Space tracking and control station configuration method and device

Abstract

The present invention provides a method and device for configuring an aerospace tracking and control station. The method comprises: obtaining a plurality of tracking and control equipment configuration information, a plurality of satellite tracking configuration information, and tracking and control plan information; based on the tracking and control plan information, determining the target tracking and control equipment configuration information from the plurality of tracking and control equipment configuration information, and determining the target satellite tracking configuration information from the plurality of satellite tracking configuration files; determining the target configuration file based on the target tracking and control equipment configuration information and the target satellite tracking configuration information; and sending the target configuration file to the target tracking and control station. The method and device for configuring an aerospace tracking and control station provided by the present invention prepare a plurality of tracking and control equipment configuration information and a plurality of satellite tracking configuration information in advance, determine the target tracking and control equipment configuration information and the target satellite tracking configuration information in a server according to the tracking and control plan information, and form a target configuration file, which can greatly reduce the workload of development and operation personnel, simplify the configuration process, and improve work efficiency.

Description

Technical Field

[0001] The present invention relates to the field of aerospace engineering technology, and in particular to a method and device for configuring an aerospace measurement and control station. Background Art

[0002] With the development of aerospace technology, humans have launched many satellites into space. During the operation of satellites, satellites need to be monitored by aerospace tracking and control stations. Multiple aerospace tracking and control stations are often deployed on the ground. At the same time, there are many satellites that need to be monitored by aerospace tracking and control stations. The ground-to-space interfaces such as the tracking and control systems, operating frequencies, channel coding, and data frame management of different satellites are constantly changing. Therefore, for each aerospace tracking and control station, when detecting different target satellites, specific and complex configuration operations are required. In addition, there are certain differences in the technical status of multiple tracking and control stations that track the same satellite.

[0003] At present, the configuration method of aerospace tracking and control stations is that before the mission begins, the station operation and maintenance personnel need to write a specific configuration file based on the matching relationship between the specific ground tracking and control station and the specific tracking service satellite object, configure various tracking devices, and control the antenna to point to the satellite when the mission starts, and start tracking and control work. Manually completing the above operations requires high requirements for the operation and management personnel of the tracking and control station, with many manual operations, low reliability, high cost and low efficiency. Summary of the invention

[0004] The present invention provides a method and device for configuring an aerospace tracking and control station, which are used to solve the defects in the prior art that manual configuration is required when detecting each satellite object, the configuration process is complicated, the manpower cost is large, and the work efficiency is low, thereby reducing the workload of development and operation and maintenance personnel, simplifying the configuration process, and improving work efficiency.

[0005] The present invention provides a method for configuring an aerospace tracking and control station, which comprises: acquiring a plurality of tracking and control equipment configuration information, a plurality of satellite tracking configuration information and tracking and control plan information; based on the tracking and control plan information, determining target tracking and control equipment configuration information from the plurality of tracking and control equipment configuration information, and determining target satellite tracking configuration information from the plurality of satellite tracking configuration files; determining a target configuration file based on the target tracking and control equipment configuration information and the target satellite tracking configuration information; and sending the target configuration file to a target tracking and control station.

[0006] According to a method for configuring an aerospace tracking and control station provided by the present invention, determining a target configuration file based on the target tracking and control equipment configuration information and the target satellite tracking configuration information includes: fusing the target tracking and control equipment configuration information with the target satellite tracking configuration information to obtain the target configuration file.

[0007] According to a method for configuring an aerospace measurement and control station provided by the present invention, the target measurement and control equipment configuration information and the target satellite tracking configuration information are merged to obtain the target configuration file, including: replacing the target satellite tracking configuration information with a corresponding position in the target measurement and control equipment configuration information to obtain the target configuration file.

[0008] According to a method for configuring an aerospace tracking and control station provided by the present invention, the target configuration file is determined based on the target tracking and control equipment configuration information and the target satellite tracking configuration information, including: determining the target configuration file based on guidance data, the target tracking and control equipment configuration information and the target satellite tracking configuration information, the guidance data including: at least one of satellite orbital elements, satellite ephemeris data and antenna pointing angle data.

