Manned spaceflight emergency rescue test launch process configuration method and system
By optimizing the test launch process configuration, building an emergency rescue test launch process pool and identification information queue, the problem of time-consuming traditional test launch process is solved, rapid technical preparation and launch is achieved, and the test launch cycle is significantly reduced.
Patent Information
- Application Number
- CN202411739308.8
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Filing Date
- 2024-11-29
- Publication Date
- 2025-03-21
AI Technical Summary
The traditional test launch process takes a long time and cannot meet the emergency rescue needs of astronauts during the space station. The rocket is idle while waiting for the spacecraft to test, wasting resources.
Provide a manned space emergency rescue test launch process configuration method. By obtaining and parsing test files and configuration files, building an emergency rescue test launch process pool and identifying information queue, optimizing the test process, and selecting the shortest time-consuming process as the optimal test launch process.
On the basis of ensuring the reliability and safety of space launch activities, the test launch cycle is significantly reduced to achieve rapid technical preparation and launch of launch vehicles and spacecraft systems.
Smart Images
Figure CN119671157A_ABST
Abstract
Description
Technical Field
[0001] The present application relates to the field of aerospace test launch technology, and in particular to a method and system for configuring a manned aerospace emergency rescue test launch process. Background Art
[0002] In order to meet the emergency rescue needs of astronauts during their stay in the space station, it is necessary to ensure that the carrier rocket is launched in a timely and accurate manner to transport the spacecraft to the designated orbit. For such needs, if the space launch site system continues to use the traditional, time-consuming test and launch process, the spacecraft and rocket will carry out technical preparations in the technical area assembly and test plant respectively. After the spacecraft is filled in the technical area, the cover assembly process is carried out to form a ship-cover assembly, which is vertically transported to the rocket assembly and test plant. After the ship-cover assembly docks with the rocket base stage, it forms a ship-rocket assembly, which is vertically transported to the launch area through a mobile launch platform to jointly carry out rocket-ground connection, filling preparation, spacecraft function inspection, pre-launch testing, filling and launching, etc. The process is implemented in series, the test items are complicated and time-consuming, and the emergency rescue effect will not be achieved. Therefore, it is necessary to significantly reduce the test launch time and optimize the test launch process.
[0003] At the same time, the traditional test and launch process has the characteristics of many spacecraft test items and a relatively long technical preparation time relative to the rocket. The rocket is idle most of the time, waiting for spacecraft testing. There is an urgent need to optimize the test and launch process and significantly reduce the pressure on the test and launch cycle.
[0004] Therefore, the technical problem that needs to be solved urgently is: how to provide the optimal test launch process configuration method to facilitate the rapid technical preparation and launch of the launch vehicle and spacecraft system in a scientific and effective manner when astronauts on the space station mission raise emergency rescue needs during their stay in the space station. On the basis of ensuring the reliability and safety of space launch activities, the test launch cycle can be greatly reduced by optimizing the test process. Summary of the invention
[0005] The purpose of this application is to provide a manned space emergency rescue test launch process configuration method and system, and to provide an optimal test launch process configuration method, so as to facilitate the scientific and effective implementation of rapid technical preparation and launch of the launch vehicle and spacecraft system when emergency rescue needs are raised during the astronauts' stay in the space station. On the basis of ensuring the reliability and safety of space launch activities, the test launch cycle can be greatly reduced by optimizing the test process.
[0006] To achieve the above objectives, the present application provides a method for configuring a manned space emergency rescue test launch process, the method comprising:
[0007] Get test files and configuration files;
[0008] Parsing the test file and the configuration file, and constructing an emergency rescue test launch process pool and an identification information queue;
[0009] Based on a first preset reading order, reading identification information from the identification information queue, and reading a test launch process from an emergency rescue test launch process pool according to the read identification information;
[0010] Based on matching with the identification information, executing the test transmission process;
[0011] After the test launch process is completed, the test result is obtained, and the test result is paired with the total time consumption information;
[0012] The process with the shortest time among all the read test emission processes is selected as the optimal test emission process.
