CN111145444A - Spacecraft switching test tool management method, system and medium - Google Patents
Spacecraft switching test tool management method, system and medium Download PDFInfo
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- CN111145444A CN111145444A CN201911295059.7A CN201911295059A CN111145444A CN 111145444 A CN111145444 A CN 111145444A CN 201911295059 A CN201911295059 A CN 201911295059A CN 111145444 A CN111145444 A CN 111145444A
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- G—PHYSICS
- G07—CHECKING-DEVICES
- G07F—COIN-FREED OR LIKE APPARATUS
- G07F17/00—Coin-freed apparatus for hiring articles; Coin-freed facilities or services
- G07F17/10—Coin-freed apparatus for hiring articles; Coin-freed facilities or services for means for safe-keeping of property, left temporarily, e.g. by fastening the property
- G07F17/12—Coin-freed apparatus for hiring articles; Coin-freed facilities or services for means for safe-keeping of property, left temporarily, e.g. by fastening the property comprising lockable containers, e.g. for accepting clothes to be cleaned
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- G—PHYSICS
- G07—CHECKING-DEVICES
- G07F—COIN-FREED OR LIKE APPARATUS
- G07F17/00—Coin-freed apparatus for hiring articles; Coin-freed facilities or services
- G07F17/42—Coin-freed apparatus for hiring articles; Coin-freed facilities or services for ticket printing or like apparatus, e.g. apparatus for dispensing of printed paper tickets or payment cards
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Abstract
The invention provides a spacecraft switching test tool management method, which comprises the following steps: step 1: inquiring a transfer test tool; step 2: selecting a transfer test tool to be borrowed and borrowing time, opening an access grid, and acquiring the transfer test tool; and step 3: after the use is finished, scanning two-dimensional code confirmation information on the transfer test tool; and 4, step 4: and after the information is confirmed, opening the access grid, and putting the access grid into a transfer test tool to finish returning. The invention has shared storage, high utilization rate and no need of repeated production; self-help borrowing and returning are realized, and the management cost is low; the use efficiency is high when the user borrows and returns the book; the using times and the using time are counted, and the tool is checked in time, so that the safety and the reliability of the tool are ensured.
Description
Technical Field
The invention relates to the technical field of intelligent control of article storage, in particular to a method, a system and a medium for managing a spacecraft switching test tool.
Background
In general, in an aerospace assembly plant, there are typically tens of (one) to tens of (one) final assembly stations for spacecraft, corresponding to an equal number of project groups, while the proportion of final assembly and testing performed simultaneously is typically around one third, and is about a few (one) to tens of (one).
The ground test of the spacecraft depends on a switching test tool, the switching test tool mainly comprises a switching cable and a switching box, and various signals on the spacecraft can be led to ground equipment through the switching test tool to be fully tested and verified. Each project group or each spacecraft (a) is generally developed with a set of corresponding transfer testing tools, which are mainly used for final assembly and testing of the project, and the projects are generally borrowed from each other or are inconvenient to borrow. The investment of the transfer test tool is a cost which is not small, and the total investment cost is huge when each project is provided with one set of calculation.
The conventional method has the advantages that the use of the project is basically guaranteed, but under the conditions that the number of aerospace projects is increased and the design of spacecrafts is more and more complex, the old mode has more and more defects in the aspects of investment cost, response efficiency, quality management, tool completeness and the like.
Under the current situation, not only the cost is increased but also other problems are caused by putting each project into production of the testing tool, for example: 1) in the existing distributed management mode, each project only considers the test requirement of the spacecraft, so that the test tool lacks in a universal design, and a phenomenon that part of the tool is idle after the project is often finished is caused; 2) the switching test tool for one project operation cannot always completely cover the requirement of the spacecraft, the temporary operation or borrowing is time-consuming and labor-consuming, the efficiency is extremely low, and the original plan can be possibly disturbed; 3) the existing testing tools are dispersedly stored in all corners of a general assembly plant in all project groups, have no general details and positions, are very inconvenient to find and borrow, cannot quickly respond to testing requirements, cause the situation that a spacecraft waits for the testing tools to be in place often occurs, and influence the working progress; 4) the aerospace tool has higher requirement on the storage environment, but the test tool of each project is stored and managed respectively at present, and the storage environment is not uniformly guaranteed; 5) the mechanical life of the electric connector is limited by the use times, but the use times cannot be counted by the current use mode, so that the tool is easy to exceed the mechanical life limit; 6) the electric connector is used as a mechanical part which is frequently plugged and pulled, is easy to damage, is easy to generate or enter redundant objects, and causes damage to spacecraft testing, and at present, the electric connector has no quick detection means and cannot detect quality conditions in time.
