Spacecraft wrist strap type intelligent wearable device data extraction method and system

Abstract

The invention belongs to the technical field of data transmission, and provides a data extraction method and system for a wristband type intelligent wearable device of a spacecraft, and the method comprises the steps: obtaining a key information selection request inputted into the wristband type intelligent wearable device; after the target wired transmission instrument equipment is in wired connection with the wrist strap type intelligent wearable equipment, spacecraft general assembly measurement data corresponding to the general assembly implementation state recording item is extracted; recording spacecraft general assembly measurement data into a target actual measurement item record table, and storing the target actual measurement item record table into a wearable end record table database; and when the wrist strap type intelligent wearable device is in wired connection with the management server, updating the server-side record table database according to the target actual measurement item record table to obtain a spacecraft general assembly implementation state record table. According to the scheme provided by the invention, the recording efficiency of the final assembly implementation state is improved, and the accuracy and reliability of the final assembly implementation state recording link are improved.

Description

Technical Field

[0001] The present invention relates to the technical field of data transmission, and in particular to a method and system for extracting data of a spacecraft wristband type intelligent wearable device. Background Art

[0002] During the overall assembly process of a spacecraft, the implementation status records cover numerous key tables, which play a crucial role in quality confirmation. The data types recorded in the tables are rich, including general assembly measurement data such as resistance measurement, geometric dimension measurement, torque measurement, and general assembly actual operation data such as compliance confirmation.

[0003] At present, there are obvious defects in the acquisition methods of general assembly measurement data, mainly relying on manual reading, collection and transmission. This process needs to go through multiple links such as "measurement, reading, and recording" at the general assembly site. Due to the intervention of human factors, the error probability increases significantly.

[0004] At the same time, the work of recording the implementation status of general assembly also faces many difficulties. Currently, it is mainly completed manually by inspectors and mainly in the form of paper records, which leads to the data in various tables being scattered, lacking systematicness and integration. In terms of data transmission, it is necessary to copy the paper records one by one into an electronic spreadsheet. This process is not only inefficient but also seriously restricts subsequent data analysis, comparison and confirmation work, and cannot meet the requirements of high-precision and high-efficiency data management for spacecraft general assembly. Summary of the Invention

[0005] The present invention provides a method and system for extracting data of a spacecraft wristband type intelligent wearable device to solve the defects of time-consuming, laborious and low reliability in the traditional general assembly implementation status recording link.

[0006] On the one hand, the present invention provides a method for extracting data of a spacecraft wristband type intelligent wearable device, including: Obtaining a key information selection request for the input wristband type intelligent wearable device, where the key information includes general assembly implementation status record items and product unique identifiers; After the target wired transmission instrument device is wired to the wristband type intelligent wearable device, extracting the spacecraft general assembly measurement data corresponding to the general assembly implementation status record items in the target wired transmission instrument device; Recording the spacecraft general assembly measurement data into a target actual measurement item record table, and storing the target actual measurement item record table into the wearable end record table database; When the wristband type intelligent wearable device is wired to the management server, updating the server-side record table database according to the target actual measurement item record table to obtain a spacecraft general assembly implementation status record table.

[0007] According to the method for extracting data of the spacecraft wristband - type intelligent wearable device provided by the present invention, extract the spacecraft general assembly measurement - type data corresponding to the general assembly implementation status record items in the target wired transmission instrument and equipment, including: If the general assembly implementation status record items include geometric dimensions and torque, extract the single - time real - time measurement data corresponding to geometric dimensions and torque respectively; If the general assembly implementation status record items include grounding resistance value, extract the maximum resistance value within the set acquisition time; If the general assembly implementation status record items include insulation resistance value, extract the minimum resistance value within the set acquisition time; If the general assembly implementation status record items include heating circuit resistance value and thermistor resistance value, extract the average resistance value within the set acquisition time.

