A space laboratory operation method and device and a storage medium

Abstract

The application relates to a space laboratory operation method and device and a storage medium. The method comprises the following steps: obtaining to-be-executed test information; obtaining a test condition database, wherein the test condition database comprises at least one test condition group and preset to-be-executed test information corresponding to each test condition group; obtaining a test condition group corresponding to the preset to-be-executed test information which is same as the to-be-executed test information; generating control information according to the test condition group, and sending the control information to a temperature and humidity adjusting system, a gas pressure adjusting system and a water inlet system of a space laboratory, so that at least one of the temperature and humidity adjusting system, the gas pressure adjusting system and the water inlet system works according to the control information. The application can automatically operate each device of the space laboratory according to a test to be performed, so that the operation condition is automatically reached.

Description

Technical Field

[0001] This application relates to the field of space laboratory operation and maintenance, and in particular to a space laboratory operation and maintenance method, device and storage medium. Background Technology

[0002] In existing technologies, space laboratories require users to set various details when performing operations. For example, temperature, gas concentration, humidity, and air pressure information need to be set according to the purpose of the experiment. This requires users to have highly specialized knowledge to make adjustments. If users are not clear about the specific data required for the experiment, they also need to consult materials to set up the various conditions of the space laboratory, which will bring various inconveniences. Summary of the Invention

[0003] In order to solve the above-mentioned technical problems, or at least partially solve the above-mentioned technical problems, this application provides a space laboratory operation and maintenance method, device and storage medium.

[0004] Firstly, this application provides a method for the operation and maintenance of a space laboratory, the method comprising the following steps:

[0005] Obtain information on the tests to be performed;

[0006] Obtain a test condition database, wherein the test condition database includes at least one test condition group and preset test information to be executed corresponding to each test condition group;

[0007] Obtain the test condition group corresponding to the preset test information that is identical to the test information to be performed;

[0008] Control information is generated based on the set of test conditions, and the control information is sent to the temperature and humidity control system, air pressure control system, and water inlet system of the space laboratory, so that at least one of the temperature and humidity control system, the air pressure control system, and the water inlet system operates according to the control information.

[0009] Preferably, the method further includes the step of:

[0010] Obtain the indoor temperature information of the space laboratory within a preset time period;

[0011] Obtain the temperature information of the air outlet of the temperature and humidity control system within the preset time period;

[0012] Obtain the trained Transformer model;

[0013] Extract the indoor temperature characteristics from the indoor temperature information;

[0014] Extract the outlet temperature characteristics of the temperature information;

[0015] The indoor temperature characteristics and the air outlet temperature characteristics are input into the Transformer model to obtain temperature prediction data.

[0016] Preferably, the test condition set includes target temperature information, and the method further includes the step of:

[0017] Obtain target temperature information;

[0018] Based on the target temperature information and the temperature prediction data, obtain the time information when the target temperature information is reached;

[0019] The time information is sent to the display unit for display.

[0020] Preferably, the test condition set includes preset gas component information, and the method further includes the following steps:

[0021] Gas control information is generated based on the preset gas component information;

[0022] The gas control information is sent to the gas generator so that the gas generator can release gas into the space laboratory.

[0023] Preferably, the method further includes the step of:

[0024] Acquire gas concentration information transmitted by the gas composition detection sensor group installed in the space laboratory;

[0025] Obtain the concentration change curve corresponding to the preset gas component information;

[0026] The gas concentration information transmitted by the gas composition detection sensor group within a preset time period is obtained;

[0027] Based on the gas concentration information, determine whether the concentration change deviates from the concentration change curve;

[0028] If so, an alarm message will be generated.

[0029] Preferably, the indoor temperature features for extracting the indoor temperature information include:

[0030] LSTM indoor temperature features are used to extract the indoor temperature information.

[0031] ARIMA indoor temperature features are extracted from the indoor temperature information using the ARIMA model.

[0032] The LSTM indoor temperature features are fused with the ARIMA indoor temperature features to obtain indoor temperature features.

[0033] Preferably, the outlet temperature characteristics for extracting the temperature information include:

[0034] The LSTM outlet temperature feature is used to extract the temperature information from the LSTM.