[0009] According to a method for configuring an aerospace tracking and control station provided by the present invention, the tracking and control equipment configuration information includes: at least one of a signal strength parameter, a channel characteristic parameter and an equipment support parameter.

[0010] According to a method for configuring an aerospace tracking and control station provided by the present invention, the satellite tracking configuration information includes at least one of a satellite code, a satellite identifier, satellite channel parameters and configuration, and a template satellite code.

[0011] According to a method for configuring a space tracking and control station provided by the present invention, the tracking and control plan information includes at least one of: a time period for the station to track a satellite, a mapping relationship between space-ground channels, and ground data transmission information.

[0012] The present invention also provides a space measurement and control station configuration device, which includes: an acquisition module, used to acquire multiple measurement and control equipment configuration information, multiple satellite tracking configuration information and measurement and control plan information; a first determination module, used to determine the target measurement and control equipment configuration information from the multiple measurement and control equipment configuration information based on the measurement and control plan information, and to determine the target satellite tracking configuration information from the multiple satellite tracking configuration files; a second determination module, used to determine the target configuration file based on the target measurement and control equipment configuration information and the target satellite tracking configuration information; and a sending module, used to send the target configuration file to the target measurement and control station.

[0013] The present invention also provides an electronic device, comprising a memory, a processor, and a computer program stored in the memory and executable on the processor, wherein the processor implements the steps of any of the above-mentioned methods for configuring a space tracking and control station when executing the computer program.

[0014] The present invention also provides a non-transitory computer-readable storage medium having a computer program stored thereon, and when the computer program is executed by a processor, the steps of any of the above-mentioned methods for configuring aerospace tracking and control stations are implemented.

[0015] The aerospace tracking and control station configuration method and device provided by the present invention respectively prepare the tracking and control equipment configuration information and the satellite tracking configuration information for each tracking and control equipment and satellite in advance, determine the target tracking and control equipment configuration information and the target satellite tracking configuration information in the server according to the tracking and control plan information, and combine the two to form a target configuration file, which can greatly reduce the workload of development and operation and maintenance personnel, simplify the configuration process, and improve work efficiency. BRIEF DESCRIPTION OF THE DRAWINGS

[0016] In order to more clearly illustrate the technical solutions in the present invention or the prior art, the following briefly introduces the drawings required for use in the embodiments or the description of the prior art. Obviously, the drawings described below are some embodiments of the present invention. For ordinary technicians in this field, other drawings can be obtained based on these drawings without paying creative work.

[0017] Figure 1 It is a flow chart of the method for configuring a space tracking and control station provided by the present invention;

[0018] Figure 2 It is a structural schematic diagram of the aerospace tracking and control station configuration device provided by the present invention;

[0019] Figure 3 It is a structural schematic diagram of the electronic device provided by the present invention. DETAILED DESCRIPTION

[0020] In order to make the purpose, technical solution and advantages of the present invention clearer, the technical solution of the present invention will be clearly and completely described below in conjunction with the drawings of the present invention. Obviously, the described embodiments are part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the present invention.

[0021] In the description of this specification, the description with reference to the terms "one embodiment", "some embodiments", "example", "specific example", or "some examples" etc. means that the specific features, structures, materials or characteristics described in conjunction with the embodiment or example are included in at least one embodiment or example of the embodiment of the present invention. In this specification, the schematic representations of the above terms do not necessarily refer to the same embodiment or example. Moreover, the specific features, structures, materials or characteristics described may be combined in any one or more embodiments or examples in a suitable manner. In addition, those skilled in the art may combine and combine the different embodiments or examples described in this specification and the features of the different embodiments or examples, without contradiction.

[0022] Combine the following Figure 1-Figure 3 The aerospace tracking and control station configuration method and device of the present invention are described.

