Radiation temperature error correction method of high-temperature blackbody radiation source

Abstract

The application discloses a radiation temperature error correction method of a high-temperature blackbody radiation source. On the basis of designing the structure of the surface source blackbody, the technical effect that the emissivity of the surface source blackbody is relatively stable and the radiation efficiency is relatively high is realized. In addition, for the surface source blackbody provided by the application, a radiation temperature error correction method of a high-temperature blackbody radiation source is also provided. Even if the emissivity of the surface source blackbody deviates from the ideal value or the emissivity of the surface source blackbody fluctuates, the error between the actual temperature of the surface source blackbody and the target temperature can be corrected by the method in the specification, so that the user can know the actual temperature of the surface source blackbody. Furthermore, when the surface source blackbody is applied to the calibration and verification of the temperature measuring product by using the method in the specification, the accuracy of the obtained result can be improved.

Description

Technical Field

[0001] This application relates to the field of monitoring or testing technology for control or regulation systems of blackbody radiation sources, and in particular to a method for correcting radiation temperature error of a high-temperature blackbody radiation source. Background Technology

[0002] Currently, blackbodies are mainly used in temperature measurement, and the main products related to blackbodies include blackbody furnaces. For example, blackbodies can be used for the calibration and verification of radiation thermometers. For instance, when calibrating a device under test using a comparative method, the temperature reproduced by the device under test needs to be compared with the temperature reproduced by a blackbody radiation source to determine whether the device under test is qualified. This requires the blackbody radiation source to reproduce a relatively accurate temperature and also to be able to determine the function of the device under test.

[0003] However, in reality, the blackbody in the relevant technology is an idealized object. In calibration and verification scenarios with high precision requirements, the temperature reproduced by the blackbody radiation source may be distorted. Summary of the Invention

[0004] This application provides a method for correcting the radiation temperature error of a high-temperature blackbody radiation source, so as to at least partially solve the above-mentioned technical problems.

[0005] The embodiments of this application adopt the following technical solutions:

[0006] In a first aspect, embodiments of this application provide a method for correcting the radiation temperature error of a high-temperature blackbody radiation source. The method is based on a surface-source blackbody, which includes: a substrate, a second radiation layer attached to one side of the substrate, and a first radiation layer attached to the side of the second radiation layer facing away from the substrate. The first radiation layer includes a plurality of first radiation units arranged sequentially along the second radiation layer. The second radiation layer includes a plurality of second radiation units arranged sequentially on the substrate. The surface-source blackbody further includes a first electrode connected to the first radiation layer and a second electrode connected to the second radiation layer. The method includes:

[0007] Upon triggering a heating command, the current temperature of the surface source blackbody and the target temperature to be reached as indicated by the heating command are obtained.

[0008] A heating strategy that matches both the current temperature and the target temperature is found in a preset heating strategy library and is used as the target strategy; wherein, the heating strategy records the correspondence between the current temperature range, the target temperature range, the first electrode control method, and the second electrode control method;

[0009] The first electrode voltage rise obtained based on the first electrode control method, the second electrode voltage rise obtained based on the second electrode control method, and the temperature rise of the target temperature relative to the current temperature are used as available parameters;

[0010] The target strategy is executed, and the current temperature of the blackbody is updated after the temperature of the blackbody stops rising.

[0011] The available parameters are used to correct the current temperature of the surface source blackbody after the update.

[0012] In an optional embodiment of this specification, the available parameters are used to correct the updated current temperature of the surface source blackbody, including:

[0013] The updated current temperature of the surface source blackbody is corrected using the following formula:

[0014]

[0015] In the formula, t f This is the result obtained through correction; t s It is the current temperature of the surface source blackbody after the update; e is the natural exponent; Δu max It is the absolute value of the larger of the first electrode voltage increase and the second electrode voltage increase; Δu min It is the absolute value of the smaller of the first electrode voltage increase and the second electrode voltage increase; Δt is the temperature increase of the target temperature compared to the current temperature before the update; |Δu 0 | is the absolute value of the larger of the two increases in voltage between the first electrode and the second electrode.

[0016] In an optional embodiment of this specification, the available parameters are used to correct the updated current temperature of the surface source blackbody, including:

[0017] Determine the time taken from the execution of the target strategy until the temperature of the surface source blackbody no longer continues to rise;

[0018] The current temperature of the surface source blackbody is corrected using the available parameters and the duration.