[0008] According to the method for extracting data of the spacecraft wristband - type intelligent wearable device provided by the present invention, the server - side record table database is established through the following process: Establish a structure tree with the field, spacecraft model, and general assembly initial record table as the layer structure; Import multiple general assembly initial record tables corresponding to multiple spacecraft models into the corresponding structure tree. Among them, the multiple general assembly initial record tables contain preset items and measured items. The content of the preset items has been filled, and the content of the measured items is to be filled; Perform format conversion on the general assembly initial record tables in the structure tree to generate the server - side record table database.

[0009] According to the method for extracting data of the spacecraft wristband - type intelligent wearable device provided by the present invention, the general assembly initial record table includes: instrument and equipment installation record table, thermistor plug - in record table, heating circuit plug - in record table, and multi - layer thermal insulation component installation record table.

[0010] According to the method for extracting data of the spacecraft wristband - type intelligent wearable device provided by the present invention, the method further includes: When the management server is wired - connected to the wristband - type intelligent wearable device, update the wearable - end record table database according to at least part of the updated data in the server - side record table database.

[0011] According to the method for extracting data of the spacecraft wristband - type intelligent wearable device provided by the present invention, the method further includes: When the management server receives a general assembly implementation status data processing request initiated by a user, in response to the general assembly implementation status data processing request, retrieve and display at least part of the target data in the server - side record table database; Among them, the general assembly implementation status data processing requests include: general assembly implementation status data browsing requests, general assembly implementation status data retrieval requests, general assembly implementation status data online confirmation requests, and general assembly implementation status data structured control requests.

[0012] On the other hand, the present invention also provides a data extraction system for a spacecraft wristband type intelligent wearable device, including: a wired transmission instrument device and a wristband type intelligent wearable device; The wired transmission instrument device is used to obtain spacecraft general assembly measurement data; The wristband type intelligent wearable device is used to receive a key information selection request, where the key information includes general assembly implementation status record items and product unique identifiers; after the target wired transmission instrument device is wiredly connected to the wristband type intelligent wearable device, extract the spacecraft general assembly measurement data corresponding to the general assembly implementation status record items in the target wired transmission instrument device; record the spacecraft general assembly measurement data in a target actual measurement item record form, and store the target actual measurement item record form in a wearable end record form database; the wristband type intelligent wearable device is also used to be wiredly connected to a management server, so that the management server updates a server-side record form database according to the target actual measurement item record form to obtain a spacecraft general assembly implementation status record form.

[0013] According to the data extraction system for a spacecraft wristband type intelligent wearable device provided by the present invention, the wristband type intelligent wearable device includes: a miniaturized smart phone, a wrist base frame, and a wristband; The miniaturized smart phone is detachably installed on the wrist base frame, and the wrist base frame is fixedly connected to the wristband.

[0014] According to the data extraction system for a spacecraft wristband type intelligent wearable device provided by the present invention, the miniaturized smart phone includes: a touch screen display module, a keyboard input module, an OTG data transmission module, and a data processing module; The touch screen display module, the keyboard input module, and the OTG data transmission module are all connected to the data processing module.

[0015] According to the data extraction system for a spacecraft wristband type intelligent wearable device provided by the present invention, the wired transmission instrument device includes: a wired transmission micro-ohmmeter, a wired transmission digital multimeter, a wired transmission digital vernier caliper, a wired transmission digital depth gauge, and a wired transmission digital torque wrench; The wired transmission micro-ohmmeter is used to measure the grounding resistance value in the spacecraft general assembly measurement data; The wired transmission digital multimeter is used to measure the insulation resistance value, the thermistor resistance value, the heating circuit resistance value, etc. in the spacecraft general assembly measurement data; The wired transmission digital display vernier caliper is used to measure the length in the measurement data of spacecraft general assembly measurement; The wired transmission digital display depth gauge is used to measure the depth in the measurement data of spacecraft general assembly measurement; The wired transmission digital display torque wrench is used to measure the torque in the measurement data of spacecraft general assembly measurement.

