CN113535259A - Configuration method and device for aerospace measurement and control station - Google Patents
Configuration method and device for aerospace measurement and control station Download PDFInfo
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Abstract
The invention provides a method and a device for configuring an aerospace measurement and control station, wherein the method for configuring the aerospace measurement and control station comprises the following steps: acquiring configuration information of a plurality of measurement and control devices, tracking configuration information of a plurality of satellites and measurement and control plan information; determining target measurement and control equipment configuration information from the plurality of measurement and control equipment configuration information and determining target satellite tracking configuration information from the plurality of satellite tracking configuration files based on the measurement and control plan information; determining a target configuration file based on the configuration information of the target measurement and control equipment and the tracking configuration information of the target satellite; and sending the target configuration file to a target measurement and control station. According to the configuration method and the configuration device for the aerospace measurement and control station, the configuration information of the plurality of measurement and control devices and the configuration information of the plurality of satellite tracking devices are manufactured in advance, the configuration information of the target measurement and control device and the configuration information of the target satellite tracking are determined in the server according to the measurement and control plan information, a target configuration file is formed, the workload of development, operation and maintenance personnel can be greatly reduced, the configuration process is simplified, and the working efficiency is improved.
Description
Technical Field
The invention relates to the technical field of aerospace engineering, in particular to a configuration method and device of an aerospace measurement and control station.
Background
With the development of aerospace technology, a plurality of satellites are launched into space by human beings, in the process of satellite operation, the satellites need to be monitored through an aerospace measurement and control station, a plurality of aerospace measurement and control stations are often deployed on the ground, meanwhile, the number of the satellites needing to be monitored by the aerospace measurement and control station is also many, and the space-ground interfaces of measurement and control systems, working frequencies, channel codes, data frame management and the like of different satellites are constantly changed, so that specific and complex configuration operation needs to be performed when different target satellites are detected for each aerospace measurement and control station. In addition, a plurality of measurement and control stations tracking the same satellite have certain differences in technical state.
In the existing method for configuring the space measurement and control station, before a task starts, a measurement station operation and maintenance worker needs to compile a specific configuration file according to the matching relationship between a specific ground measurement and control station and a specific tracking service satellite object, configure various tracking devices, and control an antenna to point to a satellite to start tracking measurement and control work after the time when the task starts. The operation is completed manually, the requirement on operation management personnel of the measurement and control station is high, the manual operation is multiple, the reliability is low, the cost is high, and the efficiency is low.
Disclosure of Invention
The invention provides a configuration method and a configuration device for an aerospace measurement and control station, which are used for solving the defects that manual configuration is needed when each satellite object is detected in the prior art, the configuration process is complex, the consumed labor cost is high, and the working efficiency is low, so that the workload of development, operation and maintenance personnel is reduced, the configuration process is simplified, and the working efficiency is improved.
The invention provides a method for configuring an aerospace measurement and control station, which comprises the following steps: acquiring configuration information of a plurality of measurement and control devices, tracking configuration information of a plurality of satellites and measurement and control plan information; determining target measurement and control equipment configuration information from the plurality of measurement and control equipment configuration information and determining target satellite tracking configuration information from the plurality of satellite tracking configuration files based on the measurement and control plan information; determining a target configuration file based on the target measurement and control equipment configuration information and the target satellite tracking configuration information; and sending the target configuration file to a target measurement and control station.
According to the configuration method of the aerospace measurement and control station, the determining of the target configuration file based on the target measurement and control equipment configuration information and the target satellite tracking configuration information comprises the following steps: and fusing the configuration information of the target measurement and control equipment and the tracking configuration information of the target satellite to obtain the target configuration file.
According to the configuration method of the aerospace measurement and control station, the fusion processing is performed on the target measurement and control equipment configuration information and the target satellite tracking configuration information to obtain the target configuration file, and the method comprises the following steps: and replacing the target satellite tracking configuration information with the corresponding position in the target measurement and control equipment configuration information to obtain the target configuration file.
According to the configuration method of the aerospace measurement and control station, the determining of the target configuration file based on the target measurement and control equipment configuration information and the target satellite tracking configuration information comprises the following steps: determining the target configuration file based on guiding data, the target measurement and control equipment configuration information and the target satellite tracking configuration information, wherein the guiding data comprises: at least one of a number of satellite orbits, satellite ephemeris data, and antenna pointing angle data.
According to the configuration method of the aerospace measurement and control station, the configuration information of the measurement and control equipment comprises the following steps: at least one of a signal strength parameter, a channel characteristic parameter, and a device support parameter.
