Alarm method, device, electronic equipment and medium for satellite testing

Abstract

The present application provides an alarm method, device, electronic device and medium for satellite testing, the method comprising: obtaining the actual voltage of the physical interface end of the satellite core control end and obtaining the transmission efficiency of the test data between the satellite core control end and the ground test computer end; determining whether there is a power supply safety hazard at the physical interface end of the satellite core control end according to the voltage difference between the actual voltage of the physical interface end of the satellite core control end and the standard operating voltage of the physical interface end of the satellite core control end, and determining whether there is a data transmission safety hazard at the physical interface end of the satellite core control end according to the transmission efficiency; if there is a power supply safety hazard, a first alarm is issued on the ground test computer end, and, if there is a data transmission safety hazard, a second alarm is issued on the ground test computer end. The present application can prevent engineers from further using the satellite test terminal to test the satellite when an error occurs in the satellite.

Description

Technical Field

[0001] The present application relates to the field of satellite testing technology, and in particular to an alarm method, device, electronic equipment and medium for satellite testing. Background Art

[0002] Satellite testing runs through the entire process of satellite development and production, and the testing time directly determines the development and production cycle of the satellite. With the steady development of my country's aerospace industry, the number of satellites is increasing, which requires improving the testing efficiency while ensuring the quality of satellite testing. According to traditional satellite testing technology, it takes at least several months to complete the production and testing of a satellite. When an error occurs in the satellite, the test system requires engineers to eliminate the error one by one. If the engineer still tests the satellite when an error occurs, the scope of the fault may be expanded and the efficiency of the test may be reduced. Summary of the invention

[0003] In view of this, the purpose of the present application is to provide an alarm method, device, electronic device and medium for satellite testing, which can prevent engineers from further using a satellite test terminal to test the satellite when an error occurs in the satellite.

[0004] In a first aspect, an embodiment of the present application provides an alarm method for satellite testing, the method comprising:

[0005] Acquire the actual voltage of the physical interface end of the satellite core control end in real time, and acquire the transmission efficiency of the test data between the satellite core control end and the ground test computer end, wherein the physical interface end of the satellite core control end is electrically connected to the physical interface end of the ground test computer end through a transmission cable, and the test data is transmitted through the transmission cable;

[0006] Determine whether there is a power supply safety hazard at the physical interface of the satellite core control end according to a voltage difference between an actual voltage at the physical interface of the satellite core control end and a standard operating voltage at the physical interface of the satellite core control end, and determine whether there is a data transmission safety hazard at the physical interface of the satellite core control end according to the transmission efficiency;

[0007] If the power supply safety hazard exists, a first alarm is issued on the ground test computer side, and if the data transmission safety hazard exists, a second alarm is issued on the ground test computer side, wherein when the first alarm and / or the second alarm is issued on the ground test computer side, the ground test computer side does not respond to any operation instructions directed to the satellite core control side.

[0008] In a possible implementation manner, obtaining the transmission efficiency of the test data between the satellite core control terminal and the ground test computer terminal includes:

[0009] Using the ground test computer to send the test data to the satellite core control terminal, wherein the test data includes a preset number of test instructions;

[0010] Using the satellite core control terminal to return the test instruction received by the satellite core control terminal to the ground test computer terminal;

[0011] The ratio of the number of target test instructions to the preset number is calculated, and the ratio is used as the transmission efficiency, wherein the target test instructions are test instructions received by the ground test computer and returned by the satellite core control terminal.

[0012] In a possible implementation manner, determining whether there is a power supply safety hazard at the physical interface end of the satellite core control end according to a voltage difference between an actual voltage at the physical interface end of the satellite core control end and a standard operating voltage at the physical interface end of the satellite core control end includes:

[0013] If the voltage difference between the actual voltage of the physical interface end of the satellite core control end and the standard operating voltage of the physical interface end of the satellite core control end is greater than a first preset voltage threshold, or the voltage difference between the actual voltage of the physical interface end of the satellite core control end and the standard operating voltage of the physical interface end of the satellite core control end is less than a second preset voltage threshold, it is determined that the physical interface end of the satellite core control end has the power supply safety hazard, wherein the first preset voltage threshold is greater than 0, and the second preset voltage threshold is less than 0;

[0014] If the voltage difference between the actual voltage of the physical interface end of the satellite core control end and the standard operating voltage of the physical interface end of the satellite core control end is between the first preset voltage threshold and the second preset voltage threshold, it is determined that the physical interface end of the satellite core control end does not have the power supply safety hazard.