[0016] The method and system for extracting data of the spacecraft wristband type intelligent wearable device provided by the present invention, by obtaining a key information selection request including the general assembly implementation status record items and the product unique identifier input into the wristband type intelligent wearable device; after the target wired transmission instrument device is wiredly connected to the wristband type intelligent wearable device, extracting the spacecraft general assembly measurement data corresponding to the general assembly implementation status record items in the target wired transmission instrument device; recording the spacecraft general assembly measurement data into the target actual measurement item record table, and storing the target actual measurement item record table into the wearable end record table database; when the wristband type intelligent wearable device is wiredly connected to the management server, updating the server end record table database according to the target actual measurement item record table to obtain the spacecraft general assembly implementation status record table. Since in the general assembly implementation status recording link, the wristband type intelligent wearable device is used to automatically extract the relevant data in the wired transmission instrument device, the recording efficiency of the general assembly implementation status is improved, the error caused by human intervention is reduced, and the accuracy and reliability of the general assembly implementation status recording link are improved. Brief Description of the Drawings

[0017] In order to more clearly illustrate the technical solutions in the present invention or the prior art, the following will briefly introduce the drawings required for use in the description of the embodiments or the prior art. Obviously, the drawings in the following description are some embodiments of the present invention. For those of ordinary skill in the art, without creative efforts, other drawings can also be obtained based on these drawings.

[0018] Figure 1 It is a schematic flowchart of the method for extracting data of the spacecraft wristband type intelligent wearable device provided by the embodiment of the present invention; Figure 2 It is a schematic structural diagram of the system for extracting data of the spacecraft wristband type intelligent wearable device provided by the embodiment of the present invention; Figure 3 It is a schematic structural diagram of the wristband type intelligent wearable device. Detailed Embodiments

[0019] To make the objectives, technical solutions and advantages of the present invention clearer, the following will, in conjunction with the accompanying drawings in the present invention, clearly and completely describe the technical solutions in the present invention. Apparently, the described embodiments are some, but not all, of the embodiments of the present invention. All other embodiments obtained by those of ordinary skill in the art based on the embodiments in the present invention without making creative efforts shall fall within the scope of protection of the present invention.

[0020] The following will Figures 1 to 3 describe in detail the solutions of the method and system for extracting data of the spacecraft wristband-type intelligent wearable device provided by the embodiments of the present invention.

[0021] Figure 1 is a schematic flowchart of the method for extracting data of the spacecraft wristband-type intelligent wearable device provided by the embodiments of the present invention.

[0022] As Figure 1 shown, the method for extracting data of the spacecraft wristband-type intelligent wearable device provided by the embodiments of the present invention mainly includes the following steps: Step 110: Obtain a key information selection request for the input wristband-type intelligent wearable device, where the key information includes the general assembly implementation status record items and the product unique identifier.

[0023] In practical applications, the general assembly inspector can enter the username and password on the wristband-type intelligent wearable device to log in to the software system. Then, the inspector can sequentially select the field, spacecraft model, and target record form by touching the screen. After that, the inspector can further select the product unique identifier to be recorded and the general assembly implementation status record items to be recorded by touching the screen, and the general assembly implementation status record items can be selected in a hierarchical manner.

[0024] In this embodiment, taking the target record form as the heating circuit plug-in record form as an example, the selected product unique identifier is specifically the heater code.

[0025] Step 120: After the target wired transmission instrument device is wiredly connected to the wristband-type intelligent wearable device, extract the spacecraft general assembly measurement data corresponding to the general assembly implementation status record items in the target wired transmission instrument device.

[0026] In practical applications, after selecting the product unique identifier and the general assembly implementation status record items, the spacecraft general assembly measurement data can be recorded based on wired transmission. Specifically, according to the selected general assembly implementation status record items, the corresponding target wired transmission instrument device can be connected to the wristband-type intelligent wearable device through a data transmission line, and a adapter can be configured for wired connection if necessary.

[0027] Step 130: Record the spacecraft general assembly measurement data in the target actual measurement item record form, and store the target actual measurement item record form in the wearable end record form database.