According to the configuration method of the aerospace measurement and control station, provided by the invention, the satellite tracking configuration information comprises: at least one of a satellite code number, a satellite identification, satellite channel parameters and configurations, and a template satellite code number.
According to the configuration method of the aerospace measurement and control station, the measurement and control plan information comprises the following steps: and the observation station tracks at least one of the time period of the satellite, the mapping relation of the sky-ground channel and the ground data transmission information.
The invention also provides a configuration device of the space measurement and control station, which comprises the following components: the acquisition module is used for acquiring configuration information of a plurality of measurement and control devices, tracking configuration information of a plurality of satellites and measurement and control plan information; the first determining module is used for determining target measurement and control equipment configuration information from the plurality of measurement and control equipment configuration information and determining target satellite tracking configuration information from the plurality of satellite tracking configuration files based on the measurement and control plan information; the second determination module is used for determining a target configuration file based on the configuration information of the target measurement and control equipment and the tracking configuration information of the target satellite; and the sending module is used for sending the target configuration file to a target measurement and control station.
The invention also provides an electronic device, which comprises a memory, a processor and a computer program which is stored on the memory and can run on the processor, wherein the processor executes the computer program to realize the steps of any one of the configuration methods of the space measurement and control station.
The invention also provides a non-transitory computer readable storage medium having stored thereon a computer program which, when executed by a processor, performs the steps of the configuration method of the space measurement and control station as described in any one of the above.
According to the configuration method and the configuration device for the aerospace measurement and control station, the measurement and control device configuration information and the satellite tracking configuration information are respectively manufactured for each measurement and control device and each satellite in advance, the target measurement and control device configuration information and the target satellite tracking configuration information are determined in the server according to the measurement and control plan information and are combined to form the target configuration file, so that the workload of development, operation and maintenance personnel can be greatly reduced, the configuration process is simplified, and the working efficiency is improved.
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In order to more clearly illustrate the technical solutions of the present invention or the prior art, the drawings needed for the description of the embodiments or the prior art will be briefly described below, and it is obvious that the drawings in the following description are some embodiments of the present invention, and those skilled in the art can also obtain other drawings according to the drawings without creative efforts.
FIG. 1 is a schematic flow chart of a configuration method of an aerospace measurement and control station provided by the invention;
FIG. 2 is a schematic structural diagram of a configuration device of an aerospace measurement and control station provided by the invention;
fig. 3 is a schematic structural diagram of an electronic device provided in the present invention.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention clearer, the technical solutions of the present invention will be clearly and completely described below with reference to the accompanying drawings, and it is obvious that the described embodiments are some, but not all embodiments of the present invention. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
In the description herein, references to the description of the term "one embodiment," "some embodiments," "an example," "a specific example," or "some examples," etc., mean that a particular feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of an embodiment of the invention. In this specification, the schematic representations of the terms used above are not necessarily intended to refer to the same embodiment or example. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples. Furthermore, various embodiments or examples and features of different embodiments or examples described in this specification can be combined and combined by one skilled in the art without contradiction.
The following describes a configuration method and device of an aerospace measurement and control station according to the present invention with reference to fig. 1 to 3.
The space flight measurement and control network is an important component of space flight system engineering and mainly comprises a space flight measurement control center, an operation management center, an application system, a user management center, a globally deployed ground measurement and control station, a marine measurement ship and a space deployed relay satellite, wherein the relay satellite belongs to a space-based measurement and control station in a broad sense, and the three types of measurement equipment are collectively called as the measurement and control station in the following.
The task of the measurement and control station is to directly perform tracking measurement, remote control, communication and the like on the spacecraft, transmit the received measurement and remote measurement information to the space control center, communicate with the spacecraft according to the instruction of the space control center, and complete the control of the spacecraft by matching with the control center. The measurement and control station can also independently control the spacecraft according to a specified program. The equipment of the measurement and control station comprises an external measurement system, a remote control system, a communication system, a television system, a time unification system, a computer system and auxiliary equipment.
The measurement and control station generally provides services for a plurality of satellites simultaneously in a time division multiplexing mode, and the measurement and control systems, the working frequency, the channel coding, the data frame management and other space-ground interfaces of different satellites are constantly changed, so that the ground needs to perform complex state configuration when tracking each satellite. In addition, there is a certain difference in the state of the art between a plurality of stations tracking the same satellite.
In a conventional operating mode, a configuration file is established for each set of ground stations and each tracking service satellite object. Before the task starts, the operation and maintenance personnel of the survey station properly revises the configuration, loads the configuration file, configures various tracking devices, and controls the antenna to point to the satellite after the time when the task starts, so as to start the tracking measurement and control work.
