Product matching management method and system for satellite full life cycle
By creating a satellite product code resource library and establishing a unified supporting transmission interface, the problems of interface incompatibility and low efficiency in the supporting management during the satellite development process were solved, realizing efficient and standardized supporting management throughout the entire satellite life cycle, and improving development efficiency and quality.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- SHANGHAI SATELLITE ENG INST
- Filing Date
- 2026-01-28
- Publication Date
- 2026-06-05
AI Technical Summary
In the current technology, the supporting management during the satellite development process suffers from problems such as incompatible digital system interfaces, low development efficiency, and poor data consistency, and lacks a unified management solution for the entire life cycle.
This paper provides a product support management method and system for the entire life cycle of satellites. By creating a satellite product code resource library, it gradually refines and automatically transfers supporting information, establishes a unified supporting transmission interface, and realizes full life cycle management from overall design to final assembly.
It has achieved data consistency throughout the entire lifecycle, improving the efficiency and quality of satellite development and realizing efficient operation and integrated quality management of the development process.
Smart Images
Figure CN122154060A_ABST
Abstract
Description
Technical Field
[0001] This invention relates to the field of satellite design and manufacturing, and more specifically, to a product support management method and system for the entire life cycle of a satellite. Background Technology
[0002] With the development of aerospace technology, spacecraft development is characterized by system complexity, a large number of supporting products, and diverse technical statuses. Almost all technical and management information is presented based on these supporting products. Currently, the management of supporting products in satellite development is carried out through a combination of "digital systems" and "documents," which presents numerous problems. For example, the lack of interoperability between digital system interfaces between upstream and downstream development units leads to the inability to transfer supporting information; incompatibility between supporting products in digital systems and development processes results in low development efficiency; and the lack of source correlation between supporting products in digital systems and documents leads to repetitive manual work and poor data consistency.
[0003] Therefore, there is an urgent need for a product support management solution covering the entire life cycle of satellites to address the current shortcomings in support management during the development process.
[0004] Patent document CN107016446A discloses a method for managing the equipment of manned spacecraft. This method manages manned spacecraft equipment according to subsystems and modules, including spare parts and their status requirements within the management scope. It also details any changes to the equipment at each development stage. While this patent document represents a general and widely used method for equipment management in spacecraft development, it does not propose a specific implementation. This differs fundamentally from the design, transfer, and management of satellite product equipment throughout its entire lifecycle, which is achieved through a digital system, as proposed in this invention.
[0005] Patent document CN107016153 discloses a weight control method for manned spacecraft systems based on a supporting system. This patent document relates to a supporting system for manned spacecraft, which includes equipment support, cable support, direct component support, pipeline support, standard component support, and thermal control material support, thus incorporating components ranging from large-scale cabin structures to small screws and fasteners. This patent document establishes the supporting system through a classification method, but does not provide a specific implementation form and is only applicable to weight assessment during the spacecraft final assembly phase. In contrast, this invention is a product support management method applicable to the entire lifecycle from overall design to final assembly, and provides a digital implementation scheme, fundamentally different from the method proposed in this patent document.
[0006] Patent document CN107644295B discloses a design and closed-loop management system and method for technical requirements of various stages of spacecraft AIT (Autonomous In-Process) technology. This system includes a basic library module for technical status requirements at each stage, a management element maintenance and management module, a module for designing and managing technical status requirements at each stage, a field technical status management module, and a summary statistical analysis module. This improves the efficiency of spacecraft development, significantly reduces administrative work, lowers human resource costs, standardizes the AIT process status establishment process, and realizes the proceduralization and standardization of various technical status information, thereby improving the efficiency of AIT process status establishment, querying, field confirmation, and management. While this patent document is applicable to the design and closed-loop management of technical requirements at each stage of spacecraft AIT, this invention is applicable to product support management throughout the entire lifecycle of satellites. Technical requirements are only a small part of product support, and AIT is only a small stage in the entire lifecycle; therefore, the applicable objects and stages of the two are fundamentally different.
