Satellite structural member inspection planning, actual measurement and recording method and system

Abstract

The invention provides a satellite structural member inspection planning, actual measurement and recording method and system, and the method comprises the steps: S1, extracting the marking information of a three-dimensional model, and forming an inspection record table; the inspection record table comprises an inspection plan; s2, detecting the structural member of the three-dimensional model based on the inspection plan of the inspection record table to obtain actual information; and S3, recording the actual information into the inspection record table, integrating to obtain an integrated data packet, and uploading the integrated data packet to a target system. According to the method, the three-dimensional model is taken as the center, scenes such as inspection planning, auxiliary measurement and actual measurement value recording related to the satellite structural member inspection process are developed based on the three-dimensional model, paperless inspection process is realized, and the working efficiency is improved.

Description

Technical Field

[0001] The present invention belongs to the technical field of product digital detection, and specifically, relates to a satellite structural component inspection planning, actual measurement and recording method and system, and more specifically, to a satellite structural component inspection planning, actual measurement and recording method and system based on a three-dimensional model. Background Art

[0002] Satellite structural parts are the basis of satellite structures. The main links of current satellite structural parts processing and inspection are: process personnel carry out process design based on 3D models, and at the same time select and copy the annotation information on the 3D model to form an inspection planning record sheet; after the structural parts processing is completed, the inspection personnel carry out physical measurement of the structural parts according to the 3D model and the inspection planning record sheet and record the measured data on the record sheet; after completing the actual measurement and recording, the inspection personnel upload the measured data to the data packet system.

[0003] By analyzing the above links, it was found that the links such as copying inspection annotations from the 3D model to other tables to form an inspection plan record sheet, reading data from measuring instruments and equipment to fill in the record sheet, and uploading measured data to the data packet system are inefficient and prone to errors.

[0004] At present, there is no patent that integrates the inspection planning, measurement and recording of relevant structural parts based on three-dimensional models.

[0005] Specifically, patent document CN104636559A discloses a method for inspecting aircraft parts using a three-dimensional inspection model. The solution quickly dimensions the geometric features of the parts, creates attribute names according to the dimensioning feature type and creates all inspection characteristic numbers at one time, and supplements the definition of the dimensioning feature attribute names and deletes the inspection characteristic numbers according to the inspection requirements. By selecting one of the dimensioning features, all inspection characteristic numbers, dimensioning feature attribute names, and dimension information are obtained. Finally, all dimensioning features and inspection characteristic number features and other information are exported in the form of an XML file. The XML file is used to generate an inspection plan, which changes the traditional mode of generating inspection information on a two-dimensional drawing from three-dimensional design model information and further generating an inspection plan, and realizes the combination of three-dimensional inspection models and inspection plans for aircraft part inspection, reduces the workload of formulating part inspection plans, and improves the reliability of inspection work.

[0006] However, this solution fails to solve the problem of integrating the inspection planning, measurement and recording of related structural parts based on the three-dimensional model.

[0007] Specifically, in the existing technology, the difficulty of integrating inspection planning, measurement and recording lies in:

[0008] 1. The existing technology cannot automatically batch extract all the annotation information on the 3D model to quickly assist process personnel in inspection planning; the so-called inspection planning refers to determining which annotation information needs to be inspected, the inspection order of each annotation information, and the inspection tools used, etc., and sometimes there are dozens or even hundreds of annotation information on the 3D model. Process personnel can only click on the annotation information on the 3D model one by one, determine the information that needs to be inspected, and then record the annotation information in another table. This makes it easy to miss a certain annotation information or extract a certain annotation information repeatedly.

[0009] 2. The existing technology has not achieved the integration of inspection tools and computers. The actual measured values ​​generated by the inspection tools need to be manually filled in on a paper or electronic record sheet, which is inefficient and prone to errors.

[0010] 3. In the prior art, since the ID of the annotation of the three-dimensional model is not explicitly displayed, the annotation information extracted in the record table also does not have the unique ID information of the annotation; when there are annotation information with the same value, it is impossible to tell which one on the three-dimensional model the annotation belongs to, which further causes misdetection or misrecording.