As shown in fig. 1, the invention provides a method for configuring an aerospace measurement and control station, where the method for configuring an aerospace measurement and control station may be run in a server, the server may be in communication connection with the measurement and control station, and the server may distribute data to the measurement and control station, and the method for configuring an aerospace measurement and control station includes: as follows from step 110 to step 140.
In step 110, configuration information of a plurality of measurement and control devices, configuration information of a plurality of satellite tracking devices, and measurement and control plan information are obtained.
It can be understood that the configuration information of the measurement and control equipment is configurable parameters and control commands corresponding to the measurement and control equipment on the ground, and the configuration information of the measurement and control equipment can ensure the normal operation of the ground through remote control and configuration and can work for the normal operation of measurement and control of various types of satellites.
It should be noted that the measurement and control device configuration information corresponding to different measurement and control stations is different, and a plurality of measurement and control stations correspond to a plurality of measurement and control device configuration information, and the plurality of measurement and control device configuration information can form a measurement and control device configuration information base.
The measurement and control device configuration information may include all parameters of the measurement and control station, and may be a file in an XML format.
The satellite tracking configuration information is physical parameters of normal operation of the satellites, each satellite has specific satellite tracking configuration information, the satellite tracking configuration information corresponding to different satellites is different, a plurality of satellites correspond to a plurality of satellite tracking configuration information, and the plurality of satellite tracking configuration information can form a satellite tracking configuration information base.
The satellite tracking configuration information may be described in the form of an XML file schema (XSD) file. Each satellite tracking configuration information is an XML file whose structure needs to satisfy the constraints of the architecture file XSD file.
The measurement and control plan information is used for presenting specific information of the measurement and control task, that is, which measurement and control station is used for measuring and controlling which satellite, and the measurement and control plan information may include at least one of a time period when the measurement station tracks the satellite, a mapping relation of a space-ground channel, and ground data transmission information.
The measurement and control plan information may be a file in an XML format.
And step 120, determining target measurement and control equipment configuration information from the plurality of measurement and control equipment configuration information and determining target satellite tracking configuration information from the plurality of satellite tracking configuration files based on the measurement and control plan information.
It can be understood that according to the measurement and control plan information, the target measurement and control station and the target satellite corresponding to the current measurement and control can be determined, and the target measurement and control station can be matched with the target satellite. Then, the configuration information of the target measurement and control equipment corresponding to the target measurement and control station can be found from the configuration information of the plurality of measurement and control equipment, and the tracking configuration information of the target satellite corresponding to the target satellite can be found from the plurality of satellite tracking configuration files.
And step 130, determining a target configuration file based on the target measurement and control equipment configuration information and the target satellite tracking configuration information.
It can be understood that after the configuration information of the target measurement and control device and the tracking configuration information of the target satellite are determined, the configuration information of the target measurement and control device and the tracking configuration information of the target satellite can be combined, so that a target configuration file can be obtained. The target configuration file can be executed by the target measurement and control station.
It should be noted that the process of combining the target measurement and control device configuration information and the target satellite tracking configuration information may be performed automatically in a computer, and may be performed by using a common fusion and matching algorithm.
The target configuration file may be an XML formatted file.
And step 140, sending the target configuration file to a target measurement and control station.
It can be understood that after the target configuration file is obtained, the target configuration file may be sent to the target measurement and control station, and the target configuration file includes, in addition to the start and end time of the measurement and control task, task type information, that is, whether to implement remote control, whether to implement external measurement, whether to accept remote measurement, and whether to receive data transmission. And after receiving the target configuration file, the target measurement and control station can automatically operate the target configuration file to perform measurement and control work on the target satellite.
It should be noted that, in the existing operating mode, for m measurement and control stations to track n satellites, an m × n set of configuration files is prepared. Because different satellite working modes and working parameters are different, n sets of configuration files of each measurement and control station are greatly different; the working mode and specific parameters of each measurement and control station are also different, so that the m configuration files of each satellite are also different.
With the rapid development of large-scale constellation systems, dozens of ground stations are required to simultaneously measure and control thousands of satellites. In the prior art, the workload is huge and the reliability is not high. The main problems are as follows: (one) difficulty in accessing the network: in the traditional mode, before the satellite is launched for the last day, a butt joint test with a ground measurement and control station is required. Even the satellite with high requirements on safety and reliability needs to be docked with each batch of ground station equipment generated by each manufacturer, and the docked configuration is solidified to be used as the tracking configuration after the satellite is in orbit. (II) difficulty in management: after the satellite enters the orbit, the technical states of the satellite and the ground measurement and control station may change, and at this time, the configuration files of all the measurement and control stations participating in the satellite measurement and control task need to be modified manually. Similarly, one state change of the satellite needs to be modified by m measurement and control stations on the ground, and one state change of the measurement and control station needs to modify the measurement and control configuration of n satellites. In addition, when the contents of the measurement and control plan are different, the configuration piece of the measurement and control station needs to be adjusted to select whether to load the corresponding link.