[0015] In a possible implementation manner, issuing a first alarm on the ground test computer terminal includes:

[0016] According to the voltage difference between the actual voltage of the physical interface end of the satellite core control end and the standard operating voltage of the physical interface end of the satellite core control end, a first alarm is issued on the ground test computer end.

[0017] In a possible implementation manner, according to the voltage difference between the actual voltage of the physical interface terminal of the satellite core control terminal and the standard operating voltage of the physical interface terminal of the satellite core control terminal, a first alarm is issued on the ground test computer terminal, including:

[0018] If the voltage difference between the actual voltage of the physical interface terminal of the satellite core control terminal and the standard operating voltage of the physical interface terminal of the satellite core control terminal is less than the second preset voltage threshold, a yellow alarm mark is generated on the ground test computer terminal;

[0019] If the voltage difference between the actual voltage of the physical interface end of the satellite core control end and the standard operating voltage of the physical interface end of the satellite core control end is greater than the first preset voltage threshold, a red alarm mark is generated on the ground test computer end.

[0020] In a possible implementation, the method further includes:

[0021] Draw an actual voltage curve graph according to the actual voltage of the physical interface terminal of the satellite core control terminal at a plurality of consecutive moments;

[0022] The actual voltage curve graph is displayed on the ground test computer terminal.

[0023] In a second aspect, an embodiment of the present application further provides an alarm method device for satellite testing, the device comprising:

[0024] An acquisition module is used to acquire in real time the actual voltage of the physical interface end of the satellite core control end, and to acquire the transmission efficiency of the test data between the satellite core control end and the ground test computer end, wherein the physical interface end of the satellite core control end is electrically connected to the physical interface end of the ground test computer end through a transmission cable, and the test data is transmitted through the transmission cable;

[0025] A potential safety hazard determination module is used to determine whether there is a potential safety hazard in power supply at the physical interface of the satellite core control end according to a voltage difference between an actual voltage at the physical interface of the satellite core control end and a standard operating voltage at the physical interface of the satellite core control end, and to determine whether there is a potential safety hazard in data transmission at the physical interface of the satellite core control end according to the transmission efficiency;

[0026] The alarm module is used to issue a first alarm on the ground test computer end if the power supply safety hazard exists, and to issue a second alarm on the ground test computer end if the data transmission safety hazard exists, wherein when the first alarm and / or the second alarm is issued on the ground test computer end, the ground test computer end does not respond to any operation instructions directed to the satellite core control end.

[0027] In a possible implementation manner, when acquiring the transmission efficiency of the test data between the satellite core control terminal and the ground test computer terminal, the acquisition module is specifically used to:

[0028] Using the ground test computer to send the test data to the satellite core control terminal, wherein the test data includes a preset number of test instructions;

[0029] Using the satellite core control terminal to return the test instruction received by the satellite core control terminal to the ground test computer terminal;

[0030] The ratio of the number of target test instructions to the preset number is calculated, and the ratio is used as the transmission efficiency, wherein the target test instructions are test instructions received by the ground test computer and returned by the satellite core control terminal.

[0031] In a possible implementation manner, the potential safety hazard determination module, when determining whether there is a power supply potential safety hazard at the physical interface end of the satellite core control end according to the voltage difference between the actual voltage of the physical interface end of the satellite core control end and the standard operating voltage of the physical interface end of the satellite core control end, is specifically used to:

[0032] If the voltage difference between the actual voltage of the physical interface end of the satellite core control end and the standard operating voltage of the physical interface end of the satellite core control end is greater than a first preset voltage threshold, or the voltage difference between the actual voltage of the physical interface end of the satellite core control end and the standard operating voltage of the physical interface end of the satellite core control end is less than a second preset voltage threshold, it is determined that the physical interface end of the satellite core control end has the power supply safety hazard, wherein the first preset voltage threshold is greater than 0, and the second preset voltage threshold is less than 0;

[0033] If the voltage difference between the actual voltage of the physical interface end of the satellite core control end and the standard operating voltage of the physical interface end of the satellite core control end is between the first preset voltage threshold and the second preset voltage threshold, it is determined that the physical interface end of the satellite core control end does not have the power supply safety hazard.