[0013] The method for configuring the manned space emergency rescue test launch process as described above, wherein, based on matching with the identification information, after running the test launch process, it also includes: determining whether the identification information in the identification information queue has been read, and if so, obtaining all test results and corresponding time-consuming information of all read test launch processes; otherwise, returning to continue executing based on matching with the identification information and running the test launch process.
[0014] The manned space emergency rescue test launch process configuration method as described above, wherein the test file includes emergency rescue test items for rockets, spacecraft, and escape tower products at the launch site and their minimum time consumption; the emergency rescue test items refer to the necessary test items that need to be completed by standby products to perform emergency rescue tasks; the configuration file includes a strong coupling relationship between the emergency rescue test items for rockets, spacecraft, and escape tower products at the launch site.
[0015] In the manned space emergency rescue test launch process configuration method as described above, the strong coupling relationship refers to the sequence of necessary test items that the standby product needs to complete in order to perform emergency rescue tasks.
[0016] The method for configuring the manned space emergency rescue test launch process as described above, wherein the method for constructing the emergency rescue test launch process pool includes:
[0017] Parsing the test file and the configuration file to identify necessary test items, minimum time consumption corresponding to a single necessary test item, and a strong coupling relationship between necessary test items;
[0018] Arrange the required test items into a test launch process based on the strong coupling relationship between the required test items;
[0019] Associating the minimum time consumption corresponding to a single required test item with the test items in the test launch process to construct the time consumption information;
[0020] Build an emergency rescue test launch process pool based on the constructed test launch process and time-consuming information.
[0021] In the above-mentioned manned space emergency rescue test launch process configuration method, the method of constructing the identification information queue includes:
[0022] Construct identification information based on the strong coupling relationship between the required test items;
[0023] The identification information is stored in a queue to construct an identification information queue;
[0024] The identification information queue is used to store identification information, and the identification information is used to obtain the corresponding test launch process from the emergency rescue test launch process pool.
[0025] The manned space emergency rescue test launch process configuration method as described above, wherein the emergency rescue test launch process pool includes multiple test launch processes;
[0026] Each test launch process includes multiple test items and the test order of the multiple test items, as well as time consumption information of each test item.
[0027] In the manned space emergency rescue test launch process configuration method as described above, the constructed emergency rescue test launch process pool and identification information queue are imported into the computing control center.
[0028] As a second aspect of the present application, the present application provides a manned space emergency rescue test launch process configuration system, the system comprising:
[0029] Acquisition module, used to obtain test files and configuration files;
[0030] A construction module is used to parse the test file and the configuration file, and to construct an emergency rescue test launch process pool and an identification information queue;
[0031] A reading module, configured to read identification information from the identification information queue based on a first preset reading order, and read a test launch process from an emergency rescue test launch process pool according to the read identification information;
[0032] An operation module, configured to execute the test transmission process based on matching with the identification information;
[0033] A pairing module, used for obtaining the test result after the test launch process is completed, and pairing the test result with the total time consumption information;
[0034] The comparison module is used to select the shortest test emission process among all the read test emission processes as the optimal test emission process.
[0035] The manned space emergency rescue test launch process configuration system as described above, wherein the system also includes:
[0036] The judgment module is used to judge whether the identification information in the identification information queue has been read. If so, all test results and corresponding time-consuming information of all read test emission processes are obtained; otherwise, the test emission process is run based on matching with the identification information and returned to continue execution.
[0037] The beneficial effects achieved by this application are as follows:
[0038] (1) This application provides an optimal test launch process configuration method to facilitate the scientific and effective implementation of rapid technical preparation and launch of launch vehicles and spacecraft systems when astronauts on a space station mission raise emergency rescue needs during their stay in the space station.
[0039] (2) This application aims to significantly reduce the test launch cycle by optimizing the test process while ensuring the reliability and safety of space launch activities. BRIEF DESCRIPTION OF THE DRAWINGS
[0040] In order to more clearly illustrate the embodiments of the present application or the technical solutions in the prior art, the drawings required for use in the embodiments or the description of the prior art will be briefly introduced below. Obviously, the drawings described below are only some embodiments recorded in the present application. For those skilled in the art, other drawings can also be obtained based on these drawings.