Under traditional mode, generally the operation managers have been disposed at observing and controlling station, and the work above the manual work is accomplished, and is high to fortune pipe personnel's requirement, and manual operation is many. With the rapid development of the constellation system, the traffic volume of the above work will increase rapidly, and the reliability will also decrease.
In other words, in the existing working mode, for m measurement and control stations tracking n satellites, m × n sets of configuration files are prepared, and because different satellite working modes and working parameters are different, n sets of configuration files of each measurement and control station have great difference; the working mode and specific parameters of each measurement and control station are also different, so that the m configuration files of each satellite are also different. With the rapid development of large-scale constellation systems, dozens of ground stations are required to simultaneously measure and control thousands of satellites. The main problems of the prior art are as follows: the method is difficult to access the network, the satellite needs to be in butt joint with a ground measurement and control station before launching the satellite, the satellite with higher requirements on safety and reliability even needs to be in butt joint with each batch of measurement and control stations generated by each manufacturer, and the butt joint configuration is solidified to be used as the tracking configuration after the satellite enters the orbit; the management is difficult: after the satellite enters the orbit, the technical states of the satellite and the measurement and control station may change, and at this time, all measurement and control configurations participating in the satellite measurement and control task need to be modified manually. Similarly, one state change of the satellite needs to be modified by m measurement and control stations on the ground, and one state change of the measurement and control station needs to modify the measurement and control configuration of n satellites. In addition, when the contents in the measurement and control plan are different, the equipment configuration of the measurement and control station needs to be adjusted, and whether a corresponding link is loaded or not is selected; the operation is completed manually, the requirement on operation management personnel of the measurement and control station is high, the manual operation is multiple, the reliability is low, the cost is high, and the efficiency is low.
The configuration method of the space measurement and control station can reduce the workload and improve the reliability. In a traditional mode, for m measurement and control stations to track n satellites, an m x n set of configuration files are prepared and maintained, and a large amount of manual operation is involved. By adopting the working mode of the invention, only one measurement and control equipment configuration information is required to be prepared for each measurement and control station, and one satellite tracking configuration information is required to be prepared for each satellite, so that only m + n sets of configuration information files are required to be prepared and maintained, the target configuration files are automatically generated in a computer, the measurement and control stations and the satellites are in template parameter configuration, and the measurement and control stations do not need to adjust equipment parameters according to different satellites; the satellite does not need to adjust parameters according to different measurement and control stations, so that the working intensity of operation and maintenance personnel is greatly reduced, and the working reliability of the system is also improved.
According to the configuration method of the aerospace measurement and control station, the measurement and control device configuration information and the satellite tracking configuration information are respectively manufactured aiming at each measurement and control device and each satellite in advance, the target measurement and control device configuration information and the target satellite tracking configuration information are determined in the server according to the measurement and control plan information and are combined to form the target configuration file, so that the workload of development, operation and maintenance personnel can be greatly reduced, the configuration process is simplified, and the working efficiency is improved.
In some embodiments, the step 130 of determining the target configuration file based on the target measurement and control device configuration information and the target satellite tracking configuration information includes: and carrying out fusion processing on the configuration information of the target measurement and control equipment and the tracking configuration information of the target satellite to obtain a target configuration file.
It can be understood that the fusion processing may be a process of superimposing the configuration information of the target measurement and control device and the tracking configuration information of the target satellite, that is, matching and fusing respective parameters, so that the formed target configuration file has parameters specific to both the configuration information of the target measurement and control device and the tracking configuration information of the target satellite.
In some embodiments, the fusion processing of the configuration information of the target measurement and control device and the tracking configuration information of the target satellite to obtain a target configuration file includes: and replacing the target satellite tracking configuration information to the corresponding position in the target measurement and control equipment configuration information to obtain a target configuration file.
It can be understood that the configuration information of the target measurement and control device may have a description section corresponding to the satellite tracking configuration information, and the target satellite tracking configuration information may be replaced to the description section, so as to generate a target configuration file.
If the target satellite tracking configuration information has the signal intensity parameters, the signal intensity parameters can be projected into the target measurement and control equipment configuration information according to the target satellite tracking configuration information, and if the target satellite tracking configuration information does not have the signal intensity parameters, the related parameters in the target measurement and control equipment configuration information can be directly used.