[0035] ARIMA outlet temperature features were extracted using the ARIMA model to obtain the temperature information.

[0036] The LSTM outlet temperature feature and the ARIMA outlet temperature feature are fused to obtain the outlet temperature feature.

[0037] Secondly, this application provides a space laboratory operation and maintenance system, including:

[0038] The module for acquiring test information to be performed is used to acquire test information to be performed.

[0039] The test condition database acquisition module is used to acquire the test condition database, wherein the test condition database includes at least one test condition group and preset test information to be executed corresponding to each test condition group;

[0040] The test condition group acquisition module is used to acquire the test condition group corresponding to the preset test information to be executed, which is the same as the test information to be executed.

[0041] The control information generation module is used to generate control information according to the test condition set, and send the control information to the temperature and humidity control system, air pressure control system and water inlet system of the space laboratory, so that at least one of the temperature and humidity control system, the air pressure control system and the water inlet system can operate according to the control information.

[0042] Thirdly, an electronic device is provided, the electronic device comprising:

[0043] At least one processor; and,

[0044] A memory communicatively connected to the at least one processor; wherein,

[0045] The memory stores instructions that can be executed by the at least one processor, which enables the at least one processor to perform any of the aforementioned space laboratory operation and maintenance methods.

[0046] Fourthly, a non-transitory computer-readable storage medium is provided, which stores computer instructions for causing the computer to execute any of the aforementioned space laboratory operation and maintenance methods.

[0047] The technical solutions provided in this application have the following advantages compared with the prior art:

[0048] The space laboratory operation and maintenance method, device and storage medium provided in this application embodiment only requires the user to input the test to be performed (test information to be performed), and this application can automatically operate the various devices of the space laboratory according to the test to be performed, thereby automatically achieving the operating conditions. Attached Figure Description

[0049] The accompanying drawings, which are incorporated in and form part of this specification, illustrate embodiments consistent with the invention and, together with the description, serve to explain the principles of the invention.

[0050] To more clearly illustrate the technical solutions in the embodiments of the present invention or the prior art, the drawings used in the description of the embodiments or the prior art will be briefly introduced below. Obviously, for those skilled in the art, other drawings can be obtained based on these drawings without creative effort.

[0051] Figure 1 This is a flowchart illustrating a space laboratory operation and maintenance method provided in an embodiment of the present invention;

[0052] Figure 2 This is a schematic diagram of the structure of a space laboratory operation and maintenance system provided in an embodiment of the present invention;

[0053] Figure 3 This is a schematic diagram of the structure of an electronic device provided by the present invention;

[0054] Figure 4 This is a schematic diagram of the structure of a non-transitory computer-readable storage medium provided by the present invention. Detailed Implementation

[0055] To make the objectives, technical solutions, and advantages of the embodiments of this application clearer, the technical solutions of the embodiments of this application will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are only some embodiments of this application, not all embodiments. Based on the embodiments of this application, all other embodiments obtained by those skilled in the art without creative effort are within the scope of protection of this application.

[0056] Figure 1 This is a flowchart illustrating a space laboratory operation and maintenance method provided in an embodiment of this application.

[0057] This application provides a method for the operation and maintenance of a space laboratory, the method comprising the following steps:

[0058] Obtain information on the tests to be performed;

[0059] Obtain a test condition database, wherein the test condition database includes at least one test condition group and preset test information to be executed corresponding to each test condition group;

[0060] Obtain the test condition group corresponding to the preset test information that is identical to the test information to be performed;

[0061] Control information is generated based on the set of test conditions, and the control information is sent to the temperature and humidity control system, air pressure control system, and water inlet system of the space laboratory, so that at least one of the temperature and humidity control system, the air pressure control system, and the water inlet system operates according to the control information.

[0062] When the space laboratory operation and maintenance method of this application is running, the user only needs to input the experiment to be performed (the experiment information to be performed), and this application can automatically operate the various devices of the space laboratory according to the experiment to be performed, thereby automatically achieving the operating conditions.