[0028] When the wristband type intelligent wearable device triggers the recording function of the wired transmission instrument and equipment through touch, the spacecraft general assembly measurement data of the wired transmission instrument and equipment can be automatically extracted into the cells corresponding to the unique product identifier and the general assembly implementation status record item in the actual measurement item record form.

[0029] Taking the heating circuit plug-in record form as an example, the record items include the heating circuit resistance value and the insulation resistance value. The wired transmission instrument and equipment corresponding to the measurement of the heating circuit resistance value and the insulation resistance value are both wired transmission digital multimeters.

[0030] After the wristband type intelligent wearable device completes the general assembly implementation status record, the obtained target actual measurement item record form will be stored in the wearable end record form database.

[0031] Step 140: When the wristband type intelligent wearable device is wired-connected to the management server, update the server-side record form database according to the target actual measurement item record form to obtain the spacecraft general assembly implementation status record form.

[0032] It can be understood that when the wristband type intelligent wearable device is wired-connected to the management server, the server-side record form database can be updated based on the target actual measurement item record form previously stored in the wearable end record form database to generate the spacecraft general assembly implementation status record form.

[0033] The solution provided in this embodiment can realize the automatic extraction of spacecraft general assembly measurement data through wired transmission, and then obtain the spacecraft general assembly implementation status record form, realizing the automatic extraction and accurate record of data related to the spacecraft general assembly implementation status.

[0034] In one embodiment, extracting the spacecraft general assembly measurement data corresponding to the general assembly implementation status record item in the target wired transmission instrument and equipment specifically includes: If the general assembly implementation status record item includes geometric dimensions and torque, the single real-time measurement data corresponding to the geometric dimensions and torque are respectively extracted.

[0035] If the general assembly implementation status record item includes the grounding resistance value, the maximum resistance value within the set acquisition time is extracted.

[0036] If the general assembly implementation status record item includes the insulation resistance value, the minimum resistance value within the set acquisition time is extracted.

[0037] If the general assembly implementation status record item includes the heating circuit resistance value and the thermistor resistance value, the average resistance value within the set acquisition time is extracted.

[0038] It is understandable that for different types of spacecraft assembly measurement data, the extraction methods of spacecraft assembly measurement data are also different. In this embodiment, the extraction methods of spacecraft assembly measurement data specifically include: extracting single - time real - time measurement data, extracting maximum measurement data, extracting minimum measurement data, and extracting average measurement data.

[0039] Specifically, when extracting geometric dimensions (such as length or depth) and torque, the method of extracting single - time real - time measurement data is adopted. When extracting grounding resistance values, the method of extracting maximum measurement data is adopted. Specifically, after setting the acquisition time and acquisition frequency, the maximum resistance value within the acquisition time can be automatically extracted. When extracting insulation resistance values, the method of extracting minimum measurement data can be adopted. Specifically, after setting the acquisition time and acquisition frequency, the minimum resistance value within the acquisition time can be automatically extracted. When extracting the resistance values of heating circuits and thermistors, the method of extracting average measurement data can be adopted. Specifically, after setting the acquisition time and acquisition frequency, the average resistance value within the acquisition time can be automatically extracted.

[0040] In practical applications, the maximum measurement data, minimum measurement data, and average measurement data can be specifically collected in the following ways: The wrist - band type intelligent wearable device initiates a real - time data request through touch control; the wired transmission instrument and equipment returns corresponding real - time data at regular intervals according to the acquisition frequency; when the configured acquisition time arrives, an end - data - acquisition request is automatically sent to the wired transmission instrument and equipment; the real - time data returned by the wired transmission instrument and equipment is subjected to corresponding logical processing according to the request parameters (i.e., maximum measurement data, minimum measurement data, and average measurement data), and the processing results are automatically returned to the software system of the wrist - band type intelligent wearable device.

[0041] In some embodiments, the single - time real - time measurement data can be collected in the following ways: The wrist - band type intelligent wearable device initiates a result - data request through touch control; after parsing and processing the result data returned by the wired transmission instrument and equipment, it is automatically returned to the software system of the wrist - band type intelligent wearable device.