[0019] In an optional embodiment of this specification, the updated current temperature of the surface source blackbody is corrected using the available parameters and the duration, including:

[0020] The updated current temperature of the surface source blackbody is corrected using the following formula:

[0021]

[0022] In the formula, L is the duration.

[0023] In an optional embodiment of this specification, the method is based on a surface-source blackbody, the extension direction of which of the first radiating elements is not parallel to the normal of the second radiating layer.

[0024] In an optional embodiment of this specification, the method is based on the surface source blackbody, wherein the extension direction of the second radiating element contained therein is parallel to the normal of the substrate.

[0025] In an optional embodiment of this specification, the first radiating layer includes a first sublayer and a second sublayer disposed side by side on the second radiating layer; the extending directions of the first radiating elements included in the first sublayer and the extending directions of the first radiating elements included in the second sublayer are not parallel.

[0026] Secondly, embodiments of this application also provide a radiation temperature error correction system for a high-temperature blackbody radiation source, characterized in that the system comprises:

[0027] A blackbody with a surface source includes: a substrate, a second radiating layer attached to one side of the substrate, and a first radiating layer attached to the side of the second radiating layer facing away from the substrate; the first radiating layer includes a plurality of first radiating units arranged sequentially along the second radiating layer; the second radiating layer includes a plurality of second radiating units arranged sequentially on the substrate; the blackbody with a surface source also includes a first electrode connected to the first radiating layer and a second electrode connected to the second radiating layer.

[0028] The error correction module is configured to: upon triggering a heating command, acquire the current temperature of the blackbody and the target temperature to be reached as indicated by the heating command; search a preset heating strategy library for a heating strategy that matches both the current temperature and the target temperature, and use this as the target strategy; wherein the heating strategy records the correspondence between the current temperature range, the target temperature range, the first electrode control method, and the second electrode control method; use the first electrode voltage increase based on the first electrode control method, the second electrode voltage increase based on the second electrode control method, and the temperature increase of the target temperature relative to the current temperature as available parameters; execute the target strategy, and update the current temperature of the blackbody after the temperature of the blackbody no longer increases; and use the available parameters to correct the updated current temperature of the blackbody.

[0029] Thirdly, embodiments of this application also provide an electronic device, including:

[0030] Processor; and

[0031] A memory configured to store computer-executable instructions, which, when executed, cause the processor to perform any of the methods described in the first aspect.

[0032] Fourthly, embodiments of this application also provide a computer-readable storage medium storing one or more programs that, when executed by an electronic device including multiple applications, cause the electronic device to perform any of the methods described in the first aspect.

[0033] The at least one technical solution adopted in the embodiments of this application can achieve the following beneficial effects: Using the radiation temperature error correction method for the high-temperature blackbody radiation source provided in this specification, based on the design of the surface source blackbody structure, a relatively stable emissivity and high radiation efficiency of the surface source blackbody are achieved. Furthermore, for the surface source blackbody provided in this application, a radiation temperature error correction method for the high-temperature blackbody radiation source is also proposed. Even if the emissivity of the surface source blackbody deviates from the ideal value or fluctuates, the method in this specification can correct the error between the actual temperature of the surface source blackbody and the target temperature, allowing the user to know the specific actual temperature of the surface source blackbody. Therefore, when the method in this specification is used to apply the surface source blackbody to the calibration and verification of temperature measurement products, it helps to improve the accuracy of the obtained results. Attached Figure Description

[0034] The accompanying drawings, which are included to provide a further understanding of this application and form part of this application, illustrate exemplary embodiments and are used to explain this application, but do not constitute an undue limitation of this application. In the drawings:

[0035] Figure 1 A schematic diagram of the surface source blackbody structure involved in a radiation temperature error correction method for a high-temperature blackbody radiation source provided in the embodiments of this specification.

[0036] Figure 2 A schematic diagram illustrating a method for correcting radiation temperature error in a high-temperature blackbody radiation source, as provided in the embodiments of this specification.