[0063] In this embodiment, the space laboratory operation and maintenance method further includes:

[0064] Obtain indoor temperature information of the space laboratory within a preset time period;

[0065] Obtain the temperature information of the air outlet of the temperature and humidity control system within a preset time period;

[0066] Obtain the trained transformer model;

[0067] Extract the indoor temperature characteristics of the space laboratory's indoor temperature information;

[0068] Extract the outlet temperature characteristics of the outlet temperature information of the temperature and humidity control system;

[0069] The indoor temperature characteristics of the indoor temperature information and the air outlet temperature characteristics of the air outlet information are input into the transformer model to obtain temperature prediction data.

[0070] In this embodiment, the set of test conditions includes target temperature information;

[0071] The space laboratory operation and maintenance method further includes:

[0072] Obtain target temperature information;

[0073] Based on the target temperature information and the temperature prediction data, obtain the time information when the target temperature information is reached;

[0074] The time information is sent to the display unit for display.

[0075] Using this method, users do not need to constantly monitor the temperature information of the space laboratory; they only need to follow the predicted time it will take to reach the corresponding temperature.

[0076] In this embodiment, the test condition set further includes preset gas component information;

[0077] The space laboratory operation and maintenance method further includes:

[0078] Gas control information is generated based on the preset gas component information;

[0079] The gas control information is sent to the gas generating device, which then discharges gas into the space laboratory.

[0080] In this embodiment, the space laboratory operation and maintenance method further includes:

[0081] Acquire gas concentration information transmitted by the gas composition detection sensor group installed in the space laboratory;

[0082] Obtain the concentration change curves corresponding to the preset gas component information;

[0083] Acquire gas concentration information transmitted by the gas composition detection sensor group within a preset time period;

[0084] Based on the gas concentration information transmitted by the gas composition detection sensor group within the preset time period, it is determined whether the concentration change deviates from the concentration change curve. If so, an alarm message is generated.

[0085] Using this method, it is possible to determine at any time whether there is a gas leak in the space laboratory or a malfunction of a gas generating device by checking whether the concentration change is consistent with the preset concentration change curve (i.e., deviates from a preset range).

[0086] In this embodiment, the gas composition detection sensor group includes a variety of gas composition detection sensors, such as oxygen concentration detection sensors, carbon dioxide concentration detection sensors, sulfur dioxide concentration detection sensors, carbon monoxide concentration detection sensors, methane concentration detection sensors, ammonia concentration detection sensors, and hydrogen sulfide concentration detection sensors.

[0087] In this embodiment, the gas generating device can provide gases such as oxygen, carbon dioxide, sulfur dioxide, carbon monoxide, methane, and ammonia as needed.

[0088] In this embodiment, the indoor temperature characteristics for extracting the indoor temperature information of the space laboratory include:

[0089] LSTM indoor temperature features were used to extract indoor temperature information of the space laboratory.

[0090] ARIMA indoor temperature features were used to extract indoor temperature information of the space laboratory using the ARIMA model.

[0091] The indoor temperature features are obtained by fusing the LSTM indoor temperature features with the ARIMA indoor temperature features.

[0092] In this embodiment, the outlet temperature characteristics for extracting the temperature information of the outlet of the temperature and humidity control system include:

[0093] LSTM outlet temperature features are used to extract the temperature information of the outlet of the temperature and humidity control system.

[0094] ARIMA outlet temperature features were used to extract the temperature information of the air outlet of the temperature and humidity control system using an ARIMA model.

[0095] The outlet temperature features are obtained by fusing the LSTM outlet temperature features with the ARIMA outlet temperature features.

[0096] This application obtains the air outlet temperature features and indoor temperature features by fusing features, thereby solving the shortcomings caused by simply using LSTM or ARIMA models.

[0097] In this embodiment, the final fusion result is obtained by weighted averaging of the digital sequences of LSTM (LSTM outlet temperature characteristics and LSTM indoor temperature characteristics) and ARIMA (ARIMA indoor temperature characteristics and ARIMA outlet temperature characteristics).

[0098] More specifically, simply average the LSTM outlet temperature characteristics with the ARIMA outlet temperature characteristics, and average the LSTM indoor temperature characteristics with the ARIMA indoor temperature characteristics.

[0099] like Figure 2 This application provides a space laboratory operation and maintenance system, including:

[0100] The test information acquisition module 10 is used to acquire test information to be performed.