Therefore, the problems of repeated production construction, no overall planning, low utilization rate, inconvenience in mutual borrowing, lack of quality guarantee and the like exist in the current method.
Before this patent is written, the search is carried out to the existing similar patent, and the search content is as follows: tool access, transfer test tool, tool management, access, self-service access, access system, loan, self-service loan, etc. Through search, the prior patents and comparison are as follows:
self-service intelligent access arrangement based on internet, patent number CN 204946190U: this patent is noted to take out through machinery is automatic, and the structure is comparatively complicated. This patent manpower is access by oneself, simple structure, and this patent is heavily underway the aerospace specialized tool's storage environment protection, self-service inspection, mobility management etc..
A self-service book borrowing and returning system and a use method thereof are disclosed in patent numbers CN 108230571A: the patent focuses on cross-region sharing, cross-region returning and the like. This patent is centralized management, for the switching test tool management of one or more adjacent space factory buildings.
A book self-help borrowing and returning method and a device thereof, and the patent number CN 101251939A: the patent is to place the book at the designated position, accords with the requirement of books management, and this patent object is switching test instrument, does not require that instrument and access grid relation are fixed, as long as the access grid that does not use all can return, has considerable flexibility, borrows still conveniently.
An access cabinet system and an access method based on RFID open self-service sharing are disclosed in patent numbers CN 107527453A: the system is based on RFID, and the system adopts the current passing two-dimensional code to identify so as to complete the borrowing, returning and other management of the transfer test tool.
A self-service intelligent access device storage grid and storage box, patent No. CN 205098823U: the patent is a design of an access box. The patent refers to the field of 'transmission of digital information'.
In view of the fact that the existing design can not meet the management requirement of a spacecraft switching test tool, a novel management system needs to be designed urgently, and a matched using method is provided to meet the current requirement.
Patent document CN109951552A (application number: 201910217090.2) discloses an intelligent storage system and an application method thereof, wherein a storage device receives an article placed by a user, a detection device detects whether the storage device has the condition of placing the article in real time, and if so, sends a placing prompt message to a control device; after receiving the first preset time for putting in the prompt message, the control device controls the intelligent storage device to move to the first preset position, and the execution mechanism controls the storage device to release the internal articles.
Disclosure of Invention
Aiming at the defects in the prior art, the invention aims to provide a spacecraft switching test tool management method, a spacecraft switching test tool management system and a spacecraft switching test tool management medium.
The spacecraft switching test tool management method provided by the invention comprises the following steps:
step 1: inquiring a transfer test tool;
step 2: selecting a transfer test tool to be borrowed and borrowing time, opening an access grid, and acquiring the transfer test tool;
and step 3: after the use is finished, scanning two-dimensional code confirmation information on the transfer test tool;
and 4, step 4: and after the information is confirmed, opening the access grid, and putting the access grid into a transfer test tool to finish returning.
Preferably, the step 1 comprises: inquiring according to the specification of the electric connector on the transfer test tool;
the query result is a list and state information of the transfer test tool;
when inquiring that the required transfer test tool is lent, selecting the lent transfer test tool, initiating a borrowing application, scanning the two-dimensional code on the transfer test tool through the image recognition device after the borrower agrees and takes the transfer test tool, reading the transfer test tool information and the borrowing information by the management system, completing the transfer after the user confirms, and automatically updating and registering the borrowing information by the management system.
Preferably, the step 2 includes: after a transfer test tool and borrowing time length are selected, the access grid sends a borrowing request, and the management system receives the borrowing request and opens the access grid;
taking out the transfer test tool, closing the access grid to complete borrowing, and automatically registering borrowing information by the management system;
when time is selected, selecting a starting point and an end point of any future time period to finish the reservation and borrowing of the transfer testing tool; starting the day before the starting point, and carrying out the reserved prompt by the management system;
when a plurality of transfer testing tools are borrowed, the selected transfer testing tools are sequentially placed into the storage vehicle, and when borrowing is selected, the transfer testing tools are sequentially taken out from the storage grids, so that batch borrowing is completed.