[0011] 4. The existing technology does not realize the integration of the record sheet and the product data package system. The completed record sheet needs to be manually uploaded to the data package system, which is inefficient.

[0012] In summary, this problem needs to be solved urgently. Summary of the invention

[0013] In view of the defects in the prior art, the purpose of the present invention is to provide a satellite structural component inspection planning, measurement and recording method and system.

[0014] A satellite structural component inspection planning, measurement and recording method provided by the present invention includes:

[0015] Step S1: extracting the annotation information of the three-dimensional model to form an inspection record table; the inspection record table includes an inspection plan;

[0016] Step S2: Based on the inspection plan in the inspection record table, inspect the structural parts of the three-dimensional model to obtain actual information;

[0017] Step S3: Record the actual information into the inspection record table, and then integrate to obtain an integrated data package, and upload it to the target system.

[0018] Preferably, the step S1 includes:

[0019] Step S1.1: extract all annotation information of the 3D model;

[0020] Step S1.2: Based on the task objective and the annotation information, an inspection record table is formed;

[0021] Step S1.3: saving the inspection record table in the three-dimensional model;

[0022] The annotation information includes basic dimensions, dimensional tolerances and geometric tolerances.

[0023] Preferably, in the step S1.1, it is determined whether the annotation information contains tolerances. If yes, the annotation information is displayed; if no, the tolerances are calculated by using preset values ​​of the software; the tolerances include dimensional tolerances and geometric tolerances;

[0024] In the step S2, it includes:

[0025] Step S2.1: Read the inspection plan of the inspection record table in the three-dimensional model;

[0026] Step S2.2: Based on the inspection plan, highlight the corresponding three-dimensional annotation to obtain a highlighted prompt;

[0027] Step S2.3: Based on the highlighted prompt, detect the structural parts of the three-dimensional model to obtain actual information;

[0028] The highlighted prompt is used to confirm the position to be measured.

[0029] Preferably, in step S3, it is determined whether the actual information as the measured value meets the design requirements of the structural parts of the three-dimensional model. If the result is yes, the actual information is recorded in the inspection record table, and then integrated to obtain an integrated data package, which is uploaded to the target system; if the result is no, the actual information is recorded in the inspection record table, and then integrated to obtain an integrated data package, which is uploaded to the target system and a rework or repair order or a scrap order for the part is issued.

[0030] A satellite structural component inspection planning, measurement and recording system provided according to the present invention includes: a structural component annotation extraction and planning module and a structural component measurement and recording module;

[0031] Instructing the structural component annotation extraction and planning module to extract annotation information of the three-dimensional model to form an inspection record table; the inspection record table includes an inspection plan;

[0032] The structural component measurement and recording module is instructed to record the actual information of the structural components of the three-dimensional model into the inspection record table based on the inspection plan of the inspection record table, and then integrate the information to obtain an integrated data package, and upload the integrated data package to the target system.

[0033] Preferably, the structural component annotation extraction and planning module includes:

[0034] Module M1.1: Extract all annotation information of the 3D model;

[0035] Module M1.2: Based on the task objectives and the annotation information, an inspection record sheet is formed;

[0036] Module M1.3: saving the inspection record sheet in the three-dimensional model;

[0037] The annotation information includes basic dimensions, dimensional tolerances and geometric tolerances;

[0038] Preferably, in the module M1.1, it is determined whether the annotation information contains tolerances. If yes, the annotation information is displayed; if no, the tolerances are calculated by using the preset values ​​of the software; the tolerances include dimensional tolerances and geometric tolerances;

[0039] The structural component annotation extraction and planning module includes:

[0040] Module M2.1: Read the inspection plan of the inspection record sheet in the 3D model;

[0041] Module M2.2: Based on the inspection plan, highlight the corresponding three-dimensional annotation to obtain a highlighted prompt;

[0042] Module M2.3: Based on the highlighted prompt, detect the structural parts of the three-dimensional model to obtain actual information;

[0043] The highlighted prompt is used to confirm the position to be measured.