[0041] Figure 1 This is a flowchart of a method for configuring a manned space emergency rescue test launch process according to an embodiment of the present application.
[0042] Figure 2 This is a structural schematic diagram of a manned space emergency rescue test launch process configuration system according to an embodiment of the present application. DETAILED DESCRIPTION
[0043] The following is a clear and complete description of the technical solutions in the embodiments of the present application in conjunction with the drawings in the embodiments of the present application. Obviously, the described embodiments are part of the embodiments of the present application, not all of the embodiments. Based on the embodiments in the present application, all other embodiments obtained by those skilled in the art without creative work are within the scope of protection of the present application.
[0044] Embodiment 1
[0045] like Figure 1As shown, the present application provides a method for configuring a manned space emergency rescue test launch process, the method comprising:
[0046] Step S1, obtaining a test file and a configuration file.
[0047] The test documents include emergency rescue test items and their minimum time consumption for rocket, spacecraft and escape tower products at the launch site. Emergency rescue test items refer to the necessary test items that standby products need to complete in order to perform emergency rescue tasks. Minimum time consumption refers to the minimum time required to complete a single required test item.
[0048] Among them, the configuration file includes the strong coupling relationship between the emergency rescue test items of rockets, spacecraft, and escape tower products at the launch site.
[0049] Among them, the strong coupling relationship refers to the sequence of necessary test items that the standby product needs to complete to perform emergency rescue tasks.
[0050] Step S2, parse the test file and configuration file, and build an emergency rescue test launch process pool and identification information queue.
[0051] As a specific embodiment of the present invention, a method for constructing an emergency rescue test launch process pool includes:
[0052] Step S210, parsing the test file and the configuration file, identifying the necessary test items, the minimum time consumption corresponding to a single necessary test item, and the strong coupling relationship between the necessary test items.
[0053] Specifically, the configuration file is parsed to identify the strong coupling relationship between the necessary test items, and the strong coupling relationship information of the test items is constructed according to the strong coupling relationship between the necessary test items.
[0054] Step S220 , arranging the necessary test items into a test launch process according to the strong coupling relationship between the necessary test items.
[0055] Specifically, according to the strong coupling relationship between the required test items, the strong coupling relationship information of the test items is constructed, and according to the strong coupling relationship information of the test items, the test launch process is constructed. For example, if project A is executed before project B, the test launch process is constructed in this order.
[0056] Step S230, associating the minimum time consumption corresponding to a single required test item with the test item in the test launch process to construct time consumption information.
[0057] Step S240, constructing an emergency rescue test launch process pool according to the constructed test launch process and time consumption information.
[0058] Specifically, the constructed test launch process and time-consuming information are stored in a data structure to form an emergency rescue test launch process pool. This data structure can be a list, in which each element is a complete test launch process. The emergency rescue test launch process pool consists of all test launch processes.
[0059] Among them, the emergency rescue test launch process pool includes multiple test launch processes;
[0060] Each test launch process includes multiple test items and the test order of the multiple test items, as well as time consumption information of each test item.
[0061] As a specific embodiment of the present invention, the method for constructing an identification information queue includes:
[0062] Step S250: constructing identification information according to the strong coupling relationship between the required test items.
[0063] The identification information is used to obtain the corresponding test launch process from the emergency test launch process pool. The identification information may include a specific identifier, a test equipment name, a test equipment model, a test item name, etc.
[0064] Step S260: Store the identification information in a queue to construct an identification information queue.
[0065] Among them, the queue can easily obtain identification information in a first-in-last-out order in subsequent processing, so as to perform strong coupling relationship processing when executing the test launch process.
[0066] The identification information queue is used to store the identification information.
[0067] It can be understood that when the identification information is unique or has a specific identifier, such as a specific number, serial number, etc., the identifier that is the same as the identification information will be directly searched in the emergency test launch process pool, thereby accurately locating the corresponding test launch process.