[0023] The space tracking and control network is an important part of the space system engineering. It is mainly composed of the space measurement and control center, operation management center, application system and user management center, as well as globally deployed ground tracking and control stations, ocean measurement ships and relay satellites deployed in space. In a broad sense, relay satellites belong to space-based tracking and control stations. The term "tracking and control stations" is used below to refer to these three types of measurement equipment.

[0024] The mission of the tracking and control station is to directly track, measure, telemeter, remotely control and communicate with the spacecraft. It transmits the received measurement and telemetering information to the space control center, communicates with the spacecraft according to the instructions of the space control center, and cooperates with the control center to complete the control of the spacecraft. The tracking and control station can also independently implement the control of the spacecraft according to the prescribed procedures. The equipment of the tracking and control station includes external measurement system, telemetry system, remote control system, communication system, television system, time unification system, computer system and auxiliary equipment.

[0025] The tracking and control stations generally provide services for multiple satellites at the same time through time division multiplexing. The ground-ground interfaces such as the tracking and control systems, operating frequencies, channel coding and data frame management of different satellites are constantly changing. Therefore, the ground must perform complex state configuration when tracking each satellite. In addition, there are certain differences in the technical status of multiple stations tracking the same satellite.

[0026] In the traditional working mode, a configuration file is created for each ground station and each tracking service satellite object. Before the mission begins, the station operation and maintenance personnel will revise the configuration appropriately, load the configuration file, configure various tracking devices, and when the mission starts, control the antenna to point to the satellite and start tracking and control work.

[0027] like Figure 1As shown, the present invention provides a method for configuring a space tracking and control station. The method can be run in a server. The server can be connected to the tracking and control station for communication. The server can distribute data to the tracking and control station. The method includes: the following steps 110 to 140.

[0028] Among them, step 110, obtains multiple measurement and control equipment configuration information, multiple satellite tracking configuration information and measurement and control plan information.

[0029] It can be understood that the measurement and control equipment configuration information is the configurable parameters and control commands corresponding to the measurement and control equipment on the ground. The measurement and control equipment configuration information can be remotely controlled and configured to ensure the normal operation of the ground and the normal operation of various types of satellite measurement and control.

[0030] It is worth noting that the measurement and control equipment configuration information corresponding to different measurement and control stations is different. Multiple measurement and control stations correspond to multiple measurement and control equipment configuration information, and multiple measurement and control equipment configuration information can form a measurement and control equipment configuration information library.

[0031] The measurement and control equipment configuration information may include all parameters of the measurement and control station, and the measurement and control equipment configuration information may be a file in XML format.

[0032] Satellite tracking configuration information is the physical parameters required for the normal operation of a satellite. Each satellite has specific satellite tracking configuration information. The satellite tracking configuration information corresponding to different satellites is different. Multiple satellites correspond to multiple satellite tracking configuration information. Multiple satellite tracking configuration information can constitute a satellite tracking configuration information library.

[0033] Satellite tracking configuration information can be described in the form of an XML file structure (XSD) file. Each satellite tracking configuration information is an XML file, and the structure of the file needs to meet the constraints of the structure file XSD file.

[0034] The measurement and control plan information is used to present the specific information of this measurement and control mission, that is, which measurement and control station is used to measure and control which satellite. The measurement and control plan information may include at least one of the time period for the station to track the satellite, the mapping relationship between the ground-space channel and the ground data transmission information.

[0035] The measurement and control plan information can be a file in XML format.

[0036] Step 120: Based on the measurement and control plan information, determine the target measurement and control equipment configuration information from the plurality of measurement and control equipment configuration information, and determine the target satellite tracking configuration information from the plurality of satellite tracking configuration files.

[0037] It can be understood that, according to the measurement and control plan information, the target measurement and control station and target satellite corresponding to this measurement and control can be determined, and the target measurement and control station can be matched with the target satellite. Then, the target measurement and control equipment configuration information corresponding to the target measurement and control station can be found from multiple measurement and control equipment configuration information, and the target satellite tracking configuration information corresponding to the target satellite can be found from multiple satellite tracking configuration files.