[0034] When the alarm module issues the first alarm on the ground test computer, it is specifically used to:

[0035] According to the voltage difference between the actual voltage of the physical interface end of the satellite core control end and the standard operating voltage of the physical interface end of the satellite core control end, a first alarm is issued on the ground test computer end.

[0036] The alarm module is specifically used for: when the first alarm is issued on the ground test computer end according to the voltage difference between the actual voltage of the physical interface end of the satellite core control end and the standard working voltage of the physical interface end of the satellite core control end:

[0037] If the voltage difference between the actual voltage of the physical interface terminal of the satellite core control terminal and the standard operating voltage of the physical interface terminal of the satellite core control terminal is less than the second preset voltage threshold, a yellow alarm mark is generated on the ground test computer terminal;

[0038] If the voltage difference between the actual voltage of the physical interface end of the satellite core control end and the standard operating voltage of the physical interface end of the satellite core control end is greater than the first preset voltage threshold, a red alarm mark is generated on the ground test computer end.

[0039] In a possible implementation, the device further includes:

[0040] A drawing module, used for drawing an actual voltage curve graph according to the actual voltage of the physical interface terminal of the satellite core control terminal at a plurality of consecutive moments;

[0041] A display module is used to display the actual voltage curve graph on the ground test computer terminal.

[0042] In a third aspect, an embodiment of the present application further provides an electronic device, comprising: a processor, a storage medium and a bus, wherein the storage medium stores machine-readable instructions executable by the processor, and when the electronic device is running, the processor communicates with the storage medium through the bus, and the processor executes the machine-readable instructions to perform the steps of the alarm method for satellite testing described in any one of the first aspects.

[0043] In a fourth aspect, an embodiment of the present application further provides a computer-readable storage medium, on which a computer program is stored. When the computer program is executed by a processor, the steps of the alarm method for satellite testing as described in any one of the first aspects are executed.

[0044] An alarm method, device, electronic device and medium for satellite testing provided in an embodiment of the present application can prevent engineers from further using a satellite test terminal to test a satellite when an error occurs in the satellite. BRIEF DESCRIPTION OF THE DRAWINGS

[0045] In order to more clearly illustrate the technical solutions of the embodiments of the present application, the drawings required for use in the embodiments will be briefly introduced below. It should be understood that the following drawings only show certain embodiments of the present application and therefore should not be regarded as limiting the scope. For ordinary technicians in this field, other related drawings can be obtained based on these drawings without paying creative work.

[0046] Figure 1 A flowchart of an alarm method for satellite testing provided by an embodiment of the present application is shown;

[0047] Figure 2 A flowchart of another alarm method for satellite testing provided by an embodiment of the present application is shown;

[0048] Figure 3 A flowchart of another alarm method for satellite testing provided by an embodiment of the present application is shown;

[0049] Figure 4 A schematic diagram of the structure of an alarm method device for satellite testing provided by an embodiment of the present application is shown;

[0050] Figure 5 A schematic structural diagram of an electronic device provided in an embodiment of the present application is shown. DETAILED DESCRIPTION

[0051] To make the purpose, technical scheme and advantages of the embodiments of the present application clearer, the technical scheme in the embodiments of the present application will be clearly and completely described below in conjunction with the drawings in the embodiments of the present application. It should be understood that the drawings in the present application only serve the purpose of explanation and description and are not used to limit the scope of protection of the present application. In addition, it should be understood that the schematic drawings are not drawn in real proportion. The flowchart used in this application shows the operations implemented according to some embodiments of the present application. It should be understood that the operations of the flowchart can be implemented out of sequence, and the steps without logical context can be reversed in order or implemented simultaneously. In addition, those skilled in the art can add one or more other operations to the flowchart under the guidance of the content of the present application, or remove one or more operations from the flowchart.

