On the other hand, the present invention provides an automated command method for aerospace launch telemetry and control missions, comprising: The first data transceiver engine sends measurement and control commands to each participating unit of the measurement and control system, driving the measurement and control system to perform measurement and control joint debugging or actual combat tasks, and sends the measurement and control commands to the measurement and control task rapid evaluation module. The system accesses task data sent by each participating unit of the measurement and control system through the second data transceiver engine, performs measurement and control task process evaluation according to the measurement and control task scenario corresponding to the current measurement and control command, generates evaluation results, and pushes the evaluation results to the measurement and control command module. The measurement and control command module sends the next measurement and control command based on the evaluation results.

[0018] Compared with the prior art, the beneficial effects of the present invention are as follows: (1) By setting up an independent data transceiver engine command module and evaluation module, and establishing a closed-loop linkage mechanism that drives the sending of command instructions based on evaluation conclusions, the automatic advancement of the measurement and control command process is realized, which solves the technical problem of the separation of command and evaluation in the existing technology. (2) By adopting a flat two-level command structure and the method of decomposing digital plans into a sequence of instructions, the command chain is shortened, intermediate links in the command process are reduced, and command efficiency is improved; (3) Through multi-level evaluation granularity and structured evaluation rules, the automated evaluation of the measurement and control task process was realized, providing commanders with real-time and quantitative decision-making basis; (4) By pre-setting five types of abnormal handling decisions and abnormal handling units, the platform’s ability to automatically handle abnormal situations has been improved, and manual intervention has been reduced. Attached Figure Description

[0019] Various other advantages and benefits will become apparent to those skilled in the art upon reading the following detailed description of preferred embodiments. The accompanying drawings are for illustrative purposes only and are not intended to limit the invention. In the drawings: Figure 1 This is a diagram illustrating the personnel composition of a space launch telemetry and control mission in an embodiment of the present invention. Figure 2 This is a schematic diagram of a space launch telemetry and control mission planning model in an embodiment of the present invention; Figure 3 This is a flowchart illustrating the process of generating a space launch telemetry and control mission plan in an embodiment of the present invention. Figure 4 This is a flowchart illustrating the decomposition of aerospace launch telemetry and control mission plans in an embodiment of the present invention. Figure 5 This is a schematic diagram of the exception handling process in an embodiment of the present invention; Figure 6 This is a schematic diagram of the evaluation item model of the aerospace launch telemetry and control system in an embodiment of the present invention; Figure 7 This is a schematic diagram of the measurement and control task scenario evaluation model in an embodiment of the present invention; Figure 8 This is a schematic diagram of the software system architecture of the space launch telemetry and control mission command automation platform in an embodiment of the present invention; Figure 9 This is a schematic diagram illustrating the software engineering implementation of the space launch telemetry and control mission command automation platform in an embodiment of the present invention. Detailed Implementation

[0020] Exemplary embodiments of the present disclosure will now be described in more detail with reference to the accompanying drawings. While exemplary embodiments of the present disclosure are shown in the drawings, it should be understood that the present disclosure may be implemented in various forms and should not be limited to the embodiments set forth herein. Rather, these embodiments are provided to enable a more thorough understanding of the present disclosure and to fully convey the scope of the disclosure to those skilled in the art. It should be noted that, unless otherwise specified, the embodiments and features described herein can be combined with each other. The present invention will now be described in detail with reference to the accompanying drawings and embodiments.

[0021] This invention discloses an automated command platform and method for aerospace launch telemetry, tracking, and command (TT&C) missions, belonging to the field of aerospace TT&C technology. The invention adopts a dual-engine architecture of a TT&C command module and a rapid TT&C mission evaluation module, both with independent data transceiver engines. The command module sends commands to the TT&C unit and drives mission execution, while simultaneously synchronizing the commands to the evaluation module. The evaluation module accesses real-time data based on the mission scenario, performs multi-granularity evaluation using structured evaluation rules, and pushes the evaluation conclusions back to the command module to drive the next command transmission, forming a closed-loop linkage between evaluation and command. The command module employs a four-layer digital modeling approach: "overall-stage-integration-project," automatically decomposing the plan into preparation commands, action commands, and stop commands, supporting five types of anomaly handling decisions: ignore, wait, eliminate, repeat, and terminate. This invention flattens the command chain, reduces manual intervention, and improves the efficiency and automation level of TT&C mission execution.