[0037] Figure 3 This is a schematic diagram of the structure of an electronic device as described in the embodiments of this specification;

[0038] 1-First radiation layer; 11-First sublayer; 13-Second sublayer;

[0039] 3-Second radiation layer;

[0040] 5-Base. Detailed Implementation

[0041] The present invention will now be described in further detail with reference to the accompanying drawings and specific embodiments. Similar elements in different embodiments are referred to by related similar element reference numerals. In the following embodiments, many details are described to facilitate a better understanding of the present application. However, those skilled in the art will readily recognize that some features may be omitted in different situations, or may be replaced by other elements, materials, or methods. In some cases, certain operations related to the present application are not shown or described in the specification. This is to avoid obscuring the core parts of the present application with excessive description. For those skilled in the art, detailed description of these related operations is not necessary; they can fully understand the related operations based on the description in the specification and general technical knowledge in the art.

[0042] Furthermore, the features, operations, or characteristics described in the specification can be combined in any suitable manner to form various embodiments. At the same time, the steps or actions in the method description can be rearranged or adjusted in a manner obvious to those skilled in the art. Therefore, the various orders in the specification and drawings are only for the clear description of a particular embodiment and do not imply a necessary order, unless otherwise stated that a particular order must be followed.

[0043] The serial numbers assigned to components in this document, such as "first" and "second," are used only to distinguish the described objects and have no sequential or technical meaning. The terms "connection" and "linkage" used in this application, unless otherwise specified, include both direct and indirect connections (linkages).

[0044] The technical solutions provided by the various embodiments of this application are described in detail below with reference to the accompanying drawings.

[0045] A blackbody is an idealized object that absorbs all incoming electromagnetic radiation without any reflection or transmission. In other words, a blackbody has an absorption coefficient of 1 and a transmission coefficient of 0 for any wavelength of electromagnetic radiation. Physicists use it as the standard object for studying thermal radiation. An object that completely absorbs all incoming electromagnetic radiation without any reflection or transmission is called an absolute blackbody, or simply a blackbody.

[0046] However, almost none of the real objects in nature are blackbodies. The radiation emitted by any real object depends not only on the wavelength of the radiation and the object's temperature, but also on factors such as the type of material used, the manufacturing method, the thermal process, the surface condition, and environmental conditions. Therefore, to make the blackbody radiation law applicable to all real objects, a proportionality coefficient related to material properties and surface condition, namely emissivity, must be introduced. This coefficient represents the degree to which the thermal radiation of a real object approximates blackbody radiation, and its value is between zero and less than 1. According to the radiation law, once the emissivity of a material is known, the infrared radiation characteristics of any object are known. The main factors affecting emissivity are: material type, surface roughness, physicochemical structure, and material thickness. Furthermore, during the heating process of a blackbody, factors affecting emissivity may also be affected by conditions such as temperature and heating rate, leading to a certain degree of change in the emissivity during the heating process, and also presenting problems such as measurement difficulties. In view of this, this application proposes a method for correcting the radiation temperature error of a high-temperature blackbody radiation source, specifically for a surface-source blackbody.

[0047] The radiation temperature error correction method for high-temperature blackbody radiation sources described in this specification applies to surface blackbody sources, such as... Figure 1 As shown, it includes: a substrate 5, a second radiating layer 3 attached to one side of the substrate 5, and a first radiating layer 1 attached to the side of the second radiating layer 3 facing away from the substrate 5. In an optional embodiment of this specification, the substrate 5 may be a thermosetting adhesive, and this specification does not impose specific limitations on the thickness of the substrate 5.

[0048] The first radiating layer 1 comprises a plurality of first radiating units arranged sequentially along the second radiating layer 3. The second radiating layer 3 comprises a plurality of second radiating units arranged sequentially on the substrate 5. Optionally, each first radiating unit is a carbon nanotube, and each second radiating unit is a carbon nanotube. The dimension of the first radiating unit in its extension direction is larger than the dimension of the second radiating unit in its extension direction. Figure 1 The textures on the first radiating layer 1 and the second radiating layer 3 shown can be considered as the extension direction of the carbon nanotubes. The first radiating layer 1 may also include a substrate (optionally, the substrate is a material with high light transmittance, such as glass). The first radiating units are grown on the substrate. Then, the first radiating layer 1, containing the substrate and the first radiating units, is coated onto the second radiating layer 3, thus achieving the connection between the first radiating layer 1 and the second radiating layer 3. In this specification, the extension direction of the carbon nanotubes is the axial direction of the carbon nanotubes.