[0038] Step 130: Determine a target configuration file based on the target measurement and control equipment configuration information and the target satellite tracking configuration information.

[0039] It is understandable that after determining the target measurement and control equipment configuration information and the target satellite tracking configuration information, the target measurement and control equipment configuration information and the target satellite tracking configuration information can be combined to obtain a target configuration file. The target configuration file can be executed by the target measurement and control station.

[0040] It is worth noting that the process of combining the target measurement and control equipment configuration information and the target satellite tracking configuration information can be performed automatically in a computer and can be completed using common fusion and matching algorithms.

[0041] The target configuration file can be a file in XML format.

[0042] Step 140: Send the target configuration file to the target measurement and control station.

[0043] It is understandable that after obtaining the target configuration file, the target configuration file can be sent to the target tracking and control station. In addition to the start and end time of the tracking and control task, the target configuration file also includes task type information, that is, whether to implement remote control, whether to implement external measurement, whether to accept telemetry, and whether to receive data transmission. After receiving the target configuration file, the target tracking and control station can automatically run the target configuration file to perform tracking and control work on the target satellite.

[0044] It should be noted that in the existing working mode, for m tracking stations to track n satellites, m×n sets of configuration files need to be prepared. Due to the different working modes and working parameters of different satellites, the n sets of configuration files of each tracking station are quite different; the working modes and specific parameters of each tracking station are also different, so the m configuration files of each satellite are also different.

[0045] With the rapid development of large-scale constellation systems, dozens of ground stations are required to implement measurement and control of thousands of satellites at the same time. Under the existing technical methods, the workload is huge and the reliability is not high. The main problems are: (i) Difficulty in accessing the network: In the traditional mode, before the satellite is launched into space, it is necessary to conduct a docking test with the ground measurement and control station. For satellites with high safety and reliability requirements, it is even necessary to dock with each batch of ground station equipment generated by each manufacturer, and solidify the docking configuration as the tracking configuration after the satellite enters orbit. (ii) Difficulty in management: After the satellite enters orbit, the technical status of the satellite and the ground measurement and control station may change. At this time, it is necessary to manually modify the configuration files of all measurement and control stations participating in the measurement and control mission of the satellite. Similarly, a change in the status of a satellite requires modification of m measurement and control stations on the ground, and a change in the status of a measurement and control station requires modification of the measurement and control configuration of n satellites. In addition, if the content in the measurement and control plan is different, it is also necessary to adjust the configuration of the measurement and control station and choose whether to load the corresponding link.

[0046] In the traditional mode, operation and management personnel are usually deployed at the measurement and control station to complete the above work manually, which has high requirements for operation and management personnel and requires a lot of manual operations. With the rapid development of the constellation system, the business volume of the above work will increase rapidly and the reliability will also decrease.

[0047] In other words, under the existing working mode, for m tracking stations to track n satellites, m×n sets of configuration files need to be prepared. Due to different satellite working modes and working parameters, the n sets of configuration files for each tracking station are quite different; the working modes and specific parameters of each tracking station are also different, so the m configuration files for each satellite are also different. With the rapid development of large constellation systems, dozens of ground stations are required to implement tracking and control of thousands of satellites at the same time. The main problems of the existing technology are: difficulty in accessing the network. Before the satellite is launched into space, it is necessary to conduct docking tests with the ground tracking and control station. For satellites with high safety and reliability requirements, it is even necessary to dock with each batch of tracking and control stations generated by each manufacturer, and solidify the docking configuration as the tracking configuration after the satellite enters orbit; management difficulties: after the satellite enters orbit, the technical status of the satellite and the tracking and control station may change. At this time, it is necessary to manually modify the tracking and control configuration of all the tracking and control tasks participating in the satellite. Similarly, a change in the state of a satellite requires modification by m ground tracking and control stations, and a change in the state of a tracking and control station requires modification of the tracking and control configuration of n satellites. In addition, when the contents of the measurement and control plan are different, it is also necessary to adjust the measurement and control station equipment configuration and choose whether to load the corresponding link; manually completing the above operations requires high requirements for the operation and management personnel of the measurement and control station, with a lot of manual operations, low reliability, high cost and low efficiency.