[0007] Patent document CN116629483A discloses a satellite AIT structured design and data management system and its implementation method and system, including: an AIT design module, a data transmission module, a status acquisition module, and an application analysis module; the AIT design module is used to define the structured data of satellite AIT; the data transmission module is used to transmit the satellite AIT structured data defined by the AIT design module to the downstream manufacturing end in the form of stage task packages for satellite final assembly and integration, and the downstream manufacturing end transmits the recorded on-site implementation status data back to the overall satellite; the status acquisition module is used by the downstream manufacturing end to collect and record on-site implementation status data according to the data feedback requirements specified in the stage task packages; the application analysis module is used to compare and analyze the defined satellite AIT structured data and implementation status data, as well as other AIT scenario application analyses. This patent document focuses on the satellite AIT process and solves the design, issuance, and final assembly implementation data acquisition and feedback of structured technical requirements. In contrast, this invention provides a supporting management method and system for the entire life cycle from overall satellite design to final assembly completion, which is a supporting management based on the satellite development process. The applicable stages and objects of the two are fundamentally different.
[0008] Design and Application of Spacecraft Thermal Test Supporting Device Management Platform [1] Wang Runze, Hou Yaqin, Shu Chengshun, et al. Design and Application of Spacecraft Thermal Test Supporting Device Management Platform [J]. Computer Applications, 2018, 38(A02):331-333. This article proposes a spacecraft thermal test supporting device management platform. The platform uses the object relational mapping method to construct a thermal test tooling database, solves the thermal test tooling management problem, provides design ideas for thermal test tooling designers in tooling development, and improves the continuous utilization capability of thermal test tooling. However, this article is only applicable to the management of thermal test tooling support, and the two are fundamentally different. Summary of the Invention
[0009] To address the shortcomings of existing technologies, the purpose of this invention is to provide a product support management method and system for the entire lifecycle of satellites.
[0010] A product support management method for the entire lifecycle of a satellite, provided by the present invention, includes: Step S1: Create a satellite product code resource library and define satellite product names and codes; Step S2: Generate satellite initial design support and satellite initial production support based on the satellite product code resource library, and distribute them to the satellite rapid design system and the planning management system respectively; Step S3: Conduct detailed satellite configuration in the satellite rapid design system, expand to form detailed satellite design support, and further obtain detailed production support, which is then distributed to the AIT status management system and the planning management system respectively. Step S4: Perform satellite AIT configuration in the AIT status management system to form satellite assembly design support, and send it to the assembly data packet system; Step S5: Configure the process in the final assembly data package system and add the final assembly implementation results to form a complete satellite final assembly process.
[0011] Preferably, step S2 includes the following sub-steps: Step S2.1: Based on the product name, product code, subsystem name and code in the satellite product code resource library, add information on the quantity of accessories, whether it is a type range, and whether it is a complete set to form the initial design accessories for the satellite; Step S2.2: Based on the initial satellite design and supporting equipment, after adding information on the research and development unit, product characteristics, and production quantity, the initial satellite production and supporting equipment is formed; Step S2.3: Distribute the initial satellite design to the satellite rapid design system to carry out detailed satellite configuration; Step S2.4: Issue the initial satellite production support documents to the planning and management system.
[0012] Preferably, step S3 includes the following sub-steps: Step S3.1: Based on the initial satellite design kit, create models of all satellite products in the satellite rapid design system, carry out detailed satellite design, and form a detailed satellite design kit; Step S3.2: Based on the detailed satellite design and supporting equipment, add information on the product types, characteristics, and production quantities of the complete kits to form the detailed satellite production and supporting equipment. Step S3.3: Distribute the detailed satellite design to the AIT status management system to initiate satellite AIT design; Step S3.4: Send the detailed satellite production support information to the planning and management system.
[0013] Preferably, step S3.1 includes the following sub-steps: Step S3.1.1: For the complete sets of equipment in the initial design of the satellite, carry out detailed design of the complete sets of equipment to generate detailed design kits; Step S3.1.2: For the non-component kits and the detailed design kits of the satellite initial design kits, expand and add product codes, types, tag numbers, model names and whether they are critical components to form the satellite detailed design kits.
[0014] Preferably, changes to product accessories throughout the satellite's entire lifecycle are initiated at the corresponding step at the source of the change information.
[0015] According to the present invention, a product support management system for the entire lifecycle of satellites includes: Module M1: Creates a satellite product code resource library, defining satellite product names and codes; Module M2: Generates satellite initial design support and satellite initial production support based on the satellite product code resource library, and distributes them to the satellite rapid design system and the planning management system respectively; Module M3: Conducts detailed satellite configuration in the satellite rapid design system, expands to form detailed satellite design support, and further obtains detailed production support, which is then distributed to the AIT status management system and the planning management system respectively. Module M4: Performs satellite AIT configuration in the AIT status management system, forms satellite assembly design support, and distributes data packets to the assembly data package system; Module M5: Performs process configuration in the final assembly data package system and adds final assembly implementation results to form satellite final assembly process support.
