Satellite control system, method, electronic device and storage medium

Abstract

The application provides a satellite control system, method, electronic equipment and storage medium. The system comprises: a ground radar detection station, a control adjustment system and an excitation emission source. The ground radar detection station is used for detecting position data and attitude data of a satellite relative to the ground in real time, and transmitting the position data and the attitude data to the control adjustment system through a first signal transmission network between the ground radar detection station and the control adjustment system. The control adjustment system is used for determining an excitation signal required by the excitation emission source to emit to the satellite according to the position data and the attitude data. The excitation emission source is used for emitting the excitation signal to the satellite through a second signal transmission network between the excitation emission source and the satellite, so as to control the operation of the satellite and enable the satellite to run on a preset operation orbit where the satellite is currently located. The application can automatically control the operation of the satellite, so as to reduce the operation burden of a satellite tester.

Description

TECHNICAL FIELD

[0001] The present application relates to the technical field of satellite testing, in particular to a satellite control system and method, an electronic device and a storage medium. BACKGROUND

[0002] Satellite testing is a necessary content before a satellite is put into the market, and the testing includes testing during ground installation, testing after a short time of flying into space and working, and testing after a long time of flying into space and working. The testing work of the satellite is throughout the whole process after the development and generation of the satellite and the flying into space.

[0003] In the prior art, the testing work of the satellite after flying into space is almost completed by manual operation, and the testing time is relatively long. Long-time satellite testing in space brings a large operation burden to the satellite tester. SUMMARY

[0004] Therefore, the present application aims to provide a satellite control system and method, an electronic device and a storage medium, which can automatically control the operation of the satellite to reduce the operation burden of the satellite tester.

[0005] In a first aspect, the present application provides a satellite control system, which comprises a ground radar detection station, a control adjustment system and an excitation emission source.

[0006] The ground radar detection station is configured to detect position data and attitude data of a satellite relative to the ground in real time, and transmit the position data and the attitude data to the control adjustment system through a first signal transmission network between the ground radar detection station and the control adjustment system.

[0007] The control adjustment system is configured to determine an excitation signal required by the excitation emission source to emit to the satellite according to the position data and the attitude data, wherein the excitation signal is used to control the operation of the satellite, so that the satellite can be kept on a preset operation orbit where the satellite is currently located.

[0008] The excitation emission source is configured to emit the excitation signal to the satellite through a second signal transmission network between the excitation emission source and the satellite, so as to control the operation of the satellite, and keep the satellite on the preset operation orbit where the satellite is currently located.

[0009] In a possible implementation, the satellite control system further comprises a data detection sensor, and the data detection sensor is arranged on the satellite.

[0010] The data detection sensor is configured to detect target data of the satellite in real time, and transmit the target data of the satellite to the control adjustment system through a third signal transmission network between the data detection sensor and the control adjustment system, wherein the target data of the satellite includes at least one of voltage data of the satellite, current data of the satellite, and telemetry data of the satellite.

[0011] The control adjustment system is configured to determine the excitation signal required by the excitation emission source to emit to the satellite according to the position data and the attitude data, and specifically configured to:

[0012] The control adjustment system is configured to determine the excitation signal required by the excitation emission source to emit to the satellite according to the position data, the attitude data, and the target data of the satellite.

[0013] In a possible implementation, the data detection sensor is further configured to determine whether the data detection sensor fails before detecting the target data of the satellite in real time.

[0014] The data detection sensor is configured to detect the target data of the satellite in real time, and specifically configured to:

[0015] If the data detection sensor does not fail, the data detection sensor is configured to detect the target data of the satellite in real time.

[0016] In a possible implementation, the satellite control system further includes a compensation system.

[0017] The compensation system is configured to enable a satellite tester to manually control the operation of the satellite.

[0018] The compensation system is configured to shut down the control adjustment system when the data detection sensor fails.

[0019] In a possible implementation, the satellite control system further includes a data recording system.

[0020] In a second aspect, the embodiments of the present application further provide a satellite control method, applied to a satellite control system, the satellite control system including a ground radar detection station, a control adjustment system, and an excitation emission source, and the method including:

[0021] The ground radar detection station is configured to detect position data and attitude data of a satellite relative to the ground in real time, and transmit the position data and the attitude data to the control adjustment system through a first signal transmission network between the ground radar detection station and the control adjustment system.