[0049] In an optional embodiment of this specification, the extension direction of the first radiating unit included in the surface-source blackbody is not parallel to the normal direction of the second radiating layer 3. This design, on the one hand, can reduce the impact of the uneven growth of carbon nanotubes on the surface smoothness of the first radiating layer 1 on the emissivity of the surface-source blackbody; on the other hand, it also helps to increase the distribution density of carbon nanotubes along the normal direction of the second radiating layer 3, which is beneficial to improving radiation efficiency. The term "parallel" in this specification means "generally parallel, with most of the carbon nanotubes extending in parallel directions," rather than an absolute concept. In reality, absolute parallelism is almost impossible to achieve.

[0050] In another optional embodiment of this specification, the extension direction of the second radiating unit included in the surface-source blackbody is parallel to the normal direction of the substrate 5. This design, on the one hand, avoids the carbon nanotubes themselves from blocking the electromagnetic waves emitted by the second radiating unit, and on the other hand, simplifies the molding process.

[0051] It should be noted that the extension directions of the first and second radiating units mentioned in this specification are their general, macroscopic extension directions. In actual production, carbon nanotubes may not have strictly uniform growth directions, and this phenomenon is also within the scope of the technical solutions described in this specification.

[0052] To further improve the uniformity of radiation from the surface-source blackbody, in a further optional embodiment of this specification, the first radiation layer 1 includes a first sub-layer 11 and a second sub-layer 13 arranged side-by-side on the second radiation layer 3; the extension directions of the first radiation units included in the first sub-layer 11 and the second sub-layer 13 are not parallel. Specifically, the radiation units on the first sub-layer 11 and the second sub-layer 13 all extend upwards at an angle towards the center of the surface-source blackbody. In this embodiment, the first sub-layer 11 and the second sub-layer 13 can be formed separately, and then spliced ​​onto the second radiation layer 3. This embodiment can at least ensure that the temperature in the middle part of the surface-source blackbody is uniform, and when applied to high-temperature scenarios, it can also ensure that the middle part of the surface-source blackbody has a high heating rate.

[0053] Furthermore, the blackbody in this specification also includes a first electrode connected to the first radiating layer 1 and a second electrode connected to the second radiating layer 3. The first electrode is used to control the radiation of the first radiating layer 1, and the second electrode is used to control the radiation of the second radiating layer 3. The overall radiation of the blackbody is formed by the superposition of the first radiating layer 1 and the second radiating layer 3. Optionally, both the first electrode and the second electrode control their respective radiating layers by adjusting the voltage.

[0054] The surface blackbody and error correction module in this specification together constitute the radiation temperature error correction system of the high-temperature blackbody radiation source. The error correction module is connected to the surface blackbody, and the methods in this specification are executed by the error correction module. Figure 2 As shown, the steps for error correction implemented by the error correction module will now be explained:

[0055] S200: Upon triggering a heating command, obtain the current temperature of the surface source blackbody and the target temperature to be reached as indicated by the heating command.

[0056] The current temperature in this step is the temperature of the surface source blackbody at the current moment. If the method in this specification was also triggered by the previous heating command, the current temperature is the temperature obtained after the previous heating and the "updated" temperature mentioned later in this specification.

[0057] In practical applications of surface-source blackbodies, users may need to adjust the temperature of the blackbodies based on their usage requirements. In such cases, a temperature increase command can be generated based on the user's temperature adjustment operation. The temperature increase command in this manual can be a string of characters, and its function includes at least a temperature increase indication and the target temperature that the surface-source blackbodies should reach (i.e., the target temperature).

[0058] S202: Find a heating strategy that matches both the current temperature and the target temperature from the preset heating strategy library, and use it as the target strategy.

[0059] The heating strategy library in this manual is based on a pre-set database of human experience. Since the surface source blackbody structure in this manual is fixed, technicians can construct the heating strategy library based on the temperature accuracy requirements of the applicable scenarios of the surface source blackbody through calculation and experimentation.

[0060] The heating strategy library can be a database containing rows and columns, representing the correspondence between elements in those rows and columns, such as a table. The heating strategy records in this specification record the correspondence between the current temperature range (e.g., the current temperature range as rows), the target temperature range (e.g., the target temperature range as columns), the first electrode control method, and the second electrode control method (e.g., as elements). Techniques based on tables used in related technologies are applicable to this specification.

[0061] The electrode (including the first electrode and the second electrode) control method indicates, on the one hand, the amount of voltage increase of the corresponding electrode; on the other hand, it also indicates the timing of the voltage increase of the electrode (for example, the second electrode starts to increase voltage 10ms after the first electrode starts to increase voltage).