[0052] In addition, the described embodiments are only a part of the embodiments of the present application, rather than all the embodiments. The components of the embodiments of the present application described and shown in the drawings here can be arranged and designed in various configurations. Therefore, the following detailed description of the embodiments of the present application provided in the drawings is not intended to limit the scope of the application claimed for protection, but merely represents the selected embodiments of the present application. Based on the embodiments of the present application, all other embodiments obtained by those skilled in the art without making creative work belong to the scope of protection of the present application.

[0053] It should be noted that the term "comprising" will be used in the embodiments of the present application to indicate the existence of the features declared thereafter, but does not exclude the addition of other features.

[0054] To facilitate understanding of this embodiment, an alarm method, device, electronic device and medium for satellite testing provided in an embodiment of the present application are introduced in detail.

[0055] Reference Figure 1 As shown, it is a flow chart of an alarm method for satellite testing provided by an embodiment of the present application, and the method includes:

[0056] S101, obtaining in real time the actual voltage of the physical interface end of the satellite core control end, and obtaining the transmission efficiency of the test data between the satellite core control end and the ground test computer end, wherein the physical interface end of the satellite core control end is electrically connected to the physical interface end of the ground test computer end through a transmission cable, and the test data is transmitted through the transmission cable;

[0057] S102, determining whether there is a power supply safety hazard at the physical interface of the satellite core control end according to a voltage difference between an actual voltage at the physical interface of the satellite core control end and a standard operating voltage at the physical interface of the satellite core control end, and determining whether there is a data transmission safety hazard at the physical interface of the satellite core control end according to the transmission efficiency;

[0058] S103. If the power supply safety hazard exists, a first alarm is issued on the ground test computer side, and if the data transmission safety hazard exists, a second alarm is issued on the ground test computer side, wherein when the first alarm and / or the second alarm is issued on the ground test computer side, the ground test computer side does not respond to any operation instructions directed to the satellite core control side.

[0059] Reference Figure 2As shown, it is a flow chart of another alarm method for satellite testing provided by an embodiment of the present application. In a possible implementation manner, obtaining the transmission efficiency of test data between the satellite core control terminal and the ground test computer terminal includes:

[0060] S201, using the ground test computer to send the test data to the satellite core control terminal, wherein the test data includes a preset number of test instructions;

[0061] Exemplarily, the preset number may be 100.

[0062] S202, using the satellite core control terminal to return the test instruction received by the satellite core control terminal to the ground test computer terminal;

[0063] S203. Calculate the ratio of the number of target test instructions to the preset number, and use the ratio as the transmission efficiency, wherein the target test instruction is the test instruction received by the ground test computer and returned by the satellite core control end.

[0064] Assuming that in step S202 the satellite core control terminal receives 99 test instructions and the ground test computer receives 98 test instructions returned by the satellite core control terminal, the transmission efficiency of the test data is 98% (98 / 100).

[0065] In a possible implementation manner, determining whether there is a power supply safety hazard at the physical interface end of the satellite core control end according to a voltage difference between an actual voltage at the physical interface end of the satellite core control end and a standard operating voltage at the physical interface end of the satellite core control end includes:

[0066] If the voltage difference between the actual voltage of the physical interface end of the satellite core control end and the standard operating voltage of the physical interface end of the satellite core control end is greater than a first preset voltage threshold, or the voltage difference between the actual voltage of the physical interface end of the satellite core control end and the standard operating voltage of the physical interface end of the satellite core control end is less than a second preset voltage threshold, it is determined that the physical interface end of the satellite core control end has the power supply safety hazard, wherein the first preset voltage threshold is greater than 0, and the second preset voltage threshold is less than 0;

[0067] The standard operating voltage of the physical interface terminal of the satellite core control terminal is generally 30V, so the first preset voltage threshold may be 0.2V, and the second preset voltage threshold may be -0.2V.

[0068] If the voltage difference between the actual voltage of the physical interface end of the satellite core control end and the standard operating voltage of the physical interface end of the satellite core control end is between the first preset voltage threshold and the second preset voltage threshold, it is determined that the physical interface end of the satellite core control end does not have the power supply safety hazard.

[0069] In a possible implementation manner, issuing a first alarm on the ground test computer terminal includes:

[0070] According to the voltage difference between the actual voltage of the physical interface end of the satellite core control end and the standard operating voltage of the physical interface end of the satellite core control end, a first alarm is issued on the ground test computer end.