[0022] The control adjustment system determines the excitation signal required to be transmitted by the excitation transmitter to the satellite according to the position data and the attitude data, wherein the excitation signal is used to control the operation of the satellite so that the satellite can keep operating on the preset operation orbit where it is currently located.

[0023] The excitation transmitter transmits the excitation signal to the satellite through a second signal transmission network between the excitation transmitter and the satellite to control the operation of the satellite so that the satellite can keep operating on the preset operation orbit where it is currently located.

[0024] In a possible implementation, the satellite control system further comprises a data detection sensor, wherein the data detection sensor is arranged on the satellite, and the method further comprises:

[0025] The data detection sensor detects target data of the satellite in real time and sends the target data of the satellite to the control adjustment system through a third signal transmission network between the data detection sensor and the control adjustment system, wherein the target data of the satellite comprises at least one of the following: voltage data of the satellite, current data of the satellite, and telemetry data of the satellite.

[0026] The control adjustment system determines the excitation signal required to be transmitted by the excitation transmitter to the satellite according to the position data and the attitude data, comprising:

[0027] The control adjustment system determines the excitation signal required to be transmitted by the excitation transmitter to the satellite according to the position data, the attitude data, and the target data of the satellite.

[0028] In a possible implementation, before the data detection sensor detects the target data of the satellite in real time, the method further comprises:

[0029] The data detection sensor determines whether the data detection sensor itself is faulty:

[0030] The data detection sensor detects the target data of the satellite in real time, comprising:

[0031] If the sensor itself is not faulty, the sensor detects the target data of the satellite in real time.

[0032] In a possible implementation, the satellite control system further comprises a compensation system.

[0033] The compensation system enables a satellite tester to manually control the operation of the satellite.

[0034] The compensation system turns off the control adjustment system when the data detection sensor is faulty.

[0035] In a possible implementation, the satellite control system further comprises a data recording system; and the method further comprises:

[0036] The data recording system records the position data, the attitude data and target data of the satellite.

[0037] In a third aspect, an electronic device is provided, which comprises a processor, a storage medium and a bus. The storage medium stores machine readable instructions executable by the processor. When the electronic device is running, the processor communicates with the storage medium through the bus. The processor executes the machine readable instructions to perform the steps of the satellite control method according to any one of the second aspect.

[0038] In a fourth aspect, a computer readable storage medium is provided, which stores a computer program. When the computer program is run by a processor, the steps of the satellite control method according to any one of the second aspect are performed.

[0039] The satellite control system, method, electronic device and storage medium provided by the embodiments of the present application can automatically control the operation of the satellite, thereby reducing the operation burden of the satellite test personnel. BRIEF DESCRIPTION OF DRAWINGS

[0040] In order to more clearly illustrate the technical solutions of the embodiments of the present application, the following will briefly introduce the drawings needed in the embodiments. It should be understood that the following drawings only show some of the embodiments of the present application, and therefore should not be considered as limiting the scope. For those skilled in the art, other related drawings can also be obtained without creative labor.

[0041] Figure 1 Fig. 1 shows a structural schematic diagram of a satellite control system provided by an embodiment of the present application;

[0042] Figure 2 Fig. 2 shows a flowchart of a satellite control method provided by an embodiment of the present application;

[0043] Figure 3 Fig. 3 shows a structural schematic diagram of an electronic device provided by an embodiment of the present application. DETAILED DESCRIPTION

[0044] To make the purposes, technical solutions, and advantages of the embodiments of the present application clearer, the technical solutions in the embodiments of the present application will be described clearly and completely below with reference to the drawings in the embodiments of the present application. It should be understood that the drawings in the present application serve only the purpose of description and illustration, and do not serve to limit the scope of protection of the present application. In addition, it should be understood that the schematic drawings are not drawn according to the actual proportions. The flowcharts used in the present application show the operations implemented according to some embodiments of the present application. It should be understood that the operations of the flowcharts can not be implemented in sequence, and the steps without logical context relationship can be reversed in sequence or implemented simultaneously. In addition, one or more other operations can be added to the flowcharts or one or more operations can be removed from the flowcharts under the guidance of the content of the present application.

[0045] In addition, the described embodiments are only some 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 herein can be arranged and designed in various different 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 claimed present application, but only represents 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 creative labor fall within the scope of protection of the present application.

[0046] It should be noted that the term "comprise" will be used in the embodiments of the present application to indicate the presence of the features declared thereafter, but does not exclude the addition of other features.