[0068] Import the constructed emergency rescue test launch process pool and identification information queue into the computing control center.
[0069] Step S3, based on the first preset reading order, read the identification information from the identification information queue, and read the test launch process from the emergency rescue test launch process pool according to the read identification information.
[0070] As a preferred embodiment of the present invention, step S3 includes: according to the read identification information, reading a test launch process whose matching value with the identification information exceeds a preset threshold from the emergency rescue test launch process pool, so as to test the read test launch process, so that the test launch process is more matched with the identification information, thereby improving the configuration efficiency of the test launch process.
[0071] As a preferred embodiment of the present invention, according to the read identification information, reading a test launch process whose matching value with the identification information exceeds a preset threshold from the emergency rescue test launch process pool includes:
[0072] Step S310, extract key features of the test launch process in the emergency rescue test launch process pool to obtain key feature data of the test launch process.
[0073] Among them, the key characteristic data of the test launch process include: test item identification information, test order of test items, identification information of test equipment, etc.
[0074] Step S320, calculating the matching value between the identification information and the test launch process according to the read identification information and the key characteristic data of the test launch process.
[0075] The identification information includes: identification of the test equipment (number, name or model of the test equipment), identification information of the test items and / or the sequence of any two test items.
[0076] Specifically, the calculation formula for the matching value between the identification information and the test launch process is as follows:
[0077]
[0078] Where BP represents the matching value between the identification information and the test launch process; α represents the influence weight of the test item on the matching value between the identification information and the test launch process; M represents the total number of test item identification information; CBs i Indicates the matching factor between the identification information of the i-th test item and the identification information of the test equipment in the key characteristic data of the test launch process; if the identification information of the i-th test item can be found in the item identification information in the key characteristic data of the test launch process, then CBs i =1, otherwise CBs i =0; Z represents the total number of combinations of any two test items selected from the identification information; Tcx j Indicates whether the order of the jth combination of any two test items selected from the identification information is the same as the order of the two test items in the key feature data of the test launch process; if so, then Tcx j =1, otherwise Tcx j=0; Xcx represents the number of test items included in the identification information that are the same as the test items in the key characteristic data of the test launch process; Bcx represents the number of test items included in the identification information that are different from the test items in the key characteristic data of the test launch process; Zcx represents the total number of test items in the key characteristic data of the test launch process; β represents the influence weight of the test equipment on the matching value between the identification information and the test launch process; α+β=1; L represents the total number of identifications of the test equipment; q k Indicates the impact factor of the identification of the kth test device; Ucs k Indicates the matching factor between the identification of the kth test device and the identification information of the test device in the key feature data of the test launch process; if the identification of the kth test device exists in the identification information of the test device in the key feature data of the test launch process, then Ucs k =1; otherwise, Ucs k =0.
[0079] Step S330, compare the matching value between the identification information and the test transmission process with the preset threshold value, if the matching value between the identification information and the test transmission process is greater than or equal to the preset threshold value, read the test transmission process, otherwise, there is no need to read the test transmission process.
[0080] As a specific embodiment of the present invention, the present application calculates the matching value between the identification information and the test emission process, thereby improving the accuracy of the calculation of the matching value between the identification information and the test emission process. The test emission process whose matching value between the identification information and the test emission process is greater than the preset threshold is read, thereby testing the read test emission process, and there is no need to read and test the test emission process whose matching value between the identification information and the test emission process is less than the preset threshold, so that the read test emission process meets the requirements, avoiding testing the test emission process that does not meet the requirements, and improving the test efficiency of the test emission process. Therefore, the test emission process with the shortest time consumption is selected from the test emission processes whose matching value with the identification information is greater than or equal to the preset threshold as the optimal test emission process, thereby improving the configuration efficiency and configuration accuracy of the optimal test emission process.
[0081] Step S4, running the test transmission process based on matching with the identification information.
[0082] Specifically, based on matching with the identification information, running the test launch process is to accurately locate the corresponding test launch process in the emergency rescue test launch process pool through specific identification information, and start and let this matched test launch process start running.