[0062] In practical applications, if the search results are not unique, the result with the largest electrode voltage change represented by the first electrode control method will be used as the target strategy. The first electrode is the most sensitive to the control of the surface source blackbody, and this embodiment improves the heating efficiency of the surface source blackbody.

[0063] S204: The increase in the first electrode voltage obtained based on the first electrode control method, the increase in the second electrode voltage obtained based on the second electrode control method, and the increase in the target temperature relative to the current temperature are used as available parameters.

[0064] S206: Execute the target strategy, and after the temperature of the surface source blackbody no longer continues to rise, update the current temperature of the surface source blackbody.

[0065] The method of executing the target strategy is to control the first and second electrodes according to the electrode control method expressed by the target strategy, so as to achieve the heating of the surface source blackbody.

[0066] The phrase "the temperature of the blackbody no longer continues to rise" in this specification means that the blackbody has theoretically reached the target temperature, but in reality, there may be a certain deviation from the target temperature, and the temperature of the blackbody may fluctuate due to various factors such as the environment. The criteria for determining that the blackbody temperature no longer continues to rise can be: after a specified time (a preset value, which can be obtained empirically) following the completion of the target strategy, the blackbody is considered to have stopped heating. Alternatively, after a specified time following the completion of the target strategy, if no voltage fluctuation of the first or second electrode greater than the fluctuation threshold (a preset value, which can be obtained empirically) can be detected, the blackbody is considered to have stopped heating.

[0067] The update in this step indicates that, based on the execution of the target strategy, the temperature of the blackbody has essentially approached the target temperature. Ideally, if the blackbody is a perfect blackbody, the electrode control does not incur additional charge loss, and other factors affecting the blackbody's radiation are ignored, then the updated current temperature is the target temperature. However, reality is not ideal. In such cases, the updated current temperature (i.e., the target temperature) often differs somewhat from the actual temperature.

[0068] In an optional embodiment of this specification, the radiation temperature error correction of the high-temperature blackbody radiation source further includes a display module. The display module is used to display the current temperature and / or the target temperature. The result of the correction obtained through this specification (i.e., the actual temperature) can also be displayed on the display module.

[0069] S208: Using the available parameters, correct the current temperature of the surface source blackbody after the update.

[0070] Absolute blackbodies do not exist in nature. The calibration and verification of temperature measurement products such as radiation thermometers based on blackbody radiation sources are mostly performed under the assumption that the blackbody radiation source used during testing is an absolute blackbody. This leads to distortions in the calibration and verification results due to the influence of the blackbody radiation source. Furthermore, in some calibration and verification scenarios, the emissivity of the blackbody radiation source is used as the basis for determining the calibration and verification results. However, in high-precision, continuous temperature measurement scenarios, the temperature of the blackbody radiation source needs to rise to a certain value, and the emissivity of the blackbody radiation source may change, thus affecting the accuracy of the calibration and verification results. In view of this, this application provides a surface-source blackbody. Based on the structural design of the surface-source blackbody, it achieves the technical effects of relatively stable emissivity and high radiation efficiency. Furthermore, for the surface blackbody provided in this application, a method for correcting the radiation temperature error of a high-temperature blackbody radiation source is proposed. Even if the emissivity of the surface blackbody deviates from the ideal value or fluctuates, the method described in this specification can correct the error between the actual temperature of the surface blackbody and the target temperature, allowing the user to know the specific actual temperature of the surface blackbody. Therefore, when using the method described in this specification to apply the surface blackbody to the calibration and verification of temperature measurement products, it helps to improve the accuracy of the results obtained.

[0071] In a further optional embodiment of this specification, the target temperature range for which the method described herein is applicable is 900 degrees Celsius to 1200 degrees Celsius.

[0072] This specification describes, in one embodiment, how corrections are made based on available parameters. Specifically, the updated current temperature of the surface source blackbody is corrected using the following formula (a):

[0073]

[0074] In the formula, t f This is the result obtained through correction; t s It is the current temperature of the surface source blackbody after the update; e is the natural exponent; Δu max It is the absolute value of the larger of the first electrode voltage increase and the second electrode voltage increase; Δu min It is the absolute value of the smaller of the first electrode voltage increase and the second electrode voltage increase; Δt is the temperature increase of the target temperature compared to the current temperature before the update; |Δu 0 | is the absolute value of the larger of the increases in voltage at the first electrode and the increases in voltage at the second electrode. The voltage is measured in volts, and the temperature in millidegrees Celsius.