[0048] The aerospace tracking and control station configuration method of the present invention can reduce workload and improve reliability. In the traditional mode, for m tracking and control stations to track n satellites, m×n sets of configuration files need to be prepared and maintained, involving a large number of manual operations. With the working method of the present invention, only one set of tracking and control equipment configuration information needs to be prepared for each tracking and control station, and one set of satellite tracking configuration information needs to be prepared for each satellite. Then, only m+n sets of configuration information files need to be prepared and maintained. The target configuration file is automatically generated in the computer. The tracking and control station and the satellite are configured with templated parameters. The tracking and control station does not need to adjust the equipment parameters according to different satellites; the satellite does not need to adjust the parameters according to different tracking and control stations. This greatly reduces the workload of the operation and maintenance personnel and improves the reliability of the system.

[0049] The aerospace tracking and control station configuration method provided by the present invention prepares tracking and control equipment configuration information and satellite tracking configuration information for each tracking and control equipment and satellite in advance, determines the target tracking and control equipment configuration information and the target satellite tracking configuration information in the server according to the tracking and control plan information, and combines the two to form a target configuration file, which can greatly reduce the workload of development and operation and maintenance personnel, simplify the configuration process, and improve work efficiency.

[0050] In some embodiments, step 130, determining a target configuration file based on target measurement and control equipment configuration information and target satellite tracking configuration information, includes: fusing the target measurement and control equipment configuration information with the target satellite tracking configuration information to obtain the target configuration file.

[0051] It can be understood that the fusion processing can be the superposition of the target measurement and control equipment configuration information and the target satellite tracking configuration information, that is, matching and fusing their respective parameters so that the formed target configuration file has parameters unique to both the target measurement and control equipment configuration information and the target satellite tracking configuration information.

[0052] In some embodiments, the target measurement and control device configuration information is fused with the target satellite tracking configuration information to obtain a target configuration file, including: replacing the target satellite tracking configuration information with a corresponding position in the target measurement and control device configuration information to obtain the target configuration file.

[0053] It is understandable that, in the target measurement and control equipment configuration information, there may be a description paragraph corresponding to the satellite tracking configuration information, and the target satellite tracking configuration information may be replaced into the description paragraph to generate a target configuration file.

[0054] If the target satellite tracking configuration information contains signal strength parameters, then the signal strength parameters can be mapped to the target measurement and control equipment configuration information based on the target satellite tracking configuration information. If the target satellite tracking configuration information does not contain signal strength parameters, the relevant parameters in the target measurement and control equipment configuration information can be directly used.

[0055] In some embodiments, step 130, determining the target configuration file based on the target measurement and control equipment configuration information and the target satellite tracking configuration information, also includes: determining the target configuration file based on guidance data, the target measurement and control equipment configuration information and the target satellite tracking configuration information, the guidance data including: at least one of the number of satellite orbital elements, satellite ephemeris data and antenna pointing angle data.

[0056] It can be understood that the boot data file can be the public parameter content pre-stored in the server, that is, no matter which tracking and control station matches the satellite, the boot data file is required. The boot data file is used to ensure that the tracking and control antenna of the tracking and control station can correctly point to the satellite when the tracking and control station tracks the satellite.

[0057] The satellite orbit elements in the guidance data file may be in an XML format file, the satellite ephemeris data may be in a TXT format file, and the antenna pointing angle data may be in a TXT format file.

[0058] In some embodiments, the measurement and control equipment configuration information includes: at least one of a signal strength parameter, a channel characteristic parameter, and an equipment support parameter.

[0059] It can be understood that the signal strength parameter is a parameter that describes the signal strength (including signal-to-noise ratio) required for sending and receiving space-ground signals. This type of parameter is an analog quantity. When setting the parameter, the target can be captured normally if it is set correctly within a range. For different types of equipment, in order to achieve the required satellite signal strength, different uplink powers and amplification factors may be used according to different orbits; in order to receive downlink signals normally, different amplification factors need to be set.