[0016] Preferably, module M2 includes the following sub-modules: Module M2.1: Based on the product name, product code, subsystem name and code in the satellite product code resource library, add information on the quantity of accessories, whether it is a type range, and whether it is a complete set to form the initial design accessories for the satellite; Module M2.2: Based on the initial satellite design support, after adding information on the research and development unit, product characteristics, and production quantity, it forms the initial satellite production support. Module M2.3: Distribute the initial satellite design to the satellite rapid design system to carry out detailed satellite configuration; Module M2.4: Distributes the initial satellite production support to the planning and management system.
[0017] Preferably, module M3 includes the following sub-modules: Module M3.1: Based on the initial satellite design kit, create models of all satellite products in the satellite rapid design system, carry out detailed satellite design, and form a detailed satellite design kit; Module M3.2: Based on the detailed satellite design and supporting system, after adding information on the product types, characteristics, and production quantities of the complete kits, a detailed satellite production and supporting system is formed. Module M3.3: Distribute the detailed satellite design to the AIT status management system to initiate satellite AIT design; Module M3.4: Distributes detailed satellite deployment specifications to the planning and management system.
[0018] Preferably, module M3.1 includes the following sub-modules: Module M3.1.1: For the complete sets of equipment in the initial design of the satellite, carry out detailed design of the complete sets of equipment and generate detailed design kits for the complete sets of equipment; Module M3.1.2: For the detailed design kits of satellite initial design kits, both non-kits and kits are expanded by adding product codes, types, tag numbers, model names, and whether they are critical components, thus forming the detailed design kits for satellites.
[0019] Preferably, changes to product accessories throughout the satellite's entire lifecycle are initiated in the corresponding module at the source of the change information.
[0020] Compared with the prior art, the present invention has the following beneficial effects: 1. This invention enables the entire lifecycle of supporting data to originate from a single source: the product code. The supporting information for each stage is gradually refined and automatically transferred layer by layer as the development progresses, ensuring that the supporting information for the products is from the same source, consistent, and standardized, thus effectively improving the efficiency and quality of satellite development.
[0021] 2. This invention is based on the supporting management of the satellite development process. It establishes a unified supporting transmission interface with external systems (satellite rapid design system, planning management system, AIT status management system, final assembly data packet system, etc.), realizing a high-efficiency development mode that integrates technical collaboration, quality supervision, and planning control.
[0022] 3. This invention provides a comprehensive management method and system for the entire lifecycle of a satellite, from overall design to final assembly. Data is transferred and refined at each stage, achieving integrated quality and planning management for the satellite development process, and effectively improving the development efficiency and quality of the satellite throughout its entire lifecycle. Attached Figure Description
[0023] Other features, objects, and advantages of the present invention will become more apparent from the following detailed description of non-limiting embodiments with reference to the accompanying drawings: Figure 1This is a flowchart of the method of the present invention.
[0024] Figure 2 This is a system composition diagram of the present invention.
[0025] In the picture: Satellite Product Code Resource Library Module 1 Satellite Initial Support Module 2 Satellite Detailed Supporting Module 3 Satellite assembly and supporting module 4 Detailed Implementation The present invention will now be described in detail with reference to specific embodiments. These embodiments will help those skilled in the art to further understand the present invention, but do not limit the invention in any way. It should be noted that those skilled in the art can make several changes and improvements without departing from the concept of the present invention. These all fall within the protection scope of the present invention.
[0026] Reference Figure 1 As shown, a product support management method for the entire lifecycle of a satellite includes: Step S1: Create a satellite product code resource library and define satellite product names and codes; Step S2: Generate satellite initial design support and satellite initial production support based on the satellite product code resource library, and distribute them to the satellite rapid design system and the planning management system respectively; Step S3: Conduct detailed satellite configuration in the satellite rapid design system, expand to form detailed satellite design support, and further obtain detailed production support, which is then distributed to the AIT status management system and the planning management system respectively. Step S4: Perform satellite AIT configuration in the AIT status management system to form satellite assembly design support, and send it to the assembly data packet system; Step S5: Configure the process in the final assembly data package system and add the final assembly implementation results to form a complete satellite final assembly process.