[0042] In one embodiment, the server record - table database is specifically established through the following process: First, a structure tree is established with the field, spacecraft model, and general - assembly initial record - table as the hierarchical structure.

[0043] In this embodiment, a tree object can be created first, and then the root node can be added. Next, domain nodes are added as child nodes of the root node, then spacecraft model nodes are added to each domain node, and finally the general assembly initial record form nodes are added to each spacecraft model node. In practical applications, the list contents of domains, spacecraft models, and general assembly initial record forms can be modified according to actual requirements.

[0044] Then, multiple general assembly initial record forms corresponding to multiple spacecraft models are imported into the corresponding structure tree. Among them, the multiple general assembly initial record forms contain preset items and measured items. The contents of the preset items have been filled in, and the contents of the measured items are to be filled in.

[0045] In practical applications, after the management server logs in to the software system, a new model can be established under the corresponding domain, and multiple general assembly initial record forms such as the instrument and equipment installation record form, thermistor plug-in record form, heating circuit plug-in record form, and multi-layer insulation component installation record form of this model are imported under the structure tree of the corresponding model.

[0046] In this embodiment, the general assembly initial record form specifically includes: instrument and equipment installation record form, thermistor plug-in record form, heating circuit plug-in record form, and multi-layer insulation component installation record form.

[0047] It can be understood that the item types of each general assembly initial record form include both preset items and measured items. The preset items are the data preset before the general assembly implementation. The preset items of each record form should include a unique product identifier. The measured items are the process data recorded by the general assembly inspection personnel during the general assembly implementation process. In practical applications, the preset items and measured items can be managed hierarchically as needed.

[0048] Taking the heating circuit plug-in record form as an example, the preset items mainly include heater code, heater name, and heater design resistance value, etc. The unique product identifier is the heater code. The first level of the measured items includes the detection before the heater is connected to the cable network and the detection after the heater is connected to the cable network. Among them, the second level of the detection before the heater is connected to the cable network includes the heating circuit resistance value, insulation resistance value, and circuit confirmation. The third level of the detection after the heater is connected to the cable network includes the heating circuit resistance value, insulation resistance value, connection method, and connection confirmation.

[0049] Finally, the format of the general assembly initial record form in the structure tree is converted to generate the server-side record form database.

[0050] After the data import is completed, the general assembly initial record form can be automatically formatted according to specific rules in the management server to generate the server-side record form database.

[0051] For example, when the initial assembly record form adopts the CSV format and the server-side record form database adopts the MySQL format, specific rules may include data conversion rules such as data type conversion for certain fields and rearrangement of field order.

[0052] In one embodiment, the above-mentioned method for extracting data from the spacecraft wristband intelligent wearable device may further include: When the management server is wired to the wristband intelligent wearable device, update the wearable-end record form database based on at least some of the updated data in the server-side record form database.

[0053] In this embodiment, when the management server is wired to the wristband intelligent wearable device, the wearable-end record form database can be updated according to the updated data in the server-side record form database to achieve data synchronization between the two record form databases.

[0054] In one embodiment, the above-mentioned method for extracting data from the spacecraft wristband intelligent wearable device may further include: When the management server receives a request for processing the general assembly implementation status data initiated by the user, in response to the request for processing the general assembly implementation status data, retrieve and display at least some of the target data in the server-side record form database.

[0055] Among them, the request for processing the general assembly implementation status data includes: a request for browsing the general assembly implementation status data, a request for retrieving the general assembly implementation status data, a request for online confirmation of the general assembly implementation status data, and a request for structured control of the general assembly implementation status data.

[0056] It can be understood that the management server can support services for browsing, quickly retrieving, online confirming, and structured controlling the general assembly implementation status data for users.

[0057] In some embodiments, the management server can display some of the general assembly implementation status data corresponding to the retrieval keyword to the user according to the retrieval keyword in the request for retrieving the general assembly implementation status data. Specifically, the retrieval keyword can be key information such as product name, product code, and pasting position.