[0071] In a possible implementation manner, according to the voltage difference between the actual voltage of the physical interface terminal of the satellite core control terminal and the standard operating voltage of the physical interface terminal of the satellite core control terminal, a first alarm is issued on the ground test computer terminal, including:

[0072] If the voltage difference between the actual voltage of the physical interface terminal of the satellite core control terminal and the standard operating voltage of the physical interface terminal of the satellite core control terminal is less than the second preset voltage threshold, a yellow alarm mark is generated on the ground test computer terminal;

[0073] Exemplarily, a prompt message indicating that the voltage difference is lower than the standard operating voltage may also be generated on the ground test computer.

[0074] Furthermore, the power supply safety hazard level can be determined based on the degree to which the voltage difference is less than the second preset voltage threshold (the more it is less than, the higher the hazard level), and the power supply safety hazard level can be displayed on the ground test computer.

[0075] For example, when a data transmission security risk occurs at a physical interface of a satellite core control terminal, a yellow warning sign may also be generated on a ground test computer terminal.

[0076] If the voltage difference between the actual voltage of the physical interface end of the satellite core control end and the standard operating voltage of the physical interface end of the satellite core control end is greater than the first preset voltage threshold, a red alarm mark is generated on the ground test computer end.

[0077] Exemplarily, a prompt message indicating that the voltage difference is higher than the standard operating voltage may also be generated on the ground test computer.

[0078] Furthermore, the power supply safety hazard level can be determined based on the degree to which the voltage difference is greater than the first preset voltage threshold (the greater the difference, the higher the hazard level), and the power supply safety hazard level can be displayed on the ground test computer.

[0079] Reference Figure 3 As shown, it is a flow chart of another alarm method for satellite testing provided by an embodiment of the present application. In a possible implementation manner, the method further includes:

[0080] S301, drawing an actual voltage curve graph according to the actual voltage of the physical interface terminal of the satellite core control terminal at a plurality of consecutive moments;

[0081] S302: Displaying the actual voltage curve graph on the ground test computer.

[0082] Combined with step S301 to step S302, the actual voltage situation within a continuous period of time is intuitively displayed to the user.

[0083] An alarm method for satellite testing provided in an embodiment of the present application can prevent engineers from further using a satellite test terminal to test the satellite when an error occurs in the satellite.

[0084] Reference Figure 4 FIG. 1 is a schematic diagram of a structure of an alarm method device for satellite testing provided by an embodiment of the present application, wherein the device comprises:

[0085] The acquisition module 401 is used to acquire the actual voltage of the physical interface end of the satellite core control end in real time, and to acquire the transmission efficiency of the test data between the satellite core control end and the ground test computer end, wherein the physical interface end of the satellite core control end is electrically connected to the physical interface end of the ground test computer end through a transmission cable, and the test data is transmitted through the transmission cable;

[0086] A potential safety hazard determination module 402 is used to determine whether there is a potential safety hazard in power supply at the physical interface of the satellite core control end according to a voltage difference between an actual voltage at the physical interface of the satellite core control end and a standard operating voltage at the physical interface of the satellite core control end, and to determine whether there is a potential safety hazard in data transmission at the physical interface of the satellite core control end according to the transmission efficiency;

[0087] The alarm module 403 is used to issue a first alarm on the ground test computer end if the power supply safety hazard exists, and to issue a second alarm on the ground test computer end if the data transmission safety hazard exists, wherein when the first alarm and / or the second alarm is issued on the ground test computer end, the ground test computer end does not respond to any operation instructions directed to the satellite core control end.

[0088] In a possible implementation manner, when acquiring the transmission efficiency of the test data between the satellite core control terminal and the ground test computer terminal, the acquisition module 401 is specifically used to:

[0089] Using the ground test computer to send the test data to the satellite core control terminal, wherein the test data includes a preset number of test instructions;

[0090] Using the satellite core control terminal to return the test instruction received by the satellite core control terminal to the ground test computer terminal;

[0091] The ratio of the number of target test instructions to the preset number is calculated, and the ratio is used as the transmission efficiency, wherein the target test instructions are test instructions received by the ground test computer and returned by the satellite core control terminal.