[0027] In one embodiment, the above steps include: Step S1: Determine the product code for the satellite's overall design and create a satellite product code resource library; Step S2: Create satellite initial design support and production support, and distribute them to the satellite rapid design system and the project management system respectively; Step S3: Conduct detailed satellite design in the satellite rapid design system, expand to form a detailed satellite design package, and then plan a detailed production package, which is then distributed to the AIT status management system and the planning management system respectively. Step S4: Conduct satellite AIT design in the AIT status management system to form satellite assembly design support and distribute it to the assembly data packet system; Step S5: Conduct process design in the final assembly data package system and add final assembly implementation results to form a complete satellite final assembly process.
[0028] Step S1 supports multiple satellite models sharing the same product code in the same resource library. That is, a brand new satellite product code resource library can be created, or an existing product code in the resource library can be directly referenced.
[0029] Step S2 specifically includes the following sub-steps: Step S2.1: Based on the product name, product code, and the name and code of the subsystem in the product code resource library, add information such as the matching quantity, whether it is a product series, and whether it is a complete set to form the initial design matching; Step S2.2: Based on the initial design, add information such as the research and development unit, product characteristics (formal prototype, initial prototype, qualification prototype, electrical components, structural components, thermal control components, etc.), and production quantity to form the initial production support; Step S2.3: Distribute the initial design to the satellite rapid design system to facilitate the detailed design of the satellite; Step S2.4: Issue the initial production support to the planning and management system to facilitate the initial production of satellite products.
[0030] Step S3 specifically includes the following sub-steps: Step S3.1: Based on the initial design kit, create models of all satellite products in the satellite rapid design system, carry out detailed satellite design, and form the satellite detailed design kit: Step S3.2: Based on the detailed design, add information such as product type, characteristics (sample, prototype, qualification sample, electrical components, structural components, thermal control components, etc.), and production quantity of the complete kit to form a detailed production kit for the satellite; Step S3.3: Distribute the detailed design to the AIT status management system to facilitate satellite AIT design; Step S3.4: Detailed production support information is distributed to the planning and management system to facilitate subsequent tracking of satellite product production.
[0031] Step S3.1 includes the following sub-steps: Step S3.1.1 For the kits in the initial design package, carry out detailed design of the kits to generate detailed design package of the kits; Step S3.1.2 For the non-component kits and component kits in the initial design kit, expand and add information such as product code, type, tag number, model name, and whether it is a critical component to form the satellite detailed design kit; Step S4 involves conducting satellite AIT design within the AIT status management system. This primarily targets the detailed design and adds design requirements related to final assembly, including batch number, fastening, anti-loosening, grounding, insulation, installation accuracy, weighing, covering, and thermal conductivity requirements.
[0032] Step S5 involves satellite process design in the final assembly data package system. This mainly targets thermal control products and directly affiliated parts of the final assembly. After the process design is carried out, detailed process specifications are added, including product name, code, batch number, and other information.
[0033] Step S5 adds the final assembly implementation results to the final assembly data package system. This mainly involves adding corresponding measurement results from the actual implementation of the final assembly requirements in the final assembly design to prove whether the requirements are met.
[0034] For any changes to product specifications throughout the satellite's lifecycle, the changes must be initiated at the source of the change information, following the steps outlined at that source. For example, changes to product names and codes must be initiated in step S1.
[0035] The present invention also provides a product support management system for the entire life cycle of satellites. The product support management system for the entire life cycle of satellites can be implemented by executing the process steps of the product support management method for the entire life cycle of satellites. That is, those skilled in the art can understand the product support management method for the entire life cycle of satellites as a preferred embodiment of the product support management system for the entire life cycle of satellites.
[0036] Specifically, a product support management system for the entire lifecycle of satellites includes: Module M1: Creates a satellite product code resource library, defining satellite product names and codes; Module M2: Generates satellite initial design support and satellite initial production support based on the satellite product code resource library, and distributes them to the satellite rapid design system and the planning management system respectively; Module M3: Conducts detailed satellite configuration in the satellite rapid design system, expands to form detailed satellite design support, and further obtains detailed production support, which is then distributed to the AIT status management system and the planning management system respectively. Module M4: Performs satellite AIT configuration in the AIT status management system, forms satellite assembly design support, and distributes data packets to the assembly data package system; Module M5: Performs process configuration in the final assembly data package system and adds final assembly implementation results to form satellite final assembly process support.
[0037] Module M2 includes the following sub-modules: Module M2.1: Based on the product name, product code, subsystem name and code in the satellite product code resource library, add information on the quantity of accessories, whether it is a type range, and whether it is a complete set to form the initial design accessories for the satellite; Module M2.2: Based on the initial satellite design support, after adding information on the research and development unit, product characteristics, and production quantity, it forms the initial satellite production support. Module M2.3: Distribute the initial satellite design to the satellite rapid design system to carry out detailed satellite configuration; Module M2.4: Distributes the initial satellite production support to the planning and management system.