[0044] Preferably, in the structural part measurement and recording module, it is determined whether the actual information as the measured value meets the design requirements of the structural parts of the three-dimensional model. If the result is yes, the actual information is recorded in the inspection record table, and then integrated to obtain an integrated data package, which is uploaded to the target system; if the result is no, the actual information is recorded in the inspection record table, and then integrated to obtain an integrated data package, which is uploaded to the target system and a rework or scrap order for the part is issued.

[0045] According to a computer-readable storage medium storing a computer program provided by the present invention, when the computer program is executed by a processor, the steps of the satellite structural component inspection planning, measurement and recording method are implemented.

[0046] An electronic device provided according to the present invention includes a memory, a processor, and a computer program stored in the memory and executable on the processor. When the computer program is executed by the processor, the steps of the satellite structural component inspection planning, measurement, and recording method are implemented.

[0047] Compared with the prior art, the present invention has the following beneficial effects:

[0048] 1. The present invention takes the three-dimensional model as the center, and carries out the inspection planning, auxiliary measurement and actual value recording related to the satellite structural parts inspection process based on the three-dimensional model, so as to realize the paperless inspection process and improve work efficiency.

[0049] 2. The present invention realizes the integration of electronic measuring instruments and computers, and the integration of the system and the data packet system, thereby improving the efficiency of data transmission and transfer, while ensuring the stability and correctness of the data.

[0050] 3. The present invention realizes the inspection dimension planning and measured value recording on the three-dimensional model of the structural part, and because the present invention realizes the data packet system integration, the paperless degree and the efficiency of data recording and transmission are improved. The present invention is also applicable to the field of structural part inspection in various industries. BRIEF DESCRIPTION OF THE DRAWINGS

[0051] Other features, objects and advantages of the present invention will become more apparent from the detailed description of non-limiting embodiments made with reference to the following drawings:

[0052] Figure 1 A schematic diagram of the system composition provided by the present invention;

[0053] Figure 2 A schematic diagram of the dimension information extraction and inspection planning page provided by the present invention;

[0054] Figure 3 A schematic diagram of the geometric tolerance information extraction and inspection planning page provided by the present invention;

[0055] Figure 4 A schematic diagram of the dimension measurement, recording and interpretation page provided by the present invention;

[0056] Figure 5 This is a schematic diagram of the inspection planning process provided by the present invention. DETAILED DESCRIPTION

[0057] The present invention is described in detail below in conjunction with specific embodiments. The following embodiments will help those skilled in the art to further understand the present invention, but are not intended to limit the present invention in any form. It should be noted that, for those of ordinary skill in the art, several changes and improvements can also be made without departing from the concept of the present invention. These all belong to the protection scope of the present invention.

[0058] The present invention solves the above problems by taking the three-dimensional model of the structural part as the core, i.e. the central body, and performing secondary development of the three-dimensional software and integrating the inspection tools and computers, the three-dimensional software and the data package. The main points are:

[0059] 1. The present invention automatically extracts all annotation information on the structural parts and displays them in a dialog box through secondary development of the 3D model software. The dialog box displays the annotation's unique ID, basic value, tolerance value and other information. The annotation information in the dialog box can be linked with the 3D annotation on the 3D model, and the corresponding 3D annotation on the 3D model can be highlighted when a certain annotation information in the dialog box is displayed.

[0060] Mark and check the specific 3D mark corresponding to the mark on the 3D model and make inspection plan by considering other factors, that is, determine whether the mark needs to be inspected and which tool needs to be used for inspection; finally, all the selected mark information forms an inspection record table and is saved in the 3D model.

[0061] 2. The present invention adopts a detection tool with digital functions, and connects the detection tool to the computer through a data cable; when inspecting the structural parts, the inspector uses 3D software to open the 3D model of the structural parts and opens the inspection record sheet planned and saved on the 3D model, checks the position of a certain mark on the model in the record sheet, and uses the inspection tool to measure the actual structural parts. After the measurement is completed, the measured data is automatically uploaded to the measured value record cell corresponding to the mark in the inspection record sheet of the 3D model. The software also compares and judges the measured value and the design value, and automatically gives a conclusion on whether the measured value meets the design requirements.