[0022] This embodiment proposes an automated command platform for aerospace launch telemetry and control missions, including: The measurement and control command module is equipped with a first data transceiver engine, which is used to send measurement and control commands to each participating unit of the measurement and control system through the first data transceiver engine, drive the measurement and control system to perform measurement and control joint debugging or actual combat tasks, and receive the feedback information returned by each participating unit. The rapid evaluation module for measurement and control tasks is equipped with a second data transceiver engine, which is used to access the task data sent by each participating unit of the measurement and control system through the second data transceiver engine, perform the evaluation of the measurement and control task process according to the measurement and control task scenario corresponding to the current measurement and control command, and generate evaluation conclusions and suggestions. The measurement and control command module sends measurement and control instructions to the measurement and control task rapid evaluation module. The measurement and control task rapid evaluation module pushes its generated evaluation conclusions and suggestions to the measurement and control command module through the second data transceiver engine. The measurement and control command module sends the next measurement and control instructions based on the evaluation conclusions and suggestions.

[0023] Furthermore, the measurement and control command module includes: The planning and arrangement component is used to arrange the measurement and control mission plan according to a hierarchical structure from macro to micro, wherein the hierarchical structure includes, in sequence, the overall mission plan, the mission phase plan, the joint debugging plan, and the joint debugging project plan; The plan decomposition component is used to decompose the arranged task plan into a sequence of measurement and control instructions, which includes project preparation instructions, action execution instructions, and project stop instructions. The instruction generation component is used to generate information-based instructions in a unified format from the decomposed instruction sequences.

[0024] Furthermore, the planning and scheduling component is also used to: automatically determine the rationality of the newly generated work plan based on the time nodes, work items, scheduling order and existing work plans in the task plan, and submit the determination result to the commander for review; and automatically generate a new task work plan based on the work plan application submitted by the test equipment.

[0025] Furthermore, the measurement and control command module is equipped with an anomaly handling unit. The anomaly handling unit is used to evaluate the operating status of each participating unit in real time based on the status information and test data of each participating unit, and automatically handle the anomaly in combination with the pre-set handling measures in the anomaly case library. When there is an anomaly that cannot be handled, it is handed over to the commander for decision-making. The anomaly handling unit supports at least one of the following decision types during the anomaly handling process: ignoring the anomaly and continuing execution as planned, waiting for the anomaly to be handled before continuing execution, removing the test unit that has experienced a major failure, repeating the previous joint debugging project, or terminating the entire system workflow.

[0026] Furthermore, the rapid evaluation module for the measurement and control task includes: The evaluation item library maintains a set of evaluation items for each type of measurement and control equipment or measurement and control unit. Each evaluation item includes a list of data sources that need to be subscribed to and structured evaluation rules. The evaluation item component is used to select applicable evaluation items from the evaluation item library according to the current measurement and control task scenario, and to evaluate the accessed task data in real time. The responsibility chain processing component is used to summarize and evaluate the results layer by layer from bottom to top according to the multi-level granularity of joint commissioning project level, single joint commissioning level, task phase level, actual combat task level and overall task level, and form evaluation conclusions and recommendations for measurement and control tasks at different granularities.

[0027] Furthermore, the structured evaluation rules are described using a JSON data structure.

[0028] Furthermore, both the measurement and control command module and the measurement and control task rapid evaluation module adopt a "framework + component" software architecture, with each module calling functional components through its main framework.

[0029] Furthermore, the platform adopts a front-end and back-end separated B / S architecture, wherein: The browser-based software includes system-level command terminal software, equipment-level command terminal software, and telemetry and control task quick evaluation terminal software. The server side includes measurement and control mission command server software, measurement and control mission quick evaluation server software, measurement and control mission planning and scheduling software, and measurement and control mission information configuration and management software.

[0030] Furthermore, the process by which the plan decomposition component decomposes the task plan into a sequence of measurement and control instructions and executes the measurement and control tasks specifically includes: The planning decomposition component first sends a project preparation instruction to each participating unit, and then assesses whether each participating unit has the ability to execute the project based on the preparation status and equipment status parameters reported by each participating unit. Under the condition that the equipment status meets the requirements, action execution instructions are sent to each participating unit according to the specific execution process of the project, and the participating units are uniformly commanded and coordinated to complete the measurement and control project work. The operating status of each participating unit is evaluated in real time during the project execution process. According to the project execution duration specified in the work plan, a project stop instruction is sent at the corresponding time node. After receiving the stop instruction, each participating unit exits the current project execution program.