[0092] In a possible implementation manner, the potential safety hazard determination module 402, when determining whether there is a potential power supply safety hazard at the physical interface end of the satellite core control end according to the voltage difference between the actual voltage of the physical interface end of the satellite core control end and the standard operating voltage of the physical interface end of the satellite core control end, is specifically used to:

[0093] If the voltage difference between the actual voltage of the physical interface end of the satellite core control end and the standard operating voltage of the physical interface end of the satellite core control end is greater than a first preset voltage threshold, or the voltage difference between the actual voltage of the physical interface end of the satellite core control end and the standard operating voltage of the physical interface end of the satellite core control end is less than a second preset voltage threshold, it is determined that the physical interface end of the satellite core control end has the power supply safety hazard, wherein the first preset voltage threshold is greater than 0, and the second preset voltage threshold is less than 0;

[0094] If the voltage difference between the actual voltage of the physical interface end of the satellite core control end and the standard operating voltage of the physical interface end of the satellite core control end is between the first preset voltage threshold and the second preset voltage threshold, it is determined that the physical interface end of the satellite core control end does not have the power supply safety hazard.

[0095] When the alarm module 403 issues the first alarm on the ground test computer, it is specifically used to:

[0096] According to the voltage difference between the actual voltage of the physical interface end of the satellite core control end and the standard operating voltage of the physical interface end of the satellite core control end, a first alarm is issued on the ground test computer end.

[0097] The alarm module 403 is specifically used to: when the first alarm is issued on the ground test computer end according to the voltage difference between the actual voltage of the physical interface end of the satellite core control end and the standard working voltage of the physical interface end of the satellite core control end;

[0098] If the voltage difference between the actual voltage of the physical interface terminal of the satellite core control terminal and the standard operating voltage of the physical interface terminal of the satellite core control terminal is less than the second preset voltage threshold, a yellow alarm mark is generated on the ground test computer terminal;

[0099] If the voltage difference between the actual voltage of the physical interface end of the satellite core control end and the standard operating voltage of the physical interface end of the satellite core control end is greater than the first preset voltage threshold, a red alarm mark is generated on the ground test computer end.

[0100] In a possible implementation, the device further includes:

[0101] A drawing module, used for drawing an actual voltage curve graph according to the actual voltage of the physical interface terminal of the satellite core control terminal at a plurality of consecutive moments;

[0102] A display module is used to display the actual voltage curve graph on the ground test computer terminal.

[0103] An alarm method and device for satellite testing provided in an embodiment of the present application can prevent engineers from further using a satellite test terminal to test a satellite when an error occurs in the satellite.

[0104] Reference Figure 5 As shown, an electronic device 500 provided in an embodiment of the present application includes: a processor 501, a memory 502 and a bus, wherein the memory 502 stores machine-readable instructions executable by the processor 501. When the electronic device is running, the processor 501 communicates with the memory 502 through the bus, and the processor 501 executes the machine-readable instructions to perform the steps of the method of the above-mentioned alarm method for satellite testing.

[0105] Specifically, the above-mentioned memory 502 and processor 501 can be general-purpose memories and processors, which are not specifically limited here. When the processor 501 runs the computer program stored in the memory 502, the above-mentioned alarm method for satellite testing can be executed.

[0106] Corresponding to the above-mentioned alarm method for satellite testing, an embodiment of the present application also provides a computer-readable storage medium, on which a computer program is stored. When the computer program is executed by a processor, the steps of the above-mentioned alarm method for satellite testing are executed.

[0107] Those skilled in the art can clearly understand that, for the convenience and simplicity of description, the specific working process of the system and device described above can refer to the corresponding process in the method embodiment, and will not be repeated in this application. In the several embodiments provided in this application, it should be understood that the disclosed system, system and method can be implemented in other ways. The device embodiments described above are merely schematic. For example, the division of the modules is only a logical function division. There may be other division methods in actual implementation. For example, multiple modules or components can be combined or integrated into another system, or some features can be ignored or not executed. Another point is that the mutual coupling or direct coupling or communication connection shown or discussed can be through some communication interfaces, indirect coupling or communication connection of devices or modules, which can be electrical, mechanical or other forms.