Preferably, the step 3 comprises: the image recognition device scans the two-dimensional code on the transfer test tool, and the management system reads the two-dimensional code and outputs transfer test tool parameters and borrowing information.
Preferably, the step 4 comprises: after borrowing information is confirmed, the borrower selects to start returning, and meanwhile, the management system receives a returning request and opens an unused access grid;
closing the access grid after putting the transfer test tool in the storage grid, completing returning, and automatically registering returning information by the management system;
when returning a plurality of transfer test tools, the two-dimensional codes on the transfer test tools are scanned in sequence and put into the access grids to finish batch returning.
Preferably, after the current transfer test tool is expired, if the current transfer test tool is to be used continuously, the tool and the lending time in use are selected, the lending is determined to be completed later, and the management system automatically registers the lending information.
Preferably, when the two-dimensional code on the transfer test tool is placed in front of the image recognition device, the image recognition device reads tool information and borrows information through the two-dimensional code to check;
when the electric connector on the transfer test tool is aligned with the image recognition device, the image recognition device captures images of the electric connector, the specification, the appearance and the integrity of the contact element of the electric connector are judged, and if the quality problem of the transfer test tool is recognized, the management system automatically feeds back the quality problem to carry out inspection and maintenance.
Preferably, the temperature, the humidity and the cleanliness in the access grids are monitored, and when the monitored value exceeds the range of a set value, the access grids are trimmed;
logging in a management system, and selecting a transfer test tool for feedback;
scanning the two-dimensional code on the transfer test tool for feedback;
the image recognition device automatically feeds back when detecting that the quality problem exists in the switching test tool;
checking and maintaining after feedback;
the using times and using time of the tool are counted, and when the using times or the using time exceed a limit value, the tool is automatically fed back to be tested.
The spacecraft switching test tool management system provided by the invention comprises:
module M1: inquiring a transfer test tool;
module M2: selecting a transfer test tool to be borrowed and borrowing time, opening an access grid, and acquiring the transfer test tool;
module M3: after the use is finished, scanning two-dimensional code confirmation information on the transfer test tool;
module M4: and after the information is confirmed, opening the access grid, and putting the access grid into a transfer test tool to finish returning.
Compared with the prior art, the invention has the following beneficial effects:
1. shared storage, high utilization rate and no need of repeated production;
2. self-help borrowing and returning are realized, and the management cost is low;
3. the use efficiency is high when the user borrows and returns the book;
4. the mobile terminal APP logs in the system at any time and any place, and the system is convenient and quick;
5. image recognition, rapid detection of tool integrity, and timely inspection and maintenance;
6. monitoring and adjusting the storage environment, and improving quality guarantee;
7. the using times and the using time are counted and checked in time, so that the safety and the reliability of the tool are ensured;
8. centralized management and overall planning are performed, so that the universality is greatly improved;
9. designing management methods such as reservation and borrowing to guarantee a spacecraft test process;
10. the design of management methods such as batch borrowing and batch returning meets the requirements of external field tests such as butt joint and emission.
Drawings
Other features, objects and advantages of the invention will become more apparent upon reading of the detailed description of non-limiting embodiments with reference to the following drawings:
FIG. 1 is a block diagram of the management system software according to the present invention;
FIG. 2 is a schematic perspective view of an embodiment of the present invention;
FIG. 3 is a control flow diagram of a management method according to the present invention;
fig. 4 is a flow chart of the user usage of the management system of the present invention.
Detailed Description
The present invention will be described in detail with reference to specific examples. The following examples will assist those skilled in the art in further understanding the invention, but are not intended to limit the invention in any way. It should be noted that it would be obvious to those skilled in the art that various changes and modifications can be made without departing from the spirit of the invention. All falling within the scope of the present invention.
The spacecraft switching test tool management system comprises one or more self-service access boxes 1, a management terminal 4, a mobile terminal APP12 and a monitoring system 13, wherein each self-service access box comprises a plurality of access grids 2 and an environment monitoring and adjusting device 3, each management terminal comprises a workbench 5, a main controller 6, a two-dimensional code device 7, an image recognition device 8, an RFID module 9, a weighing platform 10 and a printer 11, the self-service storage boxes are connected with the management terminal through cables, the management terminal is connected with the mobile terminal APP in a wireless communication mode, and the monitor monitors the use of the system.