[0062] 3. The present invention develops a function to realize the integration of three-dimensional software and data package system. When all inspection plans are inspected and recorded, all information in the inspection record table is integrated into the data package system through the integrated function.

[0063] A satellite structural component inspection planning, measurement and recording system provided by the present invention includes:

[0064] The structural part annotation extraction and planning module reads the 3D model of the structural part containing the 3D annotation, extracts the dimension annotation and geometric tolerance annotation on the 3D model and displays them on one page. The process personnel plan all or part of the annotations to form the inspection record requirements of the structural part and save them in the 3D model.

[0065] After the processing of the structural parts is completed, the inspector uses the structural parts measurement and recording module to open the three-dimensional model containing the inspection plan annotations, and uses electronic measuring tools to measure the actual size or form and position tolerances of the structural parts in the order of the inspection plan. The electronic measuring tools are directly connected to the computer and directly transmit the measured values ​​back to the inspection record table of the three-dimensional model. After all the inspection plan measurements are completed, the module and the data package are integrated, and the record table belonging to the structural part is found according to the number and name of the structural part, and the corresponding measured values ​​are integrated into the table.

[0066] In view of the problems of inefficiency and error in the structural parts inspection process, the purpose of the present invention is to provide a satellite structural parts inspection planning, measurement and recording system, which can realize various satellite structural parts inspection tasks centered on the three-dimensional model of the satellite structural parts and integrated with electronic measuring instruments and data packet systems, thereby improving the efficiency and accuracy of satellite structural parts inspection.

[0067] In other words, a satellite structural component inspection planning, measurement and recording system provided according to the present invention includes two main modules: a structural component annotation extraction and inspection planning module, and a structural component measurement and recording module;

[0068] The structural part annotation extraction and inspection planning module is used to extract all annotation information from the structural part model containing 3D annotations and plan and select all or part of the annotation information to form a planning table that needs to be inspected, and save the inspection planning table in the 3D model;

[0069] The structural parts measurement and recording module includes two main functions: auxiliary measurement of the actual dimensions of structural parts and recording of the actual dimensions of structural parts;

[0070] The structural parts measurement and recording module is used to assist inspection personnel in carrying out physical measurements of structural parts and directly save the measured values ​​measured by electronic measuring instruments into the inspection record table in the three-dimensional model. After all the measurements are completed, the module is integrated with the data package and the inspection record table containing the measured values ​​is uploaded to the data package system.

[0071] The structural part annotation extraction and inspection planning module includes structural part inspection information planning, that is, the process engineer plans the actual measurement dimensions and geometric tolerances according to the part design requirements and forms an inspection information planning table;

[0072] The inspection information planning table refers to the inspection information planning table formed by the process engineer checking all or part of the dimensions and geometric tolerances in the dimension and geometric tolerance display box according to relevant regulations and his own experience;

[0073] The dimension and geometric tolerance display frame displays information including all dimensions and geometric tolerances extracted from the three-dimensional model of the structural part.

[0074] The structural part annotation extraction and inspection planning module is used to extract the three-dimensional annotation information of the structural parts and display it in a dialog box;

[0075] The three-dimensional annotation information of the structural part includes basic dimensions and tolerance values, and design values ​​of geometric tolerances; the three-dimensional annotation information display of the structural part includes the annotation information actually extracted and the dimension tolerance values ​​calculated by default tolerances;

[0076] The dimension tolerance value calculated by the default tolerance means that if the dimension annotation does not have a tolerance marked, the software will use the default tolerance specified for the part to calculate the tolerance value for the dimension.

[0077] In other words, the structural part annotation extraction and inspection planning module includes two main functions: structural part 3D model annotation information extraction and inspection information planning.

[0078] Among them: Extracting 3D annotation information of structural parts means extracting annotations such as dimension annotations and geometric tolerance annotations on the 3D model and displaying them in the dialog box. The displayed information includes the design basic value and tolerance value of the dimension, and the design value of the geometric tolerance. If the dimension annotation does not have a tolerance, the software will calculate the tolerance value of the dimension with the default tolerance specified for the part;

[0079] In other words, it is determined whether the annotation information is annotated with tolerances. If yes, the annotation information is displayed; if no, the annotation information includes basic dimensions, dimensional tolerances, and geometric tolerances.