[0108] The modules described as separate components may or may not be physically separated, and the components shown as modules may or may not be physical units, that is, they may be located in one place or distributed on multiple network units. Some or all of the units may be selected according to actual needs to achieve the purpose of the solution of this embodiment.

[0109] In addition, each functional unit in each embodiment of the present application may be integrated into one processing unit, or each unit may exist physically separately, or two or more units may be integrated into one unit.

[0110] If the functions are implemented in the form of software functional units and sold or used as independent products, they can be stored in a non-volatile computer-readable storage medium that is executable by a processor. Based on this understanding, the technical solution of the present application, or the part that contributes to the prior art or the part of the technical solution, can be embodied in the form of a software product, which is stored in a storage medium and includes several instructions for a computer device (which can be a personal computer, server, or network device, etc.) to perform all or part of the steps of the method described in each embodiment of the present application. The aforementioned storage medium includes: various media that can store program codes, such as USB flash drives, mobile hard drives, ROM, RAM, magnetic disks, or optical disks.

[0111] The above are only specific implementations of the present application, but the protection scope of the present application is not limited thereto. Any technician familiar with the technical field can easily think of changes or substitutions within the technical scope disclosed in the present application, which should be included in the protection scope of the present application. Therefore, the protection scope of the present application should be based on the protection scope of the claims.

Claims

1. An alarm method for satellite testing, characterized in that: The method comprises: Acquire the actual voltage of the physical interface end of the satellite core control end in real time, and acquire the transmission efficiency of the test data between the satellite core control end and the ground test computer end, wherein the physical interface end of the satellite core control end is electrically connected to the physical interface end of the ground test computer end through a transmission cable, and the test data is transmitted through the transmission cable; Determine whether there is a power supply safety hazard at the physical interface of the satellite core control end according to a voltage difference between an actual voltage at the physical interface of the satellite core control end and a standard operating voltage at the physical interface of the satellite core control end, and determine whether there is a data transmission safety hazard at the physical interface of the satellite core control end according to the transmission efficiency; If the power supply safety hazard exists, a first alarm is issued on the ground test computer end, and if the data transmission safety hazard exists, a second alarm is issued on the ground test computer end, wherein when the first alarm and / or the second alarm is issued on the ground test computer end, the ground test computer end does not respond to any operation instruction directed to the satellite core control end; Determining whether there is a power supply safety hazard at the physical interface of the satellite core control end according to a voltage difference between an actual voltage at the physical interface of the satellite core control end and a standard operating voltage at the physical interface of the satellite core control end includes: If the voltage difference between the actual voltage of the physical interface end of the satellite core control end and the standard operating voltage of the physical interface end of the satellite core control end is greater than a first preset voltage threshold, or the voltage difference between the actual voltage of the physical interface end of the satellite core control end and the standard operating voltage of the physical interface end of the satellite core control end is less than a second preset voltage threshold, it is determined that the physical interface end of the satellite core control end has the power supply safety hazard, wherein the first preset voltage threshold is greater than 0, and the second preset voltage threshold is less than 0; If the voltage difference between the actual voltage of the physical interface end of the satellite core control end and the standard operating voltage of the physical interface end of the satellite core control end is between the first preset voltage threshold and the second preset voltage threshold, it is determined that the physical interface end of the satellite core control end does not have the power supply safety hazard.

2. The alarm method for satellite testing according to claim 1, characterized in that: Obtaining the transmission efficiency of the test data between the satellite core control terminal and the ground test computer terminal, including: Using the ground test computer to send the test data to the satellite core control terminal, wherein the test data includes a preset number of test instructions; Using the satellite core control terminal to return the test instruction received by the satellite core control terminal to the ground test computer terminal; The ratio of the number of target test instructions to the preset number is calculated, and the ratio is used as the transmission efficiency, wherein the target test instructions are test instructions received by the ground test computer and returned by the satellite core control terminal.

3. The alarm method for satellite testing according to claim 1, characterized in that: The first alarm is issued on the ground test computer, including: According to the voltage difference between the actual voltage of the physical interface end of the satellite core control end and the standard operating voltage of the physical interface end of the satellite core control end, a first alarm is issued on the ground test computer end.