[0083] Step S5, after the test launch process is completed, the test result is obtained and the test result is paired with the total time consumption information.
[0084] Among them, the test result refers to whether the rocket can be launched normally after the test launch process is run.
[0085] Step S6, determine whether the identification information in the identification information queue has been read. If so, obtain all test results and corresponding time-consuming information of all read test emission processes; otherwise, return to step S4 and run the test emission process based on matching with the identification information.
[0086] Step S7, selecting the shortest test transmission process among all the read test transmission processes as the optimal test transmission process.
[0087] Specifically, the time consumption information of all the read test emission processes is analyzed and compared, and the process with the shortest time consumption among all the read test emission processes is selected as the optimal test emission process.
[0088] Embodiment 2
[0089] like Figure 2 As shown, the present application provides a manned space emergency rescue test launch process configuration system 100, the system comprising:
[0090] An acquisition module 10 is used to acquire a test file and a configuration file;
[0091] Construction module 20, used for parsing test files and configuration files, building an emergency rescue test launch process pool and identification information queue;
[0092] The reading module 30 is used to read the identification information from the identification information queue based on the first preset reading order, and read the test launch process from the emergency rescue test launch process pool according to the read identification information;
[0093] An operation module 40 is used to run a test launch process based on matching with the identification information;
[0094] A pairing module 50 is used to obtain the test result after the test launch process is completed, and pair the test result with the total time consumption information;
[0095] The judgment module 60 is used to judge whether the identification information in the identification information queue has been read. If so, all test results and corresponding time-consuming information of all read test emission processes are obtained; otherwise, the test emission process is run based on matching with the identification information and returned to be executed.
[0096] The comparison module 70 is used to select the shortest test emission process among all the read test emission processes as the optimal test emission process.
[0097] The system also includes: a data processor 80, which is used to read a test launch process whose matching value with the identification information exceeds a preset threshold from the emergency rescue test launch process pool according to the read identification information.
[0098] The acquisition module 10 is also used to extract key features of the test launch process in the emergency rescue test launch process pool to obtain key feature data of the test launch process.
[0099] Among them, the key characteristic data of the test launch process include: test item identification information, test order of test items, identification information of test equipment, etc.
[0100] The data processor 80 is used to calculate the matching value between the identification information and the test emission process according to the read identification information and the key characteristic data of the test emission process.
[0101] The identification information includes: identification of the test equipment (number, name or model of the test equipment), identification information of the test items and / or the sequence of any two test items.
[0102] Specifically, the calculation formula for the matching value between the identification information and the test launch process is as follows:
[0103]
[0104] Where BP represents the matching value between the identification information and the test launch process; α represents the influence weight of the test item on the matching value between the identification information and the test launch process; M represents the total number of test item identification information; CBs i Indicates the matching factor between the identification information of the i-th test item and the identification information of the test equipment in the key characteristic data of the test launch process; if the identification information of the i-th test item can be found in the item identification information in the key characteristic data of the test launch process, then CBs i =1, otherwise CBs i =0; Z represents the total number of combinations of any two test items selected from the identification information; Tcx j Indicates whether the order of the jth combination of any two test items selected from the identification information is the same as the order of the two test items in the key feature data of the test launch process; if so, then Tcx j =1, otherwise Tcx j=0; Xcx represents the number of test items included in the identification information that are the same as the test items in the key characteristic data of the test launch process; Bcx represents the number of test items included in the identification information that are different from the test items in the key characteristic data of the test launch process; Zcx represents the total number of test items in the key characteristic data of the test launch process; β represents the influence weight of the test equipment on the matching value between the identification information and the test launch process; α+β=1; L represents the total number of identifications of the test equipment; q k Indicates the impact factor of the identification of the kth test device; Ucs k Indicates the matching factor between the identification of the kth test device and the identification information of the test device in the key feature data of the test launch process; if the identification of the kth test device exists in the identification information of the test device in the key feature data of the test launch process, then Ucs k =1; otherwise, Ucs k =0.