[0047] To facilitate the understanding of the present embodiments, a satellite control system, method, electronic device, and storage medium provided by the embodiments of the present application are described in detail.

[0048] Referring to Figure 1 FIG. 1 shows a structure schematic diagram of a satellite control system provided by the embodiments of the present application. The satellite control system comprises a ground radar detection station 101, a control adjustment system 102, and an excitation emission source 103.

[0049] The ground radar detection station 101 is configured to detect position data and attitude data of a satellite relative to the ground in real time, and transmit the position data and the attitude data to the control adjustment system 102 through a first signal transmission network between the ground radar detection station 101 and the control adjustment system 102.

[0050] The control adjustment system 102 is configured to determine an excitation signal required by the excitation emission source 103 to emit to the satellite according to the position data and the attitude data, wherein the excitation signal is used to control the operation of the satellite, so that the satellite can be kept on a preset operation orbit where the satellite is currently located.

[0051] The position data can include altitude data of the satellite relative to the ground, and / or precision data of the satellite, and / or latitude data of the satellite.

[0052] The excitation emission source 103 is configured to emit the excitation signal to the satellite through a second signal transmission network between the excitation emission source 103 and the satellite, so as to control the operation of the satellite, and enable the satellite to operate on a preset operation orbit where the satellite is currently located.

[0053] In a possible implementation, the satellite control system further includes a data detection sensor, and the data detection sensor is arranged on the satellite.

[0054] The data detection sensor can be multiple and distributed on different positions of the satellite.

[0055] The data detection sensor is configured to detect target data of the satellite in real time, and send the target data of the satellite to the control adjustment system 102 through a third signal transmission network between the data detection sensor and the control adjustment system 102, wherein the target data of the satellite includes at least one of voltage data of the satellite, current data of the satellite, and telemetry data of the satellite.

[0056] The control adjustment system 102 is specifically configured to:

[0057] determine the excitation signal that the excitation emission source needs to emit to the satellite according to the position data, the attitude data, and the target data of the satellite.

[0058] In a possible implementation, the data detection sensor is further configured to determine whether the data detection sensor is faulty before detecting the target data of the satellite in real time.

[0059] The data detection sensor is specifically configured to:

[0060] If the data detection sensor is not faulty, the data detection sensor detects the target data of the satellite in real time.

[0061] In a possible implementation, the satellite control system further includes a compensation system.

[0062] The compensation system enables a satellite tester to manually control the operation of the satellite.

[0063] The compensation system is configured to shut down the control adjustment system 102 when the data detection sensor is faulty.

[0064] The compensating system is provided with a satellite manual control function, so that the tester can manually intervene in the operation of the satellite through the compensating system, that is, the operation of the satellite can be manually controlled when the automatic adjustment fails.

[0065] In a possible implementation, the satellite control system further comprises a data recording system.

[0066] The data recording system is configured to record the position data, the attitude data and target data of the satellite.

[0067] The position data, the attitude data and the target data of the satellite are recorded, so that the satellite tester can analyze and review the three data.

[0068] The satellite control system provided by the embodiment can automatically control the operation of the satellite, thereby reducing the operation burden of the satellite tester.

[0069] Reference Figure 2 FIG. 1 shows a flowchart of a satellite control method provided by an embodiment of the present application, which is applied to a satellite control system, and the satellite control system comprises a ground radar detection station, a control adjustment system and an excitation emission source.

[0070] S201, the ground radar detection station detects position data and attitude data of a satellite relative to the ground in real time, and transmits the position data and the attitude data to the control adjustment system through a first signal transmission network between the ground radar detection station and the control adjustment system.

[0071] S202, the control adjustment system determines an excitation signal required by the excitation emission source to emit to the satellite according to the position data and the attitude data, and the excitation signal is used to control the operation of the satellite, so that the satellite can keep operating on a preset operation orbit where the satellite is currently located.

[0072] S203, the excitation emission source emits the excitation signal to the satellite through a second signal transmission network between the excitation emission source and the satellite, so as to control the operation of the satellite, and the satellite can keep operating on the preset operation orbit where the satellite is currently located.

[0073] In a possible implementation, the satellite control system further comprises a data detection sensor, and the data detection sensor is arranged on the satellite, and the method further comprises:

[0074] The data detection sensor detects target data of the satellite in real time, and sends the target data of the satellite to the control adjustment system through a third signal transmission network between the data detection sensor and the control adjustment system, wherein the target data of the satellite includes at least one of voltage data of the satellite, current data of the satellite, and telemetry data of the satellite.