[0058] In practical applications, the management server can display the confirmation information to the user with corresponding permissions according to the item to be confirmed in the request for online confirmation of the general assembly implementation status data. For example, when the general assembly task is completed or reaches a specific stage, the item to be confirmed at this time is the confirmation of the task progress. The management server can send the task progress confirmation information to the general assembly inspection personnel for online confirmation by the general assembly inspection personnel. In addition, the item to be confirmed can also be confirmation items such as quality confirmation and data specification confirmation.

[0059] In summary, the method for extracting data of the spacecraft wristband - type intelligent wearable device provided by the embodiment of the present invention uses a wristband - type intelligent wearable device in cooperation with a wired transmission instrument device, and automatically extracts data directly from the wired transmission instrument device based on the wired transmission method. By using an intelligent and digital implementation method, it can free the hands of the general assembly inspection personnel, improve the efficiency of recording the general assembly implementation status, reduce the occupation of manpower, and enhance the accuracy of recording general assembly measurement - type data.

[0060] Based on the same general inventive concept, the present invention also protects a system for extracting data of a spacecraft wristband - type intelligent wearable device. The system for extracting data of the spacecraft wristband - type intelligent wearable device provided by the present invention will be described below. The system for extracting data of the spacecraft wristband - type intelligent wearable device described below can be mutually corresponding and referred to with the method for extracting data of the spacecraft wristband - type intelligent wearable device described above.

[0061] As Figure 2 shown, the system for extracting data of the spacecraft wristband - type intelligent wearable device provided by the embodiment of the present invention specifically includes: a wired transmission instrument device 210 and a wristband - type intelligent wearable device 220.

[0062] The wired transmission instrument device 210 is used to obtain spacecraft general assembly measurement - type data.

[0063] The wristband - type intelligent wearable device 220 is used to receive a key information selection request, where the key information includes general assembly implementation status record items and product unique identifiers; after the target wired transmission instrument device is wired - connected to the wristband - type intelligent wearable device 220, it extracts the spacecraft general assembly measurement - type data corresponding to the general assembly implementation status record items in the target wired transmission instrument device; records the spacecraft general assembly measurement - type data in the target actual measurement item record form, and stores the target actual measurement item record form in the wearable - end record form database; the wristband - type intelligent wearable device 220 is also used to be wired - connected to the management server, so that the management server updates the server - end record form database according to the target actual measurement item record form to obtain a spacecraft general assembly implementation status record form.

[0064] As Figure 3 shown, the wristband - type intelligent wearable device specifically includes: a miniaturized smart phone 310, a wrist base 320, and a wristband 330.

[0065] The miniaturized smart phone 310 is detachably installed on the wrist base 320, and the wrist base 320 is fixedly connected to the wristband 330.

[0066] In some embodiments, the wrist base 320 can realize the flexible disassembly and 360° rotation function of the miniaturized smart phone 310, so as to meet the multi - angle control requirements.

[0067] In one embodiment, the miniaturized smart phone specifically includes: a touch screen display module, a keyboard input module, an OTG data transmission module, and a data processing module.

[0068] The touch screen display module, the keyboard input module, and the OTG data transmission module are all connected to the data processing module.

[0069] In this embodiment, the touch screen display module is mainly used for information input and display, allowing users to input information through the touch screen and presenting the information to the users. The keyboard input module is mainly used for users to input information by operating the keyboard, which mainly refers to a physical keyboard, such as buttons, so as to meet the multi-mode data input needs of users. The OTG data transmission module can allow a wristband-type intelligent wearable device to exchange and communicate data with a wired transmission instrument device without relying on a computer, and thus automatically extract relevant data on the wired transmission instrument device. The data processing module is mainly used to provide data analysis and data calculation services and is the core module of the miniaturized smart phone.