[0105] The comparison module 70 is also used to compare the matching value between the identification information and the test launch process with a preset threshold. If the matching value between the identification information and the test launch process is greater than or equal to the preset threshold, the test launch process is read; otherwise, the test launch process does not need to be read.
[0106] The present application also provides a computer storage medium, wherein the computer storage medium stores computer instructions, and when the computer instructions are called, they are used to execute the address mapping method of the large-capacity solid-state hard disk. The computer storage medium contains one or more program instructions, and the one or more program instructions are used by the processor to execute a manned space emergency rescue test launch process configuration method.
[0107] The embodiment disclosed in the present invention provides a computer-readable storage medium, in which computer program instructions are stored. When the computer program instructions are executed on a computer, the computer executes the above-mentioned method for configuring a manned space emergency rescue test launch process.
[0108] An embodiment of the present invention provides a processor for processing the above-mentioned manned space emergency rescue test launch process configuration method.
[0109] In the embodiment of the present invention, the processor may be an integrated circuit chip having the ability to process signals. The processor may be a general-purpose processor, a digital signal processor (DSP), an application-specific integrated circuit (ASIC), a field programmable gate array (FPGA), or other programmable logic devices, discrete gate or transistor logic devices, or discrete hardware components.
[0110] The methods, steps and logic block diagrams disclosed in the embodiments of the present invention can be implemented or executed. The general processor can be a microprocessor or the processor can also be any conventional processor, etc. The steps of the method disclosed in the embodiments of the present invention can be directly embodied as a hardware decoding processor for execution, or can be executed by a combination of hardware and software modules in the decoding processor. The software module can be located in a mature storage medium in the field such as a random access memory, a flash memory, a read-only memory, a programmable read-only memory or an electrically erasable programmable memory, a register, etc. The processor reads the information in the storage medium and completes the steps of the above method in combination with its hardware.
[0111] The storage medium may be a memory, which may be, for example, a volatile memory or a nonvolatile memory, or may include both volatile and nonvolatile memory.
[0112] Among them, the non-volatile memory can be a read-only memory (ROM), a programmable read-only memory (PROM), an erasable programmable read-only memory (EPROM), an electrically erasable programmable read-only memory (EEPROM), or a flash memory. The volatile memory can be a random access memory (RAM), which is used as an external cache. By way of example but not limitation, many forms of RAM are available, such as static random access memory (SRAM), dynamic random access memory (DRAM), synchronous dynamic random access memory (SDRAM), double data rate synchronous dynamic random access memory (DDRSDRAM), enhanced synchronous dynamic random access memory (ESDRAM), synchronous link dynamic random access memory (SLDRAM) and direct RAM bus random access memory (DRRAM).
[0113] The beneficial effects achieved by this application are as follows:
[0114] (1) This application provides an optimal test launch process configuration method to facilitate the scientific and effective implementation of rapid technical preparation and launch of launch vehicles and spacecraft systems when astronauts on a space station mission raise emergency rescue needs during their stay in the space station.
[0115] (2) This application aims to significantly reduce the test launch cycle by optimizing the test process while ensuring the reliability and safety of space launch activities.
[0116] In the description of this application, the terms "first" and "second" are used for descriptive purposes only and should not be understood as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include one or more of the features. In the description of this application, "plurality" means two or more, unless otherwise clearly and specifically defined.
[0117] In the description of the present application, the word "for example" is used to mean "used as an example, illustration or explanation". Any embodiment described as "for example" in the present application is not necessarily to be construed as being more preferred or advantageous than other embodiments. The following description is given to enable any technician in the field to implement and use the present invention. In the following description, details are listed for the purpose of explanation. It should be understood that a person of ordinary skill in the art can recognize that the present invention can be implemented without using these specific details. In other examples, well-known structures and processes will not be elaborated in detail to avoid obscuring the description of the present invention with unnecessary details. Therefore, the present invention is not intended to be limited to the embodiments shown, but is consistent with the widest scope consistent with the principles and features disclosed in the present application.