[0080] Specifically, for dimension annotation, the basic dimension and tolerance value of the dimension annotation can be obtained during extraction. If only the basic dimension value is obtained during extraction without the tolerance value or the tolerance value is 0, it is considered that the dimension annotation has no annotation tolerance.

[0081] The inspection information planning table is stored in the three-dimensional model and circulates along with the three-dimensional model.

[0082] Specifically, the three-dimensional software provides an interface for secondary development, which can save customized information such as the inspection information planning table described in the present invention in the three-dimensional model, and can also read and display the inspection information planning table through the interface provided by the software.

[0083] Inspection information planning refers to the dimensions and behavioral tolerances that need to be actually measured and planned by the process engineer in order to ensure that the final processed parts meet the design requirements. The process engineer checks all or part of the dimensions and geometric tolerances in the dimension and geometric tolerance display box according to relevant regulations and his own experience to form an inspection information planning table. The inspection information planning table is saved in the 3D model and circulated to the inspector along with the 3D model.

[0084] The structural parts measurement and recording module includes two main functions: auxiliary measurement of the actual dimensions of structural parts and recording of the actual dimensions of structural parts;

[0085] The auxiliary measurement of the actual size of the structural parts means that the inspector opens the inspection information planning table in the 3D model and clicks the dimensions or geometric tolerances in the planning table in sequence. The corresponding annotations of the clicked dimensions or geometric tolerances in the 3D model will be highlighted synchronously, and the auxiliary inspector will know the location of the information to be inspected on the physical parts and carry out the measurement;

[0086] In other words, the above steps are implemented through the software system process as follows;

[0087] First, the inspection information planning table in the three-dimensional model is read, and the information of the inspection information planning table is displayed in a dialog box;

[0088] Furthermore, according to the characteristics of the linkage between the record information in the inspection information planning table and the three-dimensional annotation, clicking on the record information in the inspection information planning table will highlight the three-dimensional annotation on the three-dimensional model so that the three-dimensional annotation corresponding to the record information can be known;

[0089] Finally, by checking the positions of the 3D annotations on the 3D model, we can know the specific positions of the points, lines, and surfaces that need to be measured on the physical model, so that we can carry out inspections at the corresponding positions on the physical object, and the information obtained from the inspection is the actual information.

[0090] The actual test measurement record of the structural parts refers to the process in which the inspector uses electronic inspection instruments to measure the size or form and position tolerance of the structural parts, and directly transmits the measured results to the three-dimensional model inspection information record table by connecting the electronic inspection instruments and computers. The software will compare the measured values ​​with the design values ​​and give a conclusion on whether they are in compliance, and automatically record the conclusion in the inspection information record table. After all the measurements and records are completed, the module integrates the inspection record information into the data package system through integration with the data package to form the final record.

[0091] The three-dimensional model inspection information recording table refers to a table for recording actual measurement information created according to the inspection information planning table;

[0092] The recorded information includes dimension name, dimension design value, dimension actual value and conclusion information;

[0093] The data package refers to the final collection of data information delivered after the product is completed.

[0094] Figure 1 The present invention is a schematic diagram of the satellite structural component inspection planning, measurement and recording system.

[0095] The system is implemented based on the secondary development of 3D design software, and includes two main modules: structural part annotation extraction and inspection planning module, and structural part measurement and recording module. Each of them is explained below.

[0096] The structural part annotation extraction and inspection planning module is used to extract the dimension and geometric tolerance information marked on the three-dimensional model of the structural part, and select all or part of the dimension and geometric tolerance information to form an inspection planning record table. The formed inspection planning record table prepares for the inspection measurement link. Dimension information extraction and inspection planning, such as Figure 2 As shown in Figure 2, geometric tolerance information extraction and inspection planning, such as Figure 3 shown.