[0070] In one embodiment, the wired transmission instrument device specifically includes: a wired transmission digital micro-ohmmeter, a wired transmission digital multimeter, a wired transmission digital vernier caliper, a wired transmission digital depth gauge, and a wired transmission digital torque wrench.

[0071] Among them, the wired transmission digital micro-ohmmeter is used to measure the grounding resistance value in the spacecraft assembly measurement data.

[0072] The wired transmission digital multimeter is used to measure the insulation resistance value, the thermistor resistance value, the heating circuit resistance value, etc. in the spacecraft assembly measurement data.

[0073] The wired transmission digital vernier caliper is used to measure the length in the spacecraft assembly measurement data.

[0074] The wired transmission digital depth gauge is used to measure the depth in the spacecraft assembly measurement data.

[0075] The wired transmission digital torque wrench is used to measure the torque in the spacecraft assembly measurement data.

[0076] The wired transmission instrument device can transmit the assembly measurement data to the wristband-type intelligent wearable device in a wired manner.

[0077] It can be seen that this embodiment provides a data extraction system for a spacecraft wristband-type intelligent wearable device. By cooperating the wristband-type intelligent wearable device with the wired transmission instrument device, the automatic extraction and recording functions of the spacecraft assembly measurement data can be realized, the recording efficiency of the assembly implementation status is improved, the error caused by human intervention is reduced, and the accuracy and reliability of the assembly implementation status recording link are improved.

[0078] Regarding the system in the above embodiments, the specific manner in which each device performs operations has been described in detail in the embodiments related to the method, and will not be elaborated here.

[0079] Through the description of the above embodiments, those skilled in the art can clearly understand that each embodiment can be implemented by means of software plus a necessary general hardware platform, and of course, it can also be implemented by hardware. Based on this understanding, the above technical solutions, in essence, or the parts that contribute to the prior art can be embodied in the form of a computer software product, which can be stored in a computer-readable storage medium, such as ROM / RAM, magnetic disk, optical disk, etc., and includes several instructions to enable a computer device (which can be a personal computer, server, or network device, etc.) to execute the methods described in each embodiment or some parts of the embodiments.

[0080] Finally, it should be noted that the above embodiments are only used to illustrate the technical solutions of the present invention, and are not intended to limit them; although the present invention has been described in detail with reference to the foregoing embodiments, those of ordinary skill in the art should understand that they can still modify the technical solutions recorded in the foregoing embodiments, or perform equivalent replacements for some of the technical features; and these modifications or replacements do not make the essence of the corresponding technical solutions deviate from the spirit and scope of the technical solutions of the embodiments of the present invention.

Claims

1. A method for extracting data of a wristband - type intelligent wearable device for a spacecraft, characterized in that, Including: Obtaining a key information selection request of an input wrist - worn intelligent wearable device, where the key information includes general assembly implementation status record items and product unique identifiers; After the target wired transmission instrument device is wired - connected to the wrist - worn intelligent wearable device, extracting spacecraft general assembly measurement - type data corresponding to the general assembly implementation status record items in the target wired transmission instrument device; Recording the spacecraft general assembly measurement - type data into a target actual measurement item record form, and storing the target actual measurement item record form into a wearable - end record form database; When the wrist - worn intelligent wearable device is wired - connected to the management server, updating the server - end record form database according to the target actual measurement item record form to obtain a spacecraft general assembly implementation status record form.

2. The method for extracting data of the spacecraft wristband type intelligent wearable device according to claim 1, wherein, Extracting the spacecraft general assembly measurement - type data corresponding to the general assembly implementation status record items in the target wired transmission instrument device includes: If the general assembly implementation status record items include geometric dimensions and torque, respectively extracting single - time real - time measurement data corresponding to the geometric dimensions and torque; If the general assembly implementation status record items include grounding resistance values, extracting the maximum resistance value within a set acquisition time; If the general assembly implementation status record items include insulation resistance values, extracting the minimum resistance value within a set acquisition time; If the general assembly implementation status record items include heating circuit resistance values and thermistor resistance values, extracting the average resistance value within a set acquisition time.