[0031] An automated command method for space launch telemetry, tracking, and command missions, applied to the aforementioned automated command platform for space launch telemetry, tracking, and command missions, includes: The first data transceiver engine sends measurement and control commands to each participating unit of the measurement and control system, drives the measurement and control system to perform measurement and control joint debugging or actual combat tasks, and receives the feedback information returned by each participating unit. The measurement and control commands are sent together to the measurement and control task rapid evaluation module; The system accesses task data sent by each participating unit of the measurement and control system through the second data transceiver engine, performs measurement and control task process evaluation according to the measurement and control task scenario corresponding to the current measurement and control command, and generates evaluation conclusions and suggestions. The evaluation conclusions and recommendations are then pushed to the measurement and control command module. Based on the assessment conclusions and recommendations, send the next step of the measurement and control instructions.

[0032] The above technical solution will be described in detail with reference to the relevant accompanying drawings and specific embodiments: Example 1: Overall Platform Architecture This embodiment provides an automated command platform for aerospace launch telemetry and control missions.

[0033] like Figure 8As shown, the platform consists of two parts: a telemetry and control command module and a rapid assessment module for telemetry and control tasks. Both modules have independent data transceiver engines, which perform information communication tasks. This dual-engine independent design allows command and assessment to work in parallel without interference, while also enabling collaborative operation through information sharing.

[0034] The measurement and control command module sends measurement and control commands to each participating unit of the measurement and control system through its data transceiver engine, driving the entire system to execute corresponding measurement and control joint debugging or practical tasks. Each measurement and control unit sends response information to the measurement and control command module. Simultaneously, the measurement and control command module sends the measurement and control commands to the rapid assessment module for the measurement and control task. The rapid assessment module identifies the current measurement and control task scenario based on the received commands, accesses the task data sent by each participating unit, performs the corresponding measurement and control task process assessment, and pushes the assessment conclusions and recommendations to the measurement and control command module through its data transceiver engine. Based on the received assessment conclusions and recommendations, the measurement and control command module sends the next measurement and control command, forming a closed loop of "command → execution → assessment → feedback → re-command."

[0035] Example 2: Planning and Decomposition This embodiment further discloses the specific composition of the measurement, control, and command module.

[0036] like Figure 2 As shown, the planning and scheduling component in the telemetry, tracking, and command module arranges the telemetry and control mission plan according to a hierarchical structure of "overall mission plan → mission phase plan → joint debugging plan → joint debugging project plan". The overall mission plan includes basic information such as the overall objectives of the telemetry and control mission, mission start and end times, mission phase divisions, participating equipment, and theoretical trajectories; the mission phase plan includes phase objectives, phase start and end times, and joint debugging plan arrangements; the joint debugging plan includes the purpose of joint debugging, joint debugging start and end times, and project plan arrangements; the project plan includes specific content such as the purpose of project joint debugging, project execution duration, and participating equipment.

[0037] like Figure 3 As shown, after the plan is arranged, the system automatically determines the rationality of the newly generated plan by combining the time nodes, work items, arrangement order, and existing work plans in the plan, and submits the determination result to the commander for review. The equipment can also submit work plan requests to the superior command, and the system has the ability to automatically generate new task work plans based on the requests submitted by the equipment.

[0038] like Figure 4As shown, during the execution of measurement and control tasks, the plan decomposition component breaks down the arranged task plan into a sequence of measurement and control instructions. The instruction generation component generates information instructions in a unified format from the instruction sequence and pushes them outward through the data transceiver engine. The instruction sequence specifically includes: first, sending a project preparation instruction to assess whether the system has the capability to execute based on the preparation status reported by each subsystem and the equipment status parameters; second, if the equipment status meets the requirements, sending action execution instructions (such as T0 sending instructions, delay test instructions, etc.) according to the specific project execution process; and third, sending a project stop instruction at the corresponding time node according to the project execution duration specified in the work plan.

[0039] Example 3: Abnormal Handling This embodiment further discloses the specific implementation of anomaly handling.