4. The alarm method for satellite testing according to claim 3, characterized in that: According to the voltage difference between the actual voltage of the physical interface end of the satellite core control end and the standard working voltage of the physical interface end of the satellite core control end, a first alarm is issued on the ground test computer end, including: If the voltage difference between the actual voltage of the physical interface terminal of the satellite core control terminal and the standard operating voltage of the physical interface terminal of the satellite core control terminal is less than the second preset voltage threshold, a yellow alarm mark is generated on the ground test computer terminal; If the voltage difference between the actual voltage of the physical interface end of the satellite core control end and the standard operating voltage of the physical interface end of the satellite core control end is greater than the first preset voltage threshold, a red alarm mark is generated on the ground test computer end.

5. The alarm method for satellite testing according to claim 1, characterized in that: The method further comprises: Draw an actual voltage curve graph according to the actual voltage of the physical interface terminal of the satellite core control terminal at a plurality of consecutive moments; The actual voltage curve graph is displayed on the ground test computer terminal.

6. An alarm device for satellite testing, characterized in that: The device comprises: An acquisition module is used to acquire in real time the actual voltage of the physical interface end of the satellite core control end, and to acquire the transmission efficiency of the test data between the satellite core control end and the ground test computer end, wherein the physical interface end of the satellite core control end is electrically connected to the physical interface end of the ground test computer end through a transmission cable, and the test data is transmitted through the transmission cable; A potential safety hazard determination module is used to determine whether there is a potential safety hazard in power supply at the physical interface of the satellite core control end according to a voltage difference between an actual voltage at the physical interface of the satellite core control end and a standard operating voltage at the physical interface of the satellite core control end, and to determine whether there is a potential safety hazard in data transmission at the physical interface of the satellite core control end according to the transmission efficiency; an alarm module, configured to issue a first alarm on the ground test computer end if the power supply safety hazard exists, and to issue a second alarm on the ground test computer end if the data transmission safety hazard exists, wherein when the first alarm and / or the second alarm is issued on the ground test computer end, the ground test computer end does not respond to any operation instruction directed to the satellite core control end; The potential safety hazard determination module is specifically used to determine whether there is a potential power supply safety hazard at the physical interface of the satellite core control end according to the voltage difference between the actual voltage of the physical interface of the satellite core control end and the standard operating voltage of the physical interface of the satellite core control end: If the voltage difference between the actual voltage of the physical interface end of the satellite core control end and the standard operating voltage of the physical interface end of the satellite core control end is greater than a first preset voltage threshold, or the voltage difference between the actual voltage of the physical interface end of the satellite core control end and the standard operating voltage of the physical interface end of the satellite core control end is less than a second preset voltage threshold, it is determined that the physical interface end of the satellite core control end has the power supply safety hazard, wherein the first preset voltage threshold is greater than 0, and the second preset voltage threshold is less than 0; If the voltage difference between the actual voltage of the physical interface end of the satellite core control end and the standard operating voltage of the physical interface end of the satellite core control end is between the first preset voltage threshold and the second preset voltage threshold, it is determined that the physical interface end of the satellite core control end does not have the power supply safety hazard.

7. The warning device for satellite testing according to claim 6, characterized in that: When acquiring the transmission efficiency of the test data between the satellite core control terminal and the ground test computer terminal, the acquisition module is specifically used to: Using the ground test computer to send the test data to the satellite core control terminal, wherein the test data includes a preset number of test instructions; Using the satellite core control terminal to return the test instruction received by the satellite core control terminal to the ground test computer terminal; The ratio of the number of target test instructions to the preset number is calculated, and the ratio is used as the transmission efficiency, wherein the target test instructions are test instructions received by the ground test computer and returned by the satellite core control terminal.

8. An electronic device, characterized in that: include: A processor, a storage medium and a bus, wherein the storage medium stores machine-readable instructions executable by the processor, and when the electronic device is running, the processor communicates with the storage medium via the bus, and the processor executes the machine-readable instructions to perform the steps of the alarm method for satellite testing as described in any one of claims 1 to 5.

9. A computer-readable storage medium, characterized in that: The computer-readable storage medium stores a computer program, and when the computer program is executed by a processor, the steps of the alarm method for satellite testing as described in any one of claims 1 to 5 are executed.

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