[0060] Channel characteristic parameters describe the characteristic types and corresponding characteristic values ​​of space-ground signals. These parameters are fixed values ​​and are deterministic and universal. When any measuring station implements measurement and control of a specific satellite, the parameters must be set completely as required.

[0061] Equipment support parameters are equipment status parameters that ensure the normal operation of ground equipment. The content of such parameters is related to the model of the equipment and is not directly related to the transmission of ground-to-ground data.

[0062] In some embodiments, the satellite tracking configuration information includes at least one of a satellite code, a satellite identifier, satellite channel parameters and configuration, and a template satellite code.

[0063] In some embodiments, the measurement and control plan information includes at least one of: a time period for the station to track the satellite, a mapping relationship between the ground and space channels, and ground data transmission information.

[0064] It is worth mentioning that the aerospace tracking and control station configuration method provided by the present invention can also enhance interactivity and reduce the workload of satellite network access. In the content of the present invention, the XSD file provides a detailed and structured description of the satellite tracking configuration content. When the tracking and control station provides services to the satellite, the satellite provides an XML file and verifies through a program to meet the constraints of the XSD file on the file structure. In this way, a large number of errors and differences in understanding that may exist in manual processing are eliminated, and the possibility of mismatching of space and earth parameters when the satellite enters the network is reduced.

[0065] The aerospace tracking and control station configuration device provided by the present invention is described below. The aerospace tracking and control station configuration device described below and the aerospace tracking and control station configuration method described above can be referenced to each other.

[0066] like Figure 2 As shown, the present invention further provides a space tracking and control station configuration device, which includes: an acquisition module 210, a first determination module 220, a second determination module 230 and a sending module 240.

[0067] An acquisition module 210 is used to acquire a plurality of measurement and control equipment configuration information, a plurality of satellite tracking configuration information and measurement and control plan information;

[0068] The first determination module 220 is used to determine the target measurement and control equipment configuration information from the plurality of measurement and control equipment configuration information and determine the target satellite tracking configuration information from the plurality of satellite tracking configuration files based on the measurement and control plan information;

[0069] A second determination module 230 is used to determine a target configuration file based on the target measurement and control equipment configuration information and the target satellite tracking configuration information;

[0070] The sending module 240 is used to send the target configuration file to the target measurement and control station.

[0071] In some embodiments, the second determination module 230 is further used to fuse the target measurement and control equipment configuration information with the target satellite tracking configuration information to obtain the target configuration file.

[0072] In some embodiments, the second determination module 230 is further used to obtain the target configuration file by replacing the target satellite tracking configuration information with a corresponding position in the target measurement and control device configuration information.

[0073] In some embodiments, the second determination module 230 is also used to determine the target configuration file based on guidance data, the target measurement and control equipment configuration information and the target satellite tracking configuration information, and the guidance data includes: at least one of: satellite orbital elements, satellite ephemeris data and antenna pointing angle data.

[0074] In some embodiments, the measurement and control equipment configuration information includes: at least one of a signal strength parameter, a channel characteristic parameter, and an equipment support parameter.

[0075] In some embodiments, the satellite tracking configuration information includes at least one of a satellite code, a satellite identifier, satellite channel parameters and configuration, and a template satellite code.

[0076] In some embodiments, the measurement and control plan information includes at least one of: a time period for the station to track the satellite, a mapping relationship between the ground and space channels, and ground data transmission information.

[0077] The aerospace tracking and control station configuration device provided in the embodiment of the present application is used to execute the above-mentioned aerospace tracking and control station configuration method. Its specific implementation method is consistent with the method implementation method and can achieve the same beneficial effects, which will not be repeated here.