[0040] like Figure 5 As shown, the measurement and control command platform collects status information and test data from various measurement and control subsystems, assesses the operational status of each subsystem in real time, and automatically handles anomalies based on pre-set contingency measures in the anomaly case database. The platform supports the following five standardized decision-making methods: (1) Ignore: Directly ignore the existing anomalies and continue to direct each subsystem to complete the subsequent work according to the plan. This is applicable to situations where the status of a single device is abnormal but does not affect the main function of the device. (2) Waiting: The entire system is in a waiting state, and the work plan will continue to be executed after the exception is handled. This is applicable to situations such as subsystem response timeout. (3) Removal: Remove abnormal test subsystems from the test equipment list. This is applicable when equipment experiences a major failure and cannot be recovered in a short period of time. (4) Repetition: Re-execute the previous joint commissioning project. This applies to situations where an anomaly occurs in the current joint commissioning project but is restored to normal before the project ends, or where the project execution results are not evaluated as satisfactory. (5) Termination: Terminate the entire system workflow. This is applicable to situations where a major anomaly occurs that affects the operation of the entire system.

[0041] If there are any anomalies that cannot be handled automatically, the decision to be made and executed shall be left to the commander.

[0042] Example 4: Task Evaluation This embodiment further discloses the specific implementation of the rapid evaluation module for measurement and control tasks.

[0043] like Figure 6 As shown, the platform maintains a set of evaluation items for each type of measurement and control equipment or measurement and control unit. Each evaluation item consists of a list of data sources that need to be subscribed to and structured evaluation rules (described using JSON data structure).

[0044] Taking Table 1 as an example, different types of telemetry and control units have different evaluation items: the takeoff control console includes T0 acquisition correctness, communication link stability, etc.; optical equipment, radar equipment, telemetry equipment, and security control equipment all include evaluation items such as T0 response correctness, ballistic loading correctness, and target tracking correctness; the central machine system includes T0 processing correctness, ballistic processing correctness, and ballistic optimization correctness, etc.; the command and display system includes information display correctness and stability, etc.

[0045]

[0046] In specific measurement and control mission scenarios, the platform selects applicable evaluation items from the evaluation item library to form a mission evaluation model for that scenario (e.g., ...). Figure 7 (As shown). By accessing subscribed real-time task data, real-time evaluation is performed according to pre-configured structured evaluation rules.

[0047] The assessment granularity covers five levels: Joint commissioning project level (assessment results are generated based on the assessment items involved in each measurement and control unit) → Single joint commissioning level (assessment reports are generated based on the assessment results of each joint commissioning project) → Mission phase level (assessment reports are generated based on the completion status of each single joint commissioning within a phase) → Practical mission level (practical assessment reports are generated) → Overall mission level (a summary assessment report is generated based on the completion status of the measurement and control system mission throughout the entire mission cycle). The responsibility chain processing component summarizes the assessment results layer by layer from bottom to top.

[0048] Example 5: Software Engineering Implementation This embodiment further discloses the software implementation of the platform.

[0049] like Figure 9 As shown, the platform adopts a B / S architecture with a front-end and back-end separation. The browser side includes system-level command terminal software, equipment-level command terminal software, and measurement and control task quick evaluation terminal software, and uses the Vue framework to implement the front-end interactive functions.

[0050] The server side includes four core software programs: the telemetry and control mission command server software and the telemetry and control mission quick evaluation server software are real-time running software for missions, developed using Qt development tools and C++ language, with complex evaluation algorithms and report generation functions developed using Python language; the telemetry and control mission planning and scheduling software and the telemetry and control mission information configuration and management software focus on the pre-configuration and storage of information, developed using Java language and using a persistence framework.

[0051] Both the measurement and control command module and the rapid assessment module for measurement and control tasks adopt a "framework + component" software architecture, which is deployed in the corresponding software on the server and browser sides. Each module calls the functional components through its main framework, which reduces the complexity of the interfaces between modules and ensures the scalability of the system.

[0052] In summary, the space launch telemetry and control mission command automation platform and method of the present invention are applicable to various space launch site telemetry and control mission organization and implementation scenarios. They can effectively solve the problems of high dependence on manual labor and low efficiency of command information transmission in existing technologies, and have broad industrial application prospects.

[0053] Contents not described in detail in this specification are prior art known to those skilled in the art. Although illustrative specific embodiments of the invention have been described above to facilitate understanding by those skilled in the art, it should be understood that the invention is not limited to the scope of the specific embodiments. Various modifications are readily apparent to those skilled in the art as long as they fall within the spirit and scope of the invention as defined and determined by the appended claims, and all inventions utilizing the concept of this invention are protected.

[0054] Finally, it should be noted that the above embodiments are only used to illustrate the technical solutions of the present invention and not to limit it. Although the present invention has been described in detail with reference to the above embodiments, those skilled in the art should understand that modifications or equivalent substitutions can still be made to the specific implementation of the present invention. Any modifications or equivalent substitutions that do not depart from the spirit and scope of the present invention should be covered within the scope of protection of the claims of the present invention.