[0075] The blackbody in this specification comprises two radiating layers: a first radiating layer 1 and a second radiating layer 3. These two radiating layers are interconnected and not independent. Voltage control of one radiating layer will cause slight changes in the adjacent radiating layer, potentially affecting the overall emissivity of the blackbody. The correction for the current temperature of the blackbody in this application, achieved through this formula, combines the voltage increase of the first electrode, the voltage increase of the second electrode, and the difference between the current temperature and the target temperature before implementing the target strategy. This results in a more accurate correction and better reflects the actual situation of the blackbody in this application.

[0076] In a further optional embodiment of this specification, in addition to using available parameters for correction, the duration of the heating process is also considered in correcting the updated current temperature. In this embodiment, the time taken from the execution of the target strategy until the temperature of the blackbody stops increasing is first determined. Then, the updated current temperature of the blackbody is corrected using the available parameters and the duration. Afterwards, the updated current temperature is corrected using the following formula (ii).

[0077]

[0078] In the formula, L is the time taken from the execution of the target strategy until the temperature of the surface source blackbody stops rising. The unit of time is milliseconds.

[0079] The heating time reflects the influence of the blackbody's structure on temperature uniformity. This temperature uniformity may cause slight temperature differences in different regions of the blackbody. Incorporating this difference into the correction calculation can, to some extent, overcome the errors caused by the blackbody's structure.

[0080] It is understood that the radiation temperature error correction system of the high-temperature blackbody radiation source described above can realize each step of the radiation temperature error correction method of the high-temperature blackbody radiation source provided in the foregoing embodiments. The radiation temperature error correction system of the high-temperature blackbody radiation source will not be described in detail here.

[0081] Figure 3 This is a schematic diagram of the structure of an electronic device according to an embodiment of this application. Please refer to it. Figure 3At the hardware level, the electronic device includes a processor, and optionally also includes an internal bus, a network interface, and memory. The memory may include main memory, such as high-speed random-access memory (RAM), or non-volatile memory, such as at least one disk drive. Of course, the electronic device may also include other hardware required for other business operations.

[0082] The processor, network interface, and memory can be interconnected via an internal bus, which can be an ISA (Industry Standard Architecture) bus, a PCI (Peripheral Component Interconnect) bus, or an EISA (Extended Industry Standard Architecture) bus, etc. This bus can be divided into address bus, data bus, control bus, etc. For ease of representation, Figure 3 The symbol is represented by a single double-headed arrow, but this does not mean that there is only one bus or one type of bus.

[0083] Memory is used to store programs. Specifically, programs may include program code, which includes computer operation instructions. Memory may include main memory and non-volatile memory, and provides instructions and data to the processor.

[0084] The processor reads the corresponding computer program from non-volatile memory into main memory and then runs it, forming a radiation temperature error correction device for a high-temperature blackbody radiation source at the logical level. The processor executes the program stored in memory and specifically performs any of the aforementioned radiation temperature error correction methods for a high-temperature blackbody radiation source.

[0085] The above is as stated in this application. Figure 2The radiation temperature error correction method for a high-temperature blackbody radiation source disclosed in the illustrated embodiment can be applied to a processor or implemented by a processor. The processor may be an integrated circuit chip with signal processing capabilities. During implementation, each step of the above method can be completed by integrated logic circuits in the processor's hardware or by instructions in software form. The processor can be a general-purpose processor, including a Central Processing Unit (CPU), a Network Processor (NP), etc.; it can also be 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. It can implement or execute the methods, steps, and logic block diagrams disclosed in the embodiments of this application. The general-purpose processor can be a microprocessor or any conventional processor. The steps of the method disclosed in the embodiments of this application can be directly manifested as execution by a hardware decoding processor, or execution by a combination of hardware and software modules in the decoding processor. The software module can reside in a mature storage medium in the field, such as random access memory, flash memory, read-only memory, programmable read-only memory, electrically erasable programmable memory, or registers. This storage medium is located in memory, and the processor reads information from the memory and, in conjunction with its hardware, completes the steps of the above method.