[0038] The module M3 includes the following sub-modules: Module M3.1: Based on the initial satellite design kit, create models of all satellite products in the satellite rapid design system, carry out detailed satellite design, and form a detailed satellite design kit; Module M3.2: Based on the detailed satellite design and supporting system, after adding information on the product types, characteristics, and production quantities of the complete kits, a detailed satellite production and supporting system is formed. Module M3.3: Distribute the detailed satellite design to the AIT status management system to initiate satellite AIT design; Module M3.4: Distributes detailed satellite deployment specifications to the planning and management system.
[0039] The module M3.1 includes the following sub-modules: Module M3.1.1: For the complete sets of equipment in the initial design of the satellite, carry out detailed design of the complete sets of equipment and generate detailed design kits for the complete sets of equipment; Module M3.1.2: For the detailed design kits of satellite initial design kits, both non-kits and kits are expanded by adding product codes, types, tag numbers, model names, and whether they are critical components, thus forming the detailed design kits for satellites.
[0040] Throughout the satellite's entire lifecycle, product-related changes are initiated at the corresponding module based on the source of the change information.
[0041] Example 1 like Figure 2 As shown, a product support management system for the entire lifecycle of a satellite includes: Satellite Product Code Resource Library Module 1: Use the satellite product code resource library to define satellite product names and codes as the basis for satellite supporting design; Satellite Initial Support Module 2: Satellite Initial Support Module 2 includes two sub-modules: Design Support and Production Support. It retrieves product name and basic code information from the product code resource library, uses the Design Support sub-module for planning to obtain the initial design support, and uses the Production Support sub-module for planning to obtain the initial production support. The results are then sent to the satellite rapid design system and the planning management system. Satellite Detailed Support Module 3: Satellite Detailed Support Module 3 includes two sub-modules: Design Support and Production Support. It obtains basic product design information from the satellite rapid design system, uses the Design Support sub-module for planning to obtain detailed design support, and uses the Production Support sub-module for planning to obtain detailed production support. The results are then sent to the satellite AIT status management system. Satellite Assembly Support Module 4: Satellite Assembly Support Module 4 includes two sub-modules: Design Support and Process Support. It obtains basic satellite assembly design information from the AIT status management system, uses the Design Support sub-module for planning to obtain the assembly design support, sends the results to the assembly data package system, and then uses the Process Support sub-module for planning to obtain the assembly process support after integrating the assembly measured information.
[0042] Those skilled in the art will understand that, besides implementing the system and its various devices, modules, and units provided by this invention in the form of purely computer-readable program code, the same functions can be achieved entirely through logical programming of the method steps, making the system and its various devices, modules, and units of this invention function in the form of logic gates, switches, application-specific integrated circuits, programmable logic controllers, and embedded microcontrollers. Therefore, the system and its various devices, modules, and units provided by this invention can be considered as a hardware component, and the devices, modules, and units included therein for implementing various functions can also be considered as structures within the hardware component; alternatively, the devices, modules, and units for implementing various functions can be considered as both software modules implementing the method and structures within the hardware component.
[0043] Specific embodiments of the present invention have been described above. It should be understood that the present invention is not limited to the specific embodiments described above, and those skilled in the art can make various changes or modifications within the scope of the claims, which do not affect the essence of the present invention. Unless otherwise specified, the embodiments and features described in this application can be arbitrarily combined with each other.
Claims
1. A product support management method for the entire lifecycle of satellites, characterized in that, include: Step S1: Create a satellite product code resource library and define satellite product names and codes; Step S2: Generate satellite initial design support and satellite initial production support based on the satellite product code resource library, and distribute them to the satellite rapid design system and the planning management system respectively; Step S3: Conduct detailed satellite configuration in the satellite rapid design system, expand to form detailed satellite design support, and further obtain detailed production support, which is then distributed to the AIT status management system and the planning management system respectively. Step S4: Perform satellite AIT configuration in the AIT status management system to form satellite assembly design support, and send it to the assembly data packet system; Step S5: Configure the process in the final assembly data package system and add the final assembly implementation results to form a complete satellite final assembly process.