And the self-service access box 1 is provided with a plurality of access grids 2 for shared storage and self-service access of the switching test tools.
The self-service storage and taking box 1 is provided with an environment monitoring and adjusting device 3 for monitoring and adjusting the storage environment in real time so as to meet the high requirement of the aerospace tool on the storage environment.
The management terminal 4 comprises a workbench 5, a main controller 6, a two-dimensional code device 7, an image recognition device 8, an RFID module 9, a weighing platform 10 and a printer 11.
The main controller 6 is a computer terminal which is provided with a touch screen operation and display end, a wireless communication device and a storage device and can automatically perform data operation, the main controller 6 is connected with the self-service access box 1, and the main controller is connected with the Internet.
The main controller 6 is a server connected with one or more computer terminals and the affiliated computer terminals.
The two-dimensional code module 7 has a two-dimensional code label making function, and the two-dimensional code module 7 is connected with the main controller 6.
The image recognition device 8 has functions of two-dimensional code reading, tool image recognition, tool reliability detection and the like, and the image recognition device 8 is connected with the main controller 6.
The FRID module 9 is a non-contact card identification device, identifies a user through a working card, and the FRID module 9 is connected with the main controller 6.
The weighing module 10 is an electronic scale used for weighing tools, and the weighing module 10 is connected with the main controller 6.
At least one printer 11 is included for printing a tool list, etc., the printer 11 being connected to the main controller 6.
The mobile terminal APP12 is application software on mobile equipment and is used for management and use of a management system, and the mobile terminal APP12 is in wireless connection with the main controller 6.
Fig. 2 is a schematic perspective view of an embodiment of a spacecraft transfer test tool management system and method according to the present invention, including:
designing one or more self-service access boxes 1, wherein the self-service access boxes are provided with a plurality of access grids 2 for accessing the switching test tools, and are provided with an environment monitoring and adjusting device 3 for monitoring and adjusting the storage environment; designing a management terminal 4, having a workbench 5, a main controller 6 with a touch screen display and wireless communication functions for system operation, display and wireless communication, having a two-dimensional code device 7 for making a two-dimensional code label, having an image recognition device 8 for recognizing and detecting a tool, having an RFID module 9 for recognizing a work card, having a weighing platform 10 for weighing the tool, and having a printer 11 for list printing; designing a mobile terminal APP12 to perform remote operation; a monitor 13 is designed to be monitored by means of a monitoring system.
Fig. 1 is a block diagram of management system software in the present invention, which is software used in the main controller and the mobile terminal APP. The system software comprises an administrator account and a common user account, and the bottom data comprises a tool database, a personnel database and management rules. The administrator account includes functions such as tool management, user management, storage environment management, message management, and the like. Adding, deleting and submitting tools through a tool management module; the user management module is used for carrying out addition, deletion and authority management on the user; the storage environment management module is used for carrying out environment monitoring and environment regulation; and processing the information fed back by the user through a message module. The user account contains my tools, tool queries, messages, personal information, payment, etc. functions. Viewing the tool and borrowing history used by the account through my tool; selecting a tool for reservation and borrowing through a tool query module; feeding back information through a message module; editing personal registration information through a personal information module; and paying the fee through the payment module.
Fig. 3 is a control flow chart of the management method of the present invention, which mainly includes the following steps:
s1: logging in a management system, and inquiring a transfer test tool through the system;
s2: selecting a tool and borrowing time, and sending an instruction to open an access grid acquisition tool to complete borrowing;
s3: after the use is finished, reading tool parameters and borrowing information on a scanning tool of the image recognition device by using the two-dimensional code;
s4: and after the information is confirmed, the system opens the access grid, and the tool is put in the access grid to finish returning.
Fig. 4 is a flow chart of the user usage of the management system of the present invention.
When the management system is used, a user firstly registers, and can use the management system after the registration is finished, and the user can identify a work card through an RFID device or directly log in through an account; then, inquiring a test tool to be borrowed, checking a list, and selecting an inventory tool and borrowing time to borrow; and secondly, after the self-service access box receives the instruction, automatically opening the corresponding access box, taking out the test tool, closing the access box and completing borrowing.