[0101] The test condition database acquisition module 20 is used to acquire a test condition database, wherein the test condition database includes at least one test condition group and preset test information to be executed corresponding to each test condition group;

[0102] The test condition group acquisition module 30 is used to acquire the test condition group corresponding to the preset test information to be executed, which is the same as the test information to be executed.

[0103] The control information generation module 40 is used to generate control information according to the test condition group and send the control information to the temperature and humidity control system, air pressure control system and water inlet system of the space laboratory, so that at least one of the temperature and humidity control system, the air pressure control system and the water inlet system can work according to the control information.

[0104] The space laboratory operation and maintenance system provided in this application can perform the space laboratory operation and maintenance method provided in the above steps.

[0105] It should be understood that the specific embodiments described above are merely illustrative or explanatory of the principles of the invention and do not constitute a limitation thereof. Therefore, any modifications, equivalent substitutions, improvements, etc., made without departing from the spirit and scope of the invention should be included within the protection scope of the invention. Furthermore, the appended claims are intended to cover all variations and modifications falling within the scope and boundaries of the appended claims, or equivalent forms of such scope and boundaries.

[0106] The following is for reference. Figure 3 The diagram illustrates a structural schematic of an electronic device 100 suitable for implementing embodiments of the present disclosure. The electronic devices in the embodiments of the present disclosure may include, but are not limited to, mobile terminals such as mobile phones, laptops, digital broadcast receivers, PDAs (personal digital assistants), PADs (tablet computers), PMPs (portable multimedia players), in-vehicle terminals (e.g., in-vehicle navigation terminals), and fixed terminals such as digital TVs and desktop computers. Figure 3 The electronic device shown is merely an example and should not be construed as limiting the functionality and scope of the embodiments disclosed herein.

[0107] like Figure 3 As shown, the electronic device 100 may include a processing unit (e.g., a central processing unit, a graphics processing unit, etc.) 101, which can perform various appropriate actions and processes according to a program stored in a read-only memory (ROM) 102 or a program loaded from a storage device 108 into a random access memory (RAM) 103. The RAM 103 also stores various programs and data required for the operation of the electronic device 100. The processing unit 101, ROM 102, and RAM 103 are interconnected via a bus 104. An input / output (I / O) interface 105 is also connected to the bus 104.

[0108] Typically, the following devices can be connected to I / O interface 105: input devices 106 including, for example, touchscreens, touchpads, keyboards, mice, image sensors, microphones, accelerometers, gyroscopes, etc.; output devices 107 including, for example, liquid crystal displays (LCDs), speakers, vibrators, etc.; storage devices 108 including, for example, magnetic tapes, hard disks, etc.; and communication devices 109. Communication device 109 allows electronic device 100 to communicate wirelessly or wiredly with other devices to exchange data. Although electronic device 100 with various devices is shown in the figure, it should be understood that it is not required to implement or possess all of the devices shown. More or fewer devices may be implemented or possessed alternatively.

[0109] In particular, according to embodiments of this disclosure, the processes described above with reference to the flowcharts can be implemented as computer software programs. For example, embodiments of this disclosure include a computer program product comprising a computer program carried on a computer-readable medium, the computer program containing program code for performing the methods shown in the flowcharts. In such embodiments, the computer program can be downloaded and installed from a network via communication device 109, or installed from storage device 108, or installed from ROM 102. When the computer program is executed by processing device 101, it performs the functions defined in the methods of embodiments of this disclosure.

[0110] The following is for reference. Figure 4 It illustrates a schematic diagram of a computer-readable storage medium suitable for implementing embodiments of the present disclosure, the computer-readable storage medium storing a computer program that, when executed by a processor, can implement the space laboratory operation and maintenance method as described above.

[0111] The space laboratory operation and maintenance method, device and storage medium provided in this application embodiment only requires the user to input the test to be performed (test information to be performed), and this application can automatically operate the various devices of the space laboratory according to the test to be performed, thereby automatically achieving the operating conditions.

[0112] It should be noted that, in this document, relational terms such as "first" and "second" are used merely to distinguish one entity or operation from another, and do not necessarily require or imply any such actual relationship or order between these entities or operations. Furthermore, the terms "comprising," "including," or any other variations thereof are intended to cover non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements includes not only those elements but also other elements not expressly listed, or elements inherent to such a process, method, article, or apparatus. Without further limitations, an element defined by the phrase "comprising one..." does not exclude the presence of other identical elements in the process, method, article, or apparatus that includes said element.