[0078] Figure 3 An example of a physical structure diagram of an electronic device is shown in FIG. Figure 3 As shown, the electronic device may include: a processor 310, a communication interface 320, a memory 330 and a communication bus 340, wherein the processor 310, the communication interface 320 and the memory 330 communicate with each other through the communication bus 340. The processor 310 may call the logic instructions in the memory 330 to execute the aerospace tracking and control station configuration method, which includes: obtaining a plurality of tracking and control equipment configuration information, a plurality of satellite tracking configuration information and tracking and control plan information; based on the tracking and control plan information, determining the target tracking and control equipment configuration information from the plurality of tracking and control equipment configuration information, and determining the target satellite tracking configuration information from the plurality of satellite tracking configuration files; determining the target configuration file based on the target tracking and control equipment configuration information and the target satellite tracking configuration information; and sending the target configuration file to the target tracking and control station.

[0079] In addition, the logic instructions in the above-mentioned memory 330 can be implemented in the form of a software functional unit and can be stored in a computer-readable storage medium when it is sold or used as an independent product. Based on such an understanding, the technical solution of the present invention, in essence, 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, and the computer software product is stored in a storage medium, including a number of instructions for a computer device (which can be a personal computer, a server, or a network device, etc.) to perform all or part of the steps of the method described in each embodiment of the present invention. The aforementioned storage medium includes: U disk, mobile hard disk, read-only memory (ROM, Read-Only Memory), random access memory (RAM, Random Access Memory), disk or optical disk and other media that can store program codes.

[0080] On the other hand, the present invention also provides a computer program product, which includes a computer program stored on a non-transitory computer-readable storage medium, and the computer program includes program instructions. When the program instructions are executed by a computer, the computer can execute the aerospace tracking and control station configuration method provided by the above-mentioned methods, and the method includes: obtaining multiple tracking and control equipment configuration information, multiple satellite tracking configuration information and tracking and control plan information; based on the tracking and control plan information, determining the target tracking and control equipment configuration information from the multiple tracking and control equipment configuration information, and determining the target satellite tracking configuration information from the multiple satellite tracking configuration files; based on the target tracking and control equipment configuration information and the target satellite tracking configuration information, determining the target configuration file; and sending the target configuration file to the target tracking and control station.

[0081] On the other hand, the present invention also provides a non-transitory computer-readable storage medium having a computer program stored thereon, which, when executed by a processor, is implemented to execute the above-mentioned aerospace tracking and control station configuration methods, the methods comprising: obtaining a plurality of tracking and control equipment configuration information, a plurality of satellite tracking configuration information and tracking and control plan information; based on the tracking and control plan information, determining target tracking and control equipment configuration information from the plurality of tracking and control equipment configuration information, and determining target satellite tracking configuration information from the plurality of satellite tracking configuration files; determining a target configuration file based on the target tracking and control equipment configuration information and the target satellite tracking configuration information; and sending the target configuration file to the target tracking and control station.

[0082] The device embodiments described above are merely illustrative, wherein the units described as separate components may or may not be physically separated, and the components displayed as units may or may not be physical units, that is, they may be located in one place, or they may be distributed on multiple network units. Some or all of the modules may be selected according to actual needs to achieve the purpose of the scheme of this embodiment. Ordinary technicians in this field can understand and implement it without paying creative labor.

[0083] Through the description of the above implementation methods, those skilled in the art can clearly understand that each implementation method can be implemented by means of software plus a necessary general hardware platform, and of course, it can also be implemented by hardware. Based on this understanding, the above technical solution is essentially or the part that contributes to the prior art can be embodied in the form of a software product, and the computer software product can be stored in a computer-readable storage medium, such as ROM / RAM, a disk, an optical disk, etc., including a number of instructions for a computer device (which can be a personal computer, a server, or a network device, etc.) to execute the methods described in each embodiment or some parts of the embodiments.

[0084] Finally, it should be noted that the above embodiments are only used to illustrate the technical solutions of the present invention, rather than to limit it. Although the present invention has been described in detail with reference to the aforementioned embodiments, those skilled in the art should understand that they can still modify the technical solutions described in the aforementioned embodiments, or make equivalent replacements for some of the technical features therein. However, these modifications or replacements do not deviate the essence of the corresponding technical solutions from the spirit and scope of the technical solutions of the embodiments of the present invention.