Claims

1. An automated command platform for space launch telemetry and control missions, characterized in that, include: The telemetry and control command module and the rapid assessment module for telemetry and control tasks; The measurement and control command module is equipped with a first data transceiver engine, which sends measurement and control commands to each participating unit in the measurement and control system to drive the measurement and control system to perform measurement and control joint debugging or actual combat tasks; and obtains the next measurement and control command based on the evaluation results transmitted by the measurement and control task rapid evaluation module. The rapid assessment module for measurement and control tasks is equipped with a second data transceiver engine. The second data transceiver engine acquires task data sent by each parameter unit of the measurement and control system, assesses the task data according to the measurement and control instructions, obtains the assessment result, and transmits the assessment result to the measurement and control command module.

2. The platform according to claim 1, characterized in that, The measurement and control command module includes a planning and arrangement component, a planning and decomposition component, and an instruction generation component. The planning and arrangement component arranges the measurement and control task plan according to a macro-to-micro hierarchical structure; the planning and decomposition component decomposes the arranged measurement and control task plan to obtain a sequence of measurement and control instructions; and the instruction generation component generates measurement and control instructions from the sequence of measurement and control instructions.

3. The platform according to claim 1, characterized in that, The planning and scheduling component also acquires and generates a new measurement and control task plan based on the new work plan application, and makes a judgment on the new measurement and control task plan.

4. The platform according to claim 1, characterized in that, The measurement and control command module is also equipped with an anomaly handling unit. The unit receives the feedback information returned by each test unit through the first data transceiver engine. The feedback information includes status information and test data. The anomaly handling unit evaluates the test unit based on the feedback information to obtain the operating status of the test unit. When an abnormal operating status occurs in the test unit, the abnormal operating status is handled by the pre-set handling measures in the abnormal case database.

5. The platform according to claim 1, characterized in that, In the abnormal case database, the decision types for handling measures include ignoring the abnormality and continuing execution as planned, waiting for the abnormality to be handled before continuing execution, removing the test unit that has experienced a major failure, repeating the previous joint debugging project, and terminating the entire system workflow.

6. The platform according to claim 1, characterized in that, The rapid evaluation module for measurement and control tasks includes: an evaluation item library, an evaluation item component, and a responsibility chain processing component. The evaluation item library maintains a set of evaluation items for each participating unit. Each evaluation item includes a corresponding data source list and evaluation rules. The evaluation item component selects the appropriate evaluation item based on the measurement and control task scenario, and performs real-time evaluation of the task data using these evaluation items. The responsibility chain processing component performs hierarchical, top-down aggregation of the real-time evaluation results to obtain the evaluation results, which include measurement and control task evaluation conclusions and recommendations at different granularities.

7. The platform according to claim 2, characterized in that, The plan decomposition component obtains the measurement and control instruction sequence and executes the measurement and control task, wherein the corresponding process includes: The project preparation instruction is sent to each participating unit through the plan decomposition component, and the preparation status and equipment status parameters returned by each participating unit are received. Capability assessment is performed based on the preparation status and equipment status parameters to obtain the execution capability assessment result. Based on the execution capability assessment result, the action execution instruction is sent to each participating unit through the plan decomposition component according to the specific execution process of the project. The action execution instruction is used to control each participating unit to complete the measurement and control project work, and the operating status of each participating unit is obtained and evaluated. According to the project execution duration of the measurement and control task plan, the project stop instruction is sent to each participating unit at the corresponding time node.

8. The platform according to claim 1, characterized in that, It adopts a B / S architecture with front-end and back-end separation. The framework and components corresponding to the measurement and control command module and the rapid evaluation module of measurement and control tasks are deployed in the B / S architecture.

9. The platform according to claim 6, characterized in that, The structured evaluation rules are described using a JSON data structure.

10. An automated command method for space launch telemetry and control missions, characterized in that, include: The first data transceiver engine sends measurement and control commands to each participating unit of the measurement and control system, driving the measurement and control system to perform measurement and control joint debugging or actual combat tasks, and sends the measurement and control commands to the measurement and control task rapid evaluation module. The system accesses task data sent by each participating unit of the measurement and control system through the second data transceiver engine, performs measurement and control task process evaluation according to the measurement and control task scenario corresponding to the current measurement and control command, and generates evaluation results. The evaluation results are then pushed to the measurement and control command module. The measurement and control command module sends the next measurement and control command based on the evaluation results.

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