When making an appointment, logging in a system, inquiring tools, and selecting the required tools to make an appointment; and selecting a time starting point and a time ending point, finishing reservation after the time starting point and the time ending point are determined, and automatically registering reservation information by the system. The day before the starting point, the system prompts that the appointment is made.
When the loan is renewed, the system is logged in, the tool in use is selected, the time of the loan is selected, the loan is completed after the confirmation, and the system automatically registers the information of the loan.
During transferring, logging in the system, inquiring the tool, selecting the lent tool, and initiating a transferring application; after the borrower agrees, and the user takes the tool, scanning the two-dimensional code on the tool through an image recognition device or a mobile terminal; the system reads the tool information and the related borrowing information, the user completes the borrowing after confirming, and the system automatically registers the tool borrowing information as a new borrower.
Finally, when the Chinese angelica is returned, firstly, the management system displays borrowing information of the test tool by identifying the two-dimensional code on the test tool; then, confirming the borrowing information of the test tool, and automatically opening an unused access box by the system after confirmation; and secondly, placing the test tool into the access box, closing the access box and completing returning.
In addition, the batch borrowing and batch returning can be carried out by matching with the weighing platform, and the steps are as follows:
when borrowing in batches, logging in the system, inquiring tools, and sequentially putting the selected tools into a storage vehicle; selecting a tool to be borrowed in a storage vehicle, and clicking to borrow in batches; the system borrows the list according to the batch to open the access grid of the 1 st tool; taking out the 1 st tool and placing the tool on a weighing table, and closing the storage grid; after the system detects that the access grids are closed and the tool is placed on the weighing table, opening the 2 nd access grid; and repeating the steps in sequence until the last 1 tool on the batch borrowing list is taken out, and completing batch borrowing.
When returning in batches, scanning the two-dimensional code of the 1 st tool by the image recognition device, and selecting batch returning after information confirmation; placing the 1 st tool on a weighing table; after the system detects that the placement is finished, scanning the 2 nd tool, and confirming the information; placing the 2 nd tool on a weighing station; after the system detects that the placement is finished, scanning a 3 rd tool, and confirming information; repeating the steps in sequence according to the 2 steps until all the tools are scanned and confirmed, placing the tools on a weighing platform, and selecting to determine returning; taking a tool from the weighing platform to scan the two-dimensional code, and opening an access grid by the system; putting the taken tool into the access grid and closing the access grid; repeating the steps in sequence until the last tool on the weighing table is placed into the storage grid, and completing batch returning.
In the description of the present application, it is to be understood that the terms "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", and the like indicate orientations or positional relationships based on those shown in the drawings, and are only for convenience in describing the present application and simplifying the description, but do not indicate or imply that the referred device or element must have a specific orientation, be constructed in a specific orientation, and be operated, and thus, should not be construed as limiting the present application.
Those skilled in the art will appreciate that, in addition to implementing the systems, apparatus, and various modules thereof provided by the present invention in purely computer readable program code, the same procedures can be implemented entirely by logically programming method steps such that the systems, apparatus, and various modules thereof are provided in the form of logic gates, switches, application specific integrated circuits, programmable logic controllers, embedded microcontrollers and the like. Therefore, the system, the device and the modules thereof provided by the present invention can be considered as a hardware component, and the modules included in the system, the device and the modules thereof for implementing various programs can also be considered as structures in the hardware component; modules for performing various functions may also be considered to be both software programs for performing the methods and structures within hardware components.
The foregoing description of specific embodiments of the present invention has been presented. It is to be understood that the present invention is not limited to the specific embodiments described above, and that various changes or modifications may be made by one skilled in the art within the scope of the appended claims without departing from the spirit of the invention. The embodiments and features of the embodiments of the present application may be combined with each other arbitrarily without conflict.
Claims (10)
1. A spacecraft switching test tool management method is characterized by comprising the following steps:
step 1: inquiring a transfer test tool;
step 2: selecting a transfer test tool to be borrowed and borrowing time, opening an access grid, and acquiring the transfer test tool;
and step 3: after the use is finished, scanning two-dimensional code confirmation information on the transfer test tool;
and 4, step 4: and after the information is confirmed, opening the access grid, and putting the access grid into a transfer test tool to finish returning.