[0118] The above description is only an embodiment of the present invention and is not intended to limit the present invention. For those skilled in the art, the present invention may have various modifications and variations. Any modification, equivalent substitution, improvement, etc. made within the spirit and principle of the present invention should be included in the scope of the claims of the present invention.
Claims
1. A method for configuring a manned space emergency rescue test launch process, characterized in that: The method includes: Get test files and configuration files; Parsing the test file and the configuration file, and constructing an emergency rescue test launch process pool and an identification information queue; Based on a first preset reading order, reading identification information from the identification information queue, and reading a test launch process from an emergency rescue test launch process pool according to the read identification information; Based on matching with the identification information, executing the test transmission process; After the test launch process is completed, the test result is obtained, and the test result is paired with the total time consumption information; The process with the shortest time among all the read test emission processes is selected as the optimal test emission process.
2. The method for configuring the manned space emergency rescue test launch process according to claim 1, characterized in that: Based on the matching with the identification information, after running the test launch process, it also includes: determining whether the identification information in the identification information queue has been read, and if so, obtaining all test results and corresponding time-consuming information of all read test launch processes; otherwise, returning to continue executing based on the matching with the identification information and running the test launch process.
3. The method for configuring the launch process of manned space emergency rescue test according to claim 1, characterized in that: The test documents include emergency rescue test items and their minimum time consumption for rocket, spacecraft and escape tower products at the launch site; The emergency rescue test items refer to the necessary test items that the standby product needs to complete in order to perform emergency rescue tasks; The configuration file includes a strong coupling relationship between emergency rescue test items of rocket, spacecraft and escape tower products at the launch site.
4. The method for configuring the manned space emergency rescue test launch process according to claim 3, characterized in that: The strong coupling relationship refers to the sequence of necessary test items that the standby product needs to complete in order to perform emergency rescue tasks.
5. The method for configuring the launch process of manned space emergency rescue test according to claim 3, characterized in that: The method of building an emergency rescue test launch process pool includes: Parsing the test file and the configuration file to identify necessary test items, minimum time consumption corresponding to a single necessary test item, and a strong coupling relationship between necessary test items; Arrange the required test items into a test launch process based on the strong coupling relationship between the required test items; Associating the minimum time consumption corresponding to a single required test item with the test items in the test launch process to construct the time consumption information; Build an emergency rescue test launch process pool based on the constructed test launch process and time-consuming information.
6. The method for configuring the launch process of manned space emergency rescue test according to claim 5, characterized in that: Methods for building identification information queues include: Construct identification information based on the strong coupling relationship between the required test items; The identification information is stored in a queue to construct an identification information queue; The identification information queue is used to store identification information, and the identification information is used to obtain the corresponding test launch process from the emergency rescue test launch process pool.
7. The method for configuring the launch process of manned space emergency rescue test according to claim 5, characterized in that: The emergency rescue test launch process pool includes multiple test launch processes; Each test launch process includes multiple test items and the test order of the multiple test items, as well as time consumption information of each test item.
8. The method for configuring the launch process of manned space emergency rescue test according to claim 1, characterized in that: Import the constructed emergency rescue test launch process pool and identification information queue into the computing control center.
9. A manned space emergency rescue test launch process configuration system, characterized in that: The system includes: Acquisition module, used to obtain test files and configuration files; A construction module is used to parse the test file and the configuration file, and to construct an emergency rescue test launch process pool and an identification information queue; A reading module, configured to read identification information from the identification information queue based on a first preset reading order, and read a test launch process from an emergency rescue test launch process pool according to the read identification information; An operation module, configured to execute the test transmission process based on matching with the identification information; A pairing module, used for obtaining the test result after the test launch process is completed, and pairing the test result with the total time consumption information; The comparison module is used to select the shortest test emission process among all the read test emission processes as the optimal test emission process.
10. The manned space emergency rescue test launch process configuration system according to claim 9, characterized in that: The system also includes: The judgment module is used to judge whether the identification information in the identification information queue has been read. If so, all test results and corresponding time-consuming information of all read test emission processes are obtained; otherwise, the test emission process is run based on matching with the identification information and returned to continue execution.