Claims

1. A method for configuring an aerospace tracking and control station, characterized in that: include: Acquire multiple measurement and control equipment configuration information, multiple satellite tracking configuration information and measurement and control plan information, wherein the satellite tracking configuration information is the physical parameters of the normal operation of the satellite, and multiple satellite tracking configuration information can form a satellite tracking configuration information library; the measurement and control equipment configuration information is the configurable parameters and control commands corresponding to the measurement and control equipment on the ground, and multiple measurement and control equipment configuration information can form a measurement and control equipment configuration information library; the measurement and control plan information is used to present specific information of this measurement and control task; Based on the measurement and control plan information, determine target measurement and control equipment configuration information from the plurality of measurement and control equipment configuration information, and determine target satellite tracking configuration information from the plurality of satellite tracking configuration files; Determining a target configuration file based on the target measurement and control equipment configuration information and the target satellite tracking configuration information; Sending the target configuration file to a target measurement and control station; Determining the target configuration file based on the target measurement and control device configuration information and the target satellite tracking configuration information includes: determining the target configuration file based on guidance data, the target measurement and control device configuration information and the target satellite tracking configuration information, wherein the guidance data includes: satellite orbit elements, satellite ephemeris data and antenna pointing angle data; The measurement and control equipment configuration information includes: signal strength parameters, channel characteristic parameters and equipment support parameters; The satellite tracking configuration information includes: satellite code, satellite identification, satellite channel parameters and configuration, and template satellite code; The measurement and control plan information includes: the time period for the station to track the satellite, the mapping relationship between the sky and the ground channels, and the ground data transmission information; The determining of the target configuration file based on the target measurement and control equipment configuration information and the target satellite tracking configuration information includes: The target measurement and control equipment configuration information is integrated with the target satellite tracking configuration information to obtain the target configuration file; If the satellite tracking configuration information includes signal strength parameters, mapping the signal strength parameters to the target measurement and control equipment configuration information according to the target satellite tracking configuration information; If the satellite tracking configuration information does not include signal strength parameters, the signal strength parameters in the target measurement and control equipment configuration information are retained.

2. The method for configuring aerospace tracking and control stations according to claim 1, characterized in that: The step of fusing the target measurement and control equipment configuration information with the target satellite tracking configuration information to obtain the target configuration file includes: The target configuration file is obtained by replacing the target satellite tracking configuration information with the corresponding position in the target measurement and control equipment configuration information.

3. A space tracking and control station configuration device, characterized in that: The method for configuring a space tracking and control station according to claim 1 comprises: An acquisition module is used to acquire multiple measurement and control equipment configuration information, multiple satellite tracking configuration information and measurement and control plan information, wherein the satellite tracking configuration information is the physical parameters of the normal operation of the satellite, and multiple satellite tracking configuration information can form a satellite tracking configuration information library; the measurement and control equipment configuration information is the configurable parameters and control commands corresponding to the measurement and control equipment on the ground, and multiple measurement and control equipment configuration information can form a measurement and control equipment configuration information library; the measurement and control plan information is used to present specific information of this measurement and control task; A first determination module is used to determine target measurement and control equipment configuration information from the plurality of measurement and control equipment configuration information based on the measurement and control plan information, and to determine target satellite tracking configuration information from the plurality of satellite tracking configuration files; A second determination module is used to determine a target configuration file based on the target measurement and control equipment configuration information and the target satellite tracking configuration information; The sending module is used to send the target configuration file to the target measurement and control station.

4. An electronic device comprising a memory, a processor, and a computer program stored in the memory and executable on the processor, wherein: When the processor executes the program, the steps of the aerospace tracking and control station configuration method as described in any one of claims 1 to 2 are implemented.

5. A non-transitory computer-readable storage medium having a computer program stored thereon, characterized in that: When the computer program is executed by a processor, the steps of the aerospace tracking and control station configuration method as described in any one of claims 1 to 2 are implemented.

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