[0097] The structural parts measurement and recording module is used to assist inspectors in measuring and recording structural parts. Inspectors use electronic measuring instruments to measure structural parts according to the size and geometric tolerance sequence of the inspection record sheet. The measured values ​​are directly integrated and fed back into the inspection record sheet in the 3D model. The system records the measured values ​​and determines whether they meet the design requirements. After all records are completed, the inspection record sheet is integrated into the data package system.

[0098] Specifically, if the measured value is within the tolerance range, the requirement is met; if the measured value is outside the tolerance range, the requirement is not met.

[0099] For example: the basic dimension is 10 and the tolerance is ±0.2. If the measured result is 10.1, it meets the design requirements, because (10-0.2)≤10.1≤(10+0.2); if the measured value is 10.3, it does not meet the design requirements, because 10.3 is not between 9.8 and 10.2.

[0100] In other words, it is determined whether the actual information as the measured value meets the design requirements. If the result is yes, the actual information is recorded in the inspection record table, and then integrated to obtain an integrated data package, which is uploaded to the target system; if the result is no, the inspection record is integrated and uploaded to the data package and the target system, and a rework or scrap order for the part is issued;

[0101] Dimension measurement, recording and interpretation page Figure 4 shown.

[0102] The measured records are integrated into the data packet system page, as shown in Table 1.

[0103] Table 1 shows the page information of the measured records integrated into the data packet system.

[0104] Table 1

[0105]

[0106] In summary, the satellite structural parts inspection planning, measurement and recording system provided by the present invention can realize the integrated realization of structural parts inspection planning, measurement and recording based on three-dimensional models, improve the degree of paperless operation, and improve work efficiency and the accuracy of data transmission.

[0107] The present invention also provides a satellite structural component inspection planning, measurement and recording system, which can be implemented by executing the process steps of the satellite structural component inspection planning, measurement and recording method, that is, technical personnel in this field can understand the satellite structural component inspection planning, measurement and recording method as a preferred implementation mode of the satellite structural component inspection planning, measurement and recording system.

[0108] A satellite structural component inspection planning, measurement and recording system provided according to the present invention includes: a structural component annotation extraction and planning module and a structural component measurement and recording module;

[0109] Instructing the structural component annotation extraction and planning module to extract annotation information of the three-dimensional model to form an inspection record table; the inspection record table includes an inspection plan;

[0110] The structural component measurement and recording module is instructed to record the actual information of the structural components of the three-dimensional model into the inspection record table based on the inspection plan of the inspection record table, and then integrate the information to obtain an integrated data package, and upload the integrated data package to the target system.

[0111] Those skilled in the art know that, in addition to realizing the system and its various devices, modules, and units provided by the present invention in a purely computer-readable program code, it is entirely possible to realize the same functions in the form of logic gates, switches, application-specific integrated circuits, programmable logic controllers, and embedded microcontrollers by logically programming the method steps. Therefore, the system and its various devices, modules, and units provided by the present invention can be considered as a hardware component, and the devices, modules, and units included therein for realizing various functions can also be regarded as structures within the hardware component; the devices, modules, and units for realizing various functions can also be regarded as both software modules for realizing the method and structures within the hardware component.

[0112] The above describes the specific embodiments of the present invention. It should be understood that the present invention is not limited to the above specific embodiments, and those skilled in the art can make various changes or modifications within the scope of the claims, which does not affect the essence of the present invention. In the absence of conflict, the embodiments of the present application and the features in the embodiments can be combined with each other arbitrarily.

Claims

1. A satellite structural component inspection planning, measurement and recording method, characterized in that: include: Step S1: extracting the annotation information of the three-dimensional model to form an inspection record table; The inspection record sheet includes an inspection plan; Step S2: Based on the inspection plan in the inspection record table, inspect the structural parts of the three-dimensional model to obtain actual information; Step S3: Record the actual information into the inspection record table, and then integrate to obtain an integrated data package, and upload it to the target system.