[0075] The control adjustment system determines, according to the position data and the attitude data, an excitation signal that needs to be emitted by the excitation emission source to the satellite, and the excitation signal includes:

[0076] The control adjustment system determines, according to the position data, the attitude data, and the target data of the satellite, the excitation signal that needs to be emitted by the excitation emission source to the satellite.

[0077] In a possible implementation, before the data detection sensor detects the target data of the satellite in real time, the method further includes:

[0078] The data detection sensor determines whether the data detection sensor itself is faulty:

[0079] The data detection sensor detects the target data of the satellite in real time, and the detecting includes:

[0080] If the sensor itself is not faulty, the sensor detects the target data of the satellite in real time.

[0081] In a possible implementation, the satellite control system further includes a compensation system.

[0082] The compensation system enables a satellite tester to manually control operation of the satellite.

[0083] The compensation system turns off the control adjustment system when the data detection sensor is faulty.

[0084] In a possible implementation, the satellite control system further includes a data recording system, and the method further includes:

[0085] The data recording system records the position data, the attitude data, and the target data of the satellite.

[0086] The satellite control method provided by the embodiments of the present application can automatically control operation of a satellite, thereby reducing an operation burden of a satellite tester.

[0087] Reference Figure 3As shown, the electronic device 300 provided by the embodiment of the present application comprises a processor 301, a memory 302 and a bus, the memory 302 stores machine readable instructions executable by the processor 301, when the electronic device is running, the processor 301 and the memory 302 communicate through the bus, and the processor 301 executes the machine readable instructions to perform the steps of the method for satellite control as described above.

[0088] Specifically, the memory 302 and the processor 301 can be general memory and processor, which are not specifically limited here, and when the processor 301 runs the computer program stored in the memory 302, the method for satellite control as described above can be executed.

[0089] Corresponding to the method for satellite control as described above, the embodiment of the present application further provides a computer readable storage medium, the computer readable storage medium stores a computer program, and the computer program is executed by the processor to perform the steps of the method for satellite control as described above.

[0090] Those skilled in the art can clearly understand that, for the convenience and brevity of description, the specific working process of the system and device described above can refer to the corresponding process in the method embodiment, which will not be described in detail in the present application. In the several embodiments provided by the present application, it should be understood that the disclosed system, system and method can be implemented by other ways. The device embodiments described above are only schematic, for example, the division of the modules is only a logical function division, and the actual implementation can be another division manner, for example, a plurality of modules or components can be combined or integrated into another system, or some features can be ignored or not executed. In addition, the coupling or direct coupling or communication connection between the shown or discussed modules can be indirect coupling or communication connection through some communication interfaces, devices or modules, which can be electrical, mechanical or other forms.

[0091] The modules described as separate components can or can not be physically separated, and the components shown as modules can or can not be physical units, that is, they can be located in one place, or they can be distributed on a plurality of network units. According to actual needs, part or all of the units can be selected to achieve the purpose of the embodiment of the present application.

[0092] In addition, each functional unit in each embodiment of the present application can be integrated in one processing unit, or each unit can exist physically, or two or more units can be integrated in one unit.

[0093] If the functions are implemented in the form of software function units and sold or used as independent products, they can be stored in a nonvolatile computer readable storage medium executable by a processor. Based on this understanding, the technical solutions of the present application essentially or the parts that contribute to the prior art or parts of the technical solutions can be embodied in the form of a software product. The computer software product is stored in a storage medium and includes a plurality of instructions for causing a computer device (which can be a personal computer, a server, or a network device, etc.) to execute all or part of the steps of the methods described in the various embodiments of the present application. The aforementioned storage medium includes: a U disk, a mobile hard disk, a ROM, a RAM, a magnetic disk or an optical disk, and various media that can store program codes.

[0094] The above is merely a specific implementation of the present application, but the protection scope of the present application is not limited thereto. Any person skilled in the art can easily think of changes or replacements within the technical scope disclosed in the present application, which should be covered within the protection scope of the present application. Therefore, the protection scope of the present application should be subject to the protection scope of the claims.