2. The product support management method for the entire lifecycle of satellites according to claim 1, characterized in that, Step S2 includes the following sub-steps: Step S2.1: Based on the product name, product code, subsystem name and code in the satellite product code resource library, add information on the quantity of accessories, whether it is a type range, and whether it is a complete set to form the initial design accessories for the satellite; Step S2.2: Based on the initial satellite design and supporting equipment, after adding information on the research and development unit, product characteristics, and production quantity, the initial satellite production and supporting equipment is formed; Step S2.3: Distribute the initial satellite design to the satellite rapid design system to carry out detailed satellite configuration; Step S2.4: Issue the initial satellite production support documents to the planning and management system.
3. The product support management method for the entire lifecycle of satellites according to claim 2, characterized in that, Step S3 includes the following sub-steps: Step S3.1: Based on the initial satellite design kit, create models of all satellite products in the satellite rapid design system, carry out detailed satellite design, and form a detailed satellite design kit; Step S3.2: Based on the detailed satellite design and supporting equipment, add information on the product types, characteristics, and production quantities of the complete kits to form the detailed satellite production and supporting equipment. Step S3.3: Distribute the detailed satellite design to the AIT status management system to initiate satellite AIT design; Step S3.4: Send the detailed satellite production support information to the planning and management system.
4. The product support management method for the entire lifecycle of satellites according to claim 2, characterized in that, Step S3.1 includes the following sub-steps: Step S3.1.1: For the complete sets of equipment in the initial design of the satellite, carry out detailed design of the complete sets of equipment to generate detailed design kits; Step S3.1.2: For the non-component kits and the detailed design kits of the satellite initial design kits, expand and add product codes, types, tag numbers, model names and whether they are critical components to form the satellite detailed design kits.
5. The product support management method for the entire lifecycle of satellites according to claim 1, characterized in that, Changes to product accessories throughout the satellite's entire lifecycle are initiated at the corresponding step based on the source of the change information.
6. A product support management system for the entire lifecycle of satellites, characterized in that, include: Module M1: Creates a satellite product code resource library, defining satellite product names and codes; Module M2: Generates satellite initial design support and satellite initial production support based on the satellite product code resource library, and distributes them to the satellite rapid design system and the planning management system respectively; Module M3: Conducts detailed satellite configuration in the satellite rapid design system, expands to form detailed satellite design support, and further obtains detailed production support, which is then distributed to the AIT status management system and the planning management system respectively. Module M4: Performs satellite AIT configuration in the AIT status management system, forms satellite assembly design support, and distributes data packets to the assembly data package system; Module M5: Performs process configuration in the final assembly data package system and adds final assembly implementation results to form satellite final assembly process support.
7. The product support management system for the entire lifecycle of satellites according to claim 6, characterized in that, Module M2 includes the following sub-modules: Module M2.1: Based on the product name, product code, subsystem name and code in the satellite product code resource library, add information on the quantity of accessories, whether it is a type range, and whether it is a complete set to form the initial design accessories for the satellite; Module M2.2: Based on the initial satellite design support, after adding information on the research and development unit, product characteristics, and production quantity, it forms the initial satellite production support. Module M2.3: Distribute the initial satellite design to the satellite rapid design system to carry out detailed satellite configuration; Module M2.4: Distributes the initial satellite production support to the planning and management system.
8. The product support management system for the entire lifecycle of satellites according to claim 7, characterized in that, The module M3 includes the following sub-modules: Module M3.1: Based on the initial satellite design kit, create models of all satellite products in the satellite rapid design system, carry out detailed satellite design, and form a detailed satellite design kit; Module M3.2: Based on the detailed satellite design and supporting system, after adding information on the product types, characteristics, and production quantities of the complete kits, a detailed satellite production and supporting system is formed. Module M3.3: Distribute the detailed satellite design to the AIT status management system to initiate satellite AIT design; Module M3.4: Distributes detailed satellite deployment specifications to the planning and management system.
9. The product support management system for the entire lifecycle of satellites according to claim 7, characterized in that, The module M3.1 includes the following sub-modules: Module M3.1.1: For the complete sets of equipment in the initial design of the satellite, carry out detailed design of the complete sets of equipment and generate detailed design kits for the complete sets of equipment; Module M3.1.2: For the detailed design kits of satellite initial design kits, both non-kits and kits are expanded by adding product codes, types, tag numbers, model names, and whether they are critical components, thus forming the detailed design kits for satellites.
10. The product support management system for the entire lifecycle of satellites according to claim 6, characterized in that, Throughout the satellite's entire lifecycle, product-related changes are initiated at the corresponding module based on the source of the change information.