[0086] The electronic device can also perform Figure 2 A method for correcting the radiation temperature error of a high-temperature blackbody radiation source is proposed and implemented. Figure 2 The functions of the embodiments shown are not described in detail here.

[0087] This application also proposes a computer-readable storage medium that stores one or more programs, the programs including instructions that, when executed by an electronic device including multiple applications, enable the electronic device to perform... Figure 2 The embodiment shown illustrates a method for performing a radiation temperature error correction device for a high-temperature blackbody radiation source, specifically used to perform any of the aforementioned radiation temperature error correction methods for a high-temperature blackbody radiation source.

[0088] Those skilled in the art will understand that embodiments of this application can be provided as methods, systems, or computer program products. Therefore, this application can take the form of a completely hardware embodiment, a completely software embodiment, or an embodiment combining software and hardware aspects. Furthermore, this application can take the form of a computer program product embodied on one or more computer-usable storage media (including but not limited to disk storage, CD-ROM, optical storage, etc.) containing computer-usable program code.

[0089] This application is described with reference to flowchart illustrations and / or block diagrams of methods, apparatus (systems), and computer program products according to embodiments of this application. It will be understood that each block of the flowchart illustrations and / or block diagrams, and combinations of blocks in the flowchart illustrations and / or block diagrams, can be implemented by computer program instructions. These computer program instructions can be provided to a processor of a general-purpose computer, special-purpose computer, embedded processor, or other programmable data processing apparatus to produce a machine, such that the instructions, which execute via the processor of the computer or other programmable data processing apparatus, generate instructions for implementing the flowchart... Figure 1 One or more processes and / or boxes Figure 1 A device that provides the functions specified in one or more boxes.

[0090] These computer program instructions may also be stored in a computer-readable storage medium that can direct a computer or other programmable data processing device to function in a particular manner, such that the instructions stored in the computer-readable storage medium produce an article of manufacture including instruction means, which are implemented in a process Figure 1 One or more processes and / or boxes Figure 1 The function specified in one or more boxes.

[0091] These computer program instructions may also be loaded onto a computer or other programmable data processing equipment to cause a series of operational steps to be performed on the computer or other programmable equipment to produce a computer-implemented process, thereby providing instructions that execute on the computer or other programmable equipment for implementing the process. Figure 1 One or more processes and / or boxes Figure 1 The steps of the function specified in one or more boxes.

[0092] In a typical configuration, a computing device includes one or more processors (CPU), input / output interfaces, network interfaces, and memory.

[0093] Memory may include non-persistent storage in computer-readable media, such as random access memory (RAM) and / or non-volatile memory, such as read-only memory (ROM) or flash RAM. Memory is an example of computer-readable media.

[0094] Computer-readable media includes both permanent and non-permanent, removable and non-removable media that can store information using any method or technology. Information can be computer-readable instructions, data structures, modules of programs, or other data. Examples of computer storage media include, but are not limited to, phase-change memory (PRAM), static random access memory (SRAM), dynamic random access memory (DRAM), other types of random access memory (RAM), read-only memory (ROM), electrically erasable programmable read-only memory (EEPROM), flash memory or other memory technologies, CD-ROM, digital versatile optical disc (DVD) or other optical storage, magnetic tape, magnetic magnetic disk storage or other magnetic storage devices, or any other non-transferable medium that can be used to store information accessible by a computing device. As defined herein, computer-readable media does not include transient computer-readable media, such as modulated data signals and carrier waves.

[0095] It should also be noted that 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 limitation, 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.

[0096] Those skilled in the art will understand that embodiments of this application can be provided as methods, systems, or computer program products. Therefore, this application can take the form of a completely hardware embodiment, a completely software embodiment, or an embodiment combining software and hardware aspects. Furthermore, this application can take the form of a computer program product embodied on one or more computer-usable storage media (including, but not limited to, disk storage, CD-ROM, optical storage, etc.) containing computer-usable program code.

[0097] The above description is merely an embodiment of this application and is not intended to limit the scope of this application. Various modifications and variations can be made to this application by those skilled in the art. Any modifications, equivalent substitutions, improvements, etc., made within the spirit and principles of this application should be included within the scope of the claims of this application.