2. The spacecraft switchover testing tool management method of claim 1, wherein step 1 comprises: inquiring according to the specification of the electric connector on the transfer test tool;
the query result is a list and state information of the transfer test tool;
when inquiring that the required transfer test tool is lent, selecting the lent transfer test tool, initiating a borrowing application, scanning the two-dimensional code on the transfer test tool through the image recognition device after the borrower agrees and takes the transfer test tool, reading the transfer test tool information and the borrowing information by the management system, completing the transfer after the user confirms, and automatically updating and registering the borrowing information by the management system.
3. The spacecraft switchover testing tool management method of claim 1, wherein said step 2 comprises: after a transfer test tool and borrowing time length are selected, the access grid sends a borrowing request, and the management system receives the borrowing request and opens the access grid;
taking out the transfer test tool, closing the access grid to complete borrowing, and automatically registering borrowing information by the management system;
when time is selected, selecting a starting point and an end point of any future time period to finish the reservation and borrowing of the transfer testing tool; starting the day before the starting point, and carrying out the reserved prompt by the management system;
when a plurality of transfer testing tools are borrowed, the selected transfer testing tools are sequentially placed into the storage vehicle, and when borrowing is selected, the transfer testing tools are sequentially taken out from the storage grids, so that batch borrowing is completed.
4. The spacecraft transfer test tool management method of claim 1, wherein the step 3 comprises: the image recognition device scans the two-dimensional code on the transfer test tool, and the management system reads the two-dimensional code and outputs transfer test tool parameters and borrowing information.
5. The spacecraft switchover testing tool management method of claim 1, wherein the step 4 comprises: after borrowing information is confirmed, the borrower selects to start returning, and meanwhile, the management system receives a returning request and opens an unused access grid;
closing the access grid after putting the transfer test tool in the storage grid, completing returning, and automatically registering returning information by the management system;
when returning a plurality of transfer test tools, the two-dimensional codes on the transfer test tools are scanned in sequence and put into the access grids to finish batch returning.
6. The method according to claim 1, wherein after the current transfer test tool has expired, if the current transfer test tool is to be used continuously, the tool in use and the renewal time are selected, and the renewal is determined to be completed, and the management system automatically registers renewal information.
7. The spacecraft switchover testing tool management method of claim 1, wherein when the two-dimensional code on the switchover testing tool is placed in front of the image recognition device, the image recognition device reads tool information and borrowing information through the two-dimensional code for checking;
when the electric connector on the transfer test tool is aligned with the image recognition device, the image recognition device captures images of the electric connector, the specification, the appearance and the integrity of the contact element of the electric connector are judged, and if the quality problem of the transfer test tool is recognized, the management system automatically feeds back the quality problem to carry out inspection and maintenance.
8. The spacecraft switchover testing tool management method of claim 1, wherein temperature, humidity, cleanliness in the access grid are monitored, and when the monitored values exceed a set value range, the access grid is trimmed;
logging in a management system, and selecting a transfer test tool for feedback;
scanning the two-dimensional code on the transfer test tool for feedback;
the image recognition device automatically feeds back when detecting that the quality problem exists in the switching test tool;
checking and maintaining after feedback;
the using times and using time of the tool are counted, and when the using times or the using time exceed a limit value, the tool is automatically fed back to be tested.
9. A spacecraft transfer test tool management system, comprising:
module M1: inquiring a transfer test tool;
module M2: selecting a transfer test tool to be borrowed and borrowing time, opening an access grid, and acquiring the transfer test tool;
module M3: after the use is finished, scanning two-dimensional code confirmation information on the transfer test tool;
module M4: and after the information is confirmed, opening the access grid, and putting the access grid into a transfer test tool to finish returning.
10. A computer-readable storage medium, in which a computer program is stored which, when being executed by a processor, carries out the steps of the method according to any one of claims 1 to 8.
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| CN112444692A (en) * | 2020-10-22 | 2021-03-05 | 上海卫星工程研究所 | Automatic lightweight ground switching test system for spacecraft |
| CN115240329A (en) * | 2021-04-22 | 2022-10-25 | 航天科工惯性技术有限公司 | Intelligent storage management system for tooling cables and management method using intelligent storage management system |
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