[0113] The above description is merely a specific embodiment of the present invention, enabling those skilled in the art to understand or implement the invention. Various modifications to these embodiments will be readily apparent to those skilled in the art, and the general principles defined herein may be implemented in other embodiments without departing from the spirit or scope of the invention. Therefore, the present invention is not to be limited to the embodiments shown herein, but is to be accorded the widest scope consistent with the principles and novel features claimed herein.

Claims

1. A method for the operation and maintenance of a space laboratory, characterized in that, The method includes the following steps: Obtain information on the tests to be performed; Obtain a test condition database, wherein the test condition database includes at least one test condition group and preset test information to be executed corresponding to each test condition group; Obtain the test condition group corresponding to the preset test information that is identical to the test information to be performed; Control information is generated based on the set of test conditions, and the control information is sent to the temperature and humidity control system, air pressure control system, and water inlet system of the space laboratory, so that at least one of the temperature and humidity control system, the air pressure control system, and the water inlet system operates according to the control information. The method further includes the following steps: Obtain the indoor temperature information of the space laboratory within a preset time period; Obtain the temperature information of the air outlet of the temperature and humidity control system within the preset time period; Obtain the trained Transformer model; Extract the indoor temperature characteristics from the indoor temperature information; Extract the outlet temperature characteristics of the temperature information; The indoor temperature characteristics and the air outlet temperature characteristics are input into the Transformer model to obtain temperature prediction data; The test condition set includes target temperature information, and the method further includes the following steps: Obtain target temperature information; Based on the target temperature information and the temperature prediction data, obtain the time information when the target temperature information is reached; The time information is sent to the display unit for display. The test condition set includes preset gas component information, and the method further includes the following steps: Gas control information is generated based on the preset gas component information; The gas control information is sent to the gas generator so that the gas generator discharges gas into the space laboratory; The method further includes the following steps: Acquire gas concentration information transmitted by the gas composition detection sensor group installed in the space laboratory; Obtain the concentration change curve corresponding to the preset gas component information; The gas concentration information transmitted by the gas composition detection sensor group within a preset time period is obtained; Based on the gas concentration information, determine whether the concentration change deviates from the concentration change curve; If so, an alarm message will be generated; The indoor temperature features from which the indoor temperature information is extracted include: LSTM indoor temperature features are used to extract the indoor temperature information. ARIMA indoor temperature features are extracted from the indoor temperature information using the ARIMA model. The LSTM indoor temperature features are fused with the ARIMA indoor temperature features to obtain indoor temperature features; The outlet temperature characteristics from which the temperature information is extracted include: The LSTM outlet temperature feature is used to extract the temperature information from the LSTM. ARIMA outlet temperature features were extracted using the ARIMA model to obtain the temperature information. The LSTM outlet temperature feature and the ARIMA outlet temperature feature are fused to obtain the outlet temperature feature.

2. A space laboratory operation and maintenance system, applicable to the method described in claim 1, characterized in that, include: The module for acquiring test information to be performed is used to acquire test information to be performed. The test condition database acquisition module is used to acquire the test condition database, wherein the test condition database includes at least one test condition group and preset test information to be executed corresponding to each test condition group; The test condition group acquisition module is used to acquire the test condition group corresponding to the preset test information to be executed, which is the same as the test information to be executed. The control information generation module is used to generate control information according to the test condition set, and send the control information to the temperature and humidity control system, air pressure control system and water inlet system of the space laboratory, so that at least one of the temperature and humidity control system, the air pressure control system and the water inlet system can operate according to the control information.

3. An electronic device, characterized in that, The electronic device includes: At least one processor; and, A memory communicatively connected to the at least one processor; wherein, The memory stores instructions that can be executed by the at least one processor, which, when executed by the at least one processor, enables the at least one processor to perform the space laboratory operation and maintenance method of claim 1.

4. A non-transitory computer-readable storage medium storing computer instructions for causing the computer to perform the space laboratory operation and maintenance method of claim 1.

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