Claims

1. A satellite control system, characterized by, The satellite control system comprises a ground radar detection station, a control adjustment system and an excitation emission source. The ground radar detection station is configured to detect position data and attitude data of the satellite relative to the ground in real time, and transmit the position data and the attitude data to the control adjustment system through a first signal transmission network between the ground radar detection station and the control adjustment system. The control adjustment system is configured to determine an excitation signal required by the excitation emission source to emit to the satellite according to the position data and the attitude data, wherein the excitation signal is used to control operation of the satellite, so that the satellite can be kept on a preset operation orbit where the satellite is currently located. The excitation emission source is configured to emit the excitation signal to the satellite through a second signal transmission network between the excitation emission source and the satellite, so as to control operation of the satellite, so that the satellite can be kept on a preset operation orbit where the satellite is currently located. The satellite control system further comprises a data detection sensor, and the data detection sensor is arranged on the satellite. The data detection sensor is configured to detect target data of the satellite in real time, and transmit the target data of the satellite to the control adjustment system through a third signal transmission network between the data detection sensor and the control adjustment system, wherein the target data of the satellite comprises at least one of voltage data of the satellite, current data of the satellite and telemetry data of the satellite. The control adjustment system is specifically configured to determine the excitation signal required by the excitation emission source to emit to the satellite according to the position data, the attitude data and the target data of the satellite. The data detection sensor is further configured to determine whether the data detection sensor is faulty before detecting the target data of the satellite in real time.

2. The satellite control system of claim 1, wherein, The data detection sensor is specifically configured to detect the target data of the satellite in real time if the data detection sensor is not faulty. The satellite control system further comprises a compensation system. The compensation system enables a satellite tester to manually control operation of the satellite.

3. The satellite control system of claim 2, wherein, The compensation system is configured to shut down the control adjustment system when the data detection sensor is faulty. The satellite control system further comprises a data recording system. The data recording system is configured to record the position data, the attitude data and the target data of the satellite.

4. The satellite control system of claim 1, wherein, The method is applied to a satellite control system, and the satellite control system comprises a ground radar detection station, a control adjustment system and an excitation emission source. The ground radar detection station is configured to detect position data and attitude data of the satellite relative to the ground in real time, and transmit the position data and the attitude data to the control adjustment system through a first signal transmission network between the ground radar detection station and the control adjustment system.

5. A satellite control method characterized by, The ground radar detection station is configured to detect position data and attitude data of the satellite relative to the ground in real time, and transmit the position data and the attitude data to the control adjustment system through a first signal transmission network between the ground radar detection station and the control adjustment system. ​ The control adjustment system determines, according to the position data and the attitude data, an excitation signal required to be transmitted by the excitation transmitter to the satellite, wherein the excitation signal is used to control the operation of the satellite, so that the satellite can keep operating on the preset operation orbit where the satellite is currently located. The excitation transmitter transmits the excitation signal to the satellite through a second signal transmission network between the excitation transmitter and the satellite, so as to control the operation of the satellite, so that the satellite can keep operating on the preset operation orbit where the satellite is currently located. The satellite control system further comprises a data detection sensor, wherein the data detection sensor is arranged on the satellite, and the method further comprises: The data detection sensor detects target data of the satellite in real time, and sends the target data of the satellite to the control adjustment system through a third signal transmission network between the data detection sensor and the control adjustment system, wherein the target data of the satellite comprises at least one of voltage data of the satellite, current data of the satellite, and telemetry data of the satellite. The control adjustment system determines, according to the position data and the attitude data, the excitation signal required to be transmitted by the excitation transmitter to the satellite, comprising: The control adjustment system determines, according to the position data, the attitude data and the target data of the satellite, the excitation signal required to be transmitted by the excitation transmitter to the satellite.

6. The satellite control method according to claim 5, characterized by, Before the data detection sensor detects the target data of the satellite in real time, the method further comprises: The data detection sensor judges whether the data detection sensor itself is faulty or not. The data detection sensor detects the target data of the satellite in real time, comprising: If the sensor itself is not faulty, the sensor detects the target data of the satellite in real time.

7. An electronic device, comprising: Comprising: A processor, a storage medium and a bus, the storage medium stores machine readable instructions executable by the processor, when the electronic device is running, the processor and the storage medium communicate through the bus, the processor executes the machine readable instructions to execute the steps of the satellite control method in any one of claims 5 to 6.

8. A computer-readable storage medium, characterized in that, The computer readable storage medium stores a computer program, when the computer program is run by the processor, the steps of the satellite control method in any one of claims 5 to 6 are executed.

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