Claims

1. A method for correcting the radiation temperature error of a high-temperature blackbody radiation source, characterized in that, The method is based on a surface source blackbody, which includes: a substrate, a second radiation layer attached to one side of the substrate, and a first radiation layer attached to the side of the second radiation layer facing away from the substrate; the first radiation layer includes a plurality of first radiation units arranged sequentially along the second radiation layer; the second radiation layer includes a plurality of second radiation units arranged sequentially on the substrate. The blackbody further includes a first electrode connected to the first radiating layer and a second electrode connected to the second radiating layer; the method includes: Upon triggering a heating command, the current temperature of the surface source blackbody and the target temperature to be reached as indicated by the heating command are obtained. A heating strategy that matches both the current temperature and the target temperature is found in a preset heating strategy library and is used as the target strategy; wherein, the heating strategy records the correspondence between the current temperature range, the target temperature range, the first electrode control method, and the second electrode control method; The first electrode voltage rise obtained based on the first electrode control method, the second electrode voltage rise obtained based on the second electrode control method, and the temperature rise of the target temperature relative to the current temperature are used as available parameters; The target strategy is executed, and the current temperature of the blackbody is updated after the temperature of the blackbody stops rising. The available parameters are used to correct the current temperature of the surface source blackbody after the update.

2. The method as described in claim 1, characterized in that, Using the available parameters, the current temperature of the surface source blackbody after the update is corrected, including: The updated current temperature of the surface source blackbody is corrected using the following formula: In the formula, It is the result obtained through correction; It is the current temperature of the surface source blackbody after the update; e is the natural index; It is the absolute value of the larger of the first electrode voltage increase and the second electrode voltage increase; It is the absolute value of the smaller of the first electrode voltage increase and the second electrode voltage increase; It is the temperature increase of the target temperature compared to the current temperature before the update; It is the absolute value of the larger of the two increases in voltage between the first electrode and the second electrode.

3. The method as described in claim 2, characterized in that, Using the available parameters, the current temperature of the surface source blackbody after the update is corrected, including: Determine the time taken from the execution of the target strategy until the temperature of the surface source blackbody no longer continues to rise; The current temperature of the surface source blackbody is corrected using the available parameters and the duration.

4. The method as described in claim 3, characterized in that, Using the available parameters and the duration, the current temperature of the surface source blackbody after the update is corrected, including: The updated current temperature of the surface source blackbody is corrected using the following formula: In the formula, L is the duration.

5. The method as described in claim 1, characterized in that, The method is based on a surface-source blackbody, in which the extension direction of the first radiating element is not parallel to the normal of the second radiating layer.

6. The method as described in claim 1, characterized in that, The method is based on a surface-source blackbody, wherein the extension direction of the second radiating element contained therein is parallel to the normal of the substrate.

7. The method as described in claim 5, characterized in that, The first radiating layer includes a first sub-layer and a second sub-layer arranged side by side on the second radiating layer; the extension direction of the first radiating element included in the first sub-layer and the extension direction of the first radiating element included in the second sub-layer are not parallel.

8. A radiation temperature error correction system for a high-temperature blackbody radiation source, characterized in that, The system includes: A blackbody with a surface source includes: a substrate, a second radiating layer attached to one side of the substrate, and a first radiating layer attached to the side of the second radiating layer facing away from the substrate; the first radiating layer includes a plurality of first radiating units arranged sequentially along the second radiating layer; the second radiating layer includes a plurality of second radiating units arranged sequentially on the substrate; the blackbody with a surface source also includes a first electrode connected to the first radiating layer and a second electrode connected to the second radiating layer. The error correction module is configured to: upon triggering a heating command, acquire the current temperature of the blackbody and the target temperature to be reached as indicated by the heating command; search a preset heating strategy library for a heating strategy that matches both the current temperature and the target temperature, and use this as the target strategy; wherein the heating strategy records the correspondence between the current temperature range, the target temperature range, the first electrode control method, and the second electrode control method; use the first electrode voltage increase based on the first electrode control method, the second electrode voltage increase based on the second electrode control method, and the temperature increase of the target temperature relative to the current temperature as available parameters; execute the target strategy, and update the current temperature of the blackbody after the temperature of the blackbody no longer increases; and use the available parameters to correct the updated current temperature of the blackbody.

9. An electronic device, comprising: processor; as well as A memory configured to store computer-executable instructions, which, when executed, cause the processor to perform the method of any one of claims 1 to 7.

10. A computer-readable storage medium storing one or more programs, which, when executed by an electronic device including a plurality of applications, cause the electronic device to perform the method of any one of claims 1 to 7.

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