2. The satellite structural component inspection planning, measurement and recording method according to claim 1, characterized in that: In the step S1, it includes: Step S1.1: extract all annotation information of the 3D model; Step S1.2: Based on the task objective and the annotation information, an inspection record table is formed; Step S1.3: saving the inspection record table in the three-dimensional model; The annotation information includes basic dimensions, dimensional tolerances and geometric tolerances.

3. The satellite structural component inspection planning, measurement and recording method according to claim 2, characterized in that: In the step S1.1, it is determined whether the annotation information includes a tolerance, and if so, the annotation information is displayed; If the answer is no, the tolerance is calculated using the preset value of the software; The tolerance includes dimensional tolerance and geometric tolerance; In the step S2, it includes: Step S2.1: Read the inspection plan of the inspection record table in the three-dimensional model; Step S2.2: Based on the inspection plan, highlight the corresponding three-dimensional annotation to obtain a highlighted prompt; Step S2.3: Based on the highlighted prompt, detect the structural parts of the three-dimensional model to obtain actual information; The highlighted prompt is used to confirm the position to be measured.

4. The satellite structural component inspection planning, measurement and recording method according to claim 1, characterized in that: In the step S3, it is determined whether the actual information as the measured value meets the design requirements of the structural parts of the three-dimensional model. If yes, the actual information is recorded in the inspection record table, and then integrated to obtain an integrated data package, which is uploaded to the target system. If the result is no, the actual information is recorded in the inspection record table, and then integrated to obtain an integrated data package, which is uploaded to the target system and a rework or repair order or a cancellation order for the part is issued.

5. A satellite structural component inspection planning, measurement and recording system, characterized in that: include: Structural parts annotation extraction and planning module and structural parts measurement and recording module; Instructing the structural component annotation extraction and planning module to extract annotation information of the three-dimensional model to form an inspection record table; The inspection record sheet includes an inspection plan; The structural component measurement and recording module is instructed to record the actual information of the structural components of the three-dimensional model into the inspection record table based on the inspection plan of the inspection record table, and then integrate the information to obtain an integrated data package, and upload the integrated data package to the target system.

6. The satellite structural component inspection planning, measurement and recording system according to claim 5, characterized in that: The structural component annotation extraction and planning module includes: Module M1.1: Extract all annotation information of the 3D model; Module M1.2: Based on the task objectives and the annotation information, an inspection record sheet is formed; Module M1.3: saving the inspection record sheet in the three-dimensional model; The annotation information includes basic dimensions, dimensional tolerances and geometric tolerances.

7. The satellite structural component inspection planning, measurement and recording system according to claim 6, characterized in that: In the module M1.1, it is determined whether the annotation information includes a tolerance, and if so, the annotation information is displayed; If the answer is no, the tolerance is calculated using the preset value of the software; The tolerance includes dimensional tolerance and geometric tolerance; The structural component annotation extraction and planning module includes: Module M2.1: Read the inspection plan of the inspection record sheet in the 3D model; Module M2.2: Based on the inspection plan, highlight the corresponding three-dimensional annotation to obtain a highlighted prompt; Module M2.3: Based on the highlighted prompt, detect the structural parts of the three-dimensional model to obtain actual information; The highlighted prompt is used to confirm the position to be measured.

8. The satellite structural component inspection planning, measurement and recording system according to claim 5, characterized in that: In the structural component measurement and recording module, it is determined whether the actual information as the measured value meets the design requirements of the structural component of the three-dimensional model. If yes, the actual information is recorded in the inspection record table, and then integrated to obtain an integrated data package, which is uploaded to the target system; If the result is no, the actual information is recorded in the inspection record table, and then integrated to obtain an integrated data package, which is uploaded to the target system and a rework or repair order or a cancellation order for the part is issued.

9. A computer-readable storage medium storing a computer program, characterized in that: When the computer program is executed by a processor, the steps of the satellite structural component inspection planning, measurement and recording method described in any one of claims 1 to 4 are implemented.

10. An electronic device comprising a memory, a processor, and a computer program stored in the memory and executable on the processor, wherein: When the computer program is executed by a processor, the steps of the satellite structural component inspection planning, measurement and recording method described in any one of claims 1 to 4 are implemented.

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