3. The method for extracting data of the spacecraft wristband type intelligent wearable device according to claim 1, wherein The server - end record form database is established through the following process: Establishing a structure tree with the field, spacecraft model, and general assembly initial record form as the layer structure; Importing multiple general assembly initial record forms corresponding to multiple spacecraft models into the corresponding structure tree, where the multiple general assembly initial record forms contain preset items and actual measurement items, the content of the preset items has been filled, and the content of the actual measurement items is to be filled; Converting the format of the general assembly initial record form in the structure tree to generate a server - end record form database.

4. The method for extracting data of the spacecraft wristband type intelligent wearable device according to claim 3, wherein, The general assembly initial record form includes: instrument equipment installation record form, thermistor plug - in record form, heating circuit plug - in record form, and multi - layer heat insulation component installation record form.

5. The method for extracting data of the spacecraft wristband-type intelligent wearable device according to claim 1, wherein, The method further includes: When the management server is wired - connected to the wrist - worn intelligent wearable device, updating the wearable - end record form database according to at least part of the updated data in the server - end record form database.

6. The method for extracting data of the spacecraft wristband type intelligent wearable device according to claim 1, wherein, The method further includes: When the management server receives a general assembly implementation status data processing request initiated by a user, in response to the general assembly implementation status data processing request, retrieving and displaying at least part of the target data in the server - end record form database; Wherein, the general assembly implementation status data processing request includes: general assembly implementation status data browsing request, general assembly implementation status data retrieval request, general assembly implementation status data online confirmation request, and general assembly implementation status data structured control request.

7. A data extraction system for a spacecraft wristband - type intelligent wearable device, characterized in that, Including: A wired transmission instrument device and a wrist - worn intelligent wearable device; The wired transmission instrument device is used to obtain spacecraft general assembly measurement - type data; The wristband-type intelligent wearable device is used to receive a key information selection request, where the key information includes the general assembly implementation status record items and the product unique identifier; after the target wired transmission instrument device is wiredly connected to the wristband-type intelligent wearable device, extract the spacecraft general assembly measurement data corresponding to the general assembly implementation status record items in the target wired transmission instrument device; record the spacecraft general assembly measurement data into the target actual measurement item record table, and store the target actual measurement item record table into the wearable end record table database; the wristband-type intelligent wearable device is also used to be wiredly connected to the management server, so that the management server updates the server-side record table database according to the target actual measurement item record table to obtain the spacecraft general assembly implementation status record table.

8. The data extraction system for the spacecraft wristband type intelligent wearable device according to claim 7, characterized in that, The wristband-type intelligent wearable device includes: a miniaturized smartphone, a wrist chassis, and a wristband; The miniaturized smartphone is detachably installed on the wrist chassis, and the wrist chassis is fixedly connected to the wristband.

9. The spacecraft wristband-type intelligent wearable device data extraction system according to claim 8, characterized in that The miniaturized smartphone includes: a touch screen display module, a keyboard input module, an OTG data transmission module, and a data processing module; The touch screen display module, the keyboard input module, and the OTG data transmission module are all connected to the data processing module.

10. The spacecraft wristband-type intelligent wearable device data extraction system according to claim 7, characterized in that, The wired transmission instrument device includes: a wired transmission digital micro-ohmmeter, a wired transmission digital multimeter, a wired transmission digital vernier caliper, a wired transmission digital depth gauge, and a wired transmission digital torque wrench; The wired transmission digital micro-ohmmeter is used to measure the ground resistance value in the spacecraft general assembly measurement data; The wired transmission digital multimeter is used to measure the insulation resistance value, the thermistor resistance value, and the heating circuit resistance value in the spacecraft general assembly measurement data; The wired transmission digital vernier caliper is used to measure the length in the spacecraft general assembly measurement data; The wired transmission digital depth gauge is used to measure the depth in the spacecraft general assembly measurement data; The wired transmission digital torque wrench is used to measure the torque in the spacecraft general assembly measurement data.

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