In some embodiments, the step 130 of determining the target configuration file based on the target measurement and control device configuration information and the target satellite tracking configuration information further includes: determining a target configuration file based on the guiding data, the target measurement and control equipment configuration information and the target satellite tracking configuration information, wherein the guiding data comprises: at least one of a number of satellite orbits, satellite ephemeris data, and antenna pointing angle data.
It can be understood that the guidance data file may be public parameter content pre-stored in the server, that is, the guidance data file is required no matter which measurement and control station is matched with the satellite, and the guidance data file is used when the measurement and control station tracks the satellite, and the measurement and control antenna of the measurement and control station can correctly point to the satellite.
The number of satellite orbits in the guidance data file may be an XML format file, the satellite ephemeris data may be a TXT format file, and the antenna pointing angle data may be a TXT format file.
In some embodiments, the measurement and control device configuration information includes: at least one of a signal strength parameter, a channel characteristic parameter, and a device support parameter.
It is understood that the signal strength parameter is a parameter describing the signal strength (including signal-to-noise ratio) required for the transmission and reception of the signals from the sky and the earth, and such a parameter is an analog quantity, and when the parameter is set, the target can be normally captured within a range by correctly setting the parameter. For different types of equipment, different uplink powers and amplification factors may be adopted according to different orbits in order to realize the required satellite required signal intensity; in order to normally receive downlink signals, different amplification factors need to be set.
The channel characteristic parameters are used for describing the characteristic types and corresponding characteristic values of the space and ground signals, the parameters are determined values and have determinacy and universality, and when any one observation station carries out measurement and control on a specific satellite, the parameters must be set completely according to requirements.
The equipment support parameters are equipment state parameters for ensuring normal operation of ground equipment, and the content of the parameters is related to the model of the equipment and is not directly related to the transmission of the world data.
In some embodiments, the satellite tracking configuration information includes: at least one of a satellite code number, a satellite identification, satellite channel parameters and configurations, and a template satellite code number.
In some embodiments, the measurement and control plan information includes: and the observation station tracks at least one of the time period of the satellite, the mapping relation of the sky-ground channel and the ground data transmission information.
It is worth mentioning that the configuration method of the space flight measurement and control station provided by the invention can also enhance the interactivity and reduce the workload of satellite network access. In the context of the present invention, the XSD file describes the satellite tracking configuration context in a detailed and structured manner. When the measurement and control station provides service for the satellite, the satellite side provides an XML file, and the restriction of an XSD file on a file structure is met through program verification. In this way, a great amount of errors and understanding differences which may exist in manual processing are eliminated, and the possibility of mismatching of the space and ground parameters when the satellite accesses the network is reduced.
The following describes the configuration device of the space measurement and control station provided by the present invention, and the configuration device of the space measurement and control station described below and the configuration method of the space measurement and control station described above can be referred to correspondingly.
As shown in fig. 2, the present invention further provides an aerospace measurement and control station configuration device, where the aerospace measurement and control station configuration device includes: an acquisition module 210, a first determination module 220, a second determination module 230, and a sending module 240.
An obtaining module 210, configured to obtain configuration information of a plurality of measurement and control devices, configuration information of a plurality of satellite tracking, and measurement and control plan information;
the first determining module 220 is configured to determine target measurement and control device configuration information from the plurality of measurement and control device configuration information and determine target satellite tracking configuration information from the plurality of satellite tracking configuration files based on the measurement and control plan information;
a second determining module 230, configured to determine a target configuration file based on the target measurement and control device configuration information and the target satellite tracking configuration information;
and the sending module 240 is configured to send the target configuration file to the target measurement and control station.
In some embodiments, the second determining module 230 is further configured to perform fusion processing on the configuration information of the target measurement and control device and the configuration information of the target satellite tracking, so as to obtain the target configuration file.
In some embodiments, the second determining module 230 is further configured 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.
In some embodiments, the second determining module 230 is further configured to determine the target configuration file based on guidance data, the target measurement and control device configuration information, and the target satellite tracking configuration information, where the guidance data includes: at least one of a number of satellite orbits, satellite ephemeris data, and antenna pointing angle data.
In some embodiments, the measurement and control device configuration information includes: at least one of a signal strength parameter, a channel characteristic parameter, and a device support parameter.
In some embodiments, the satellite tracking configuration information comprises: at least one of a satellite code number, a satellite identification, satellite channel parameters and configurations, and a template satellite code number.
In some embodiments, the measurement and control plan information includes: and the observation station tracks at least one of the time period of the satellite, the mapping relation of the sky-ground channel and the ground data transmission information.
The configuration device for the space measurement and control station provided by the embodiment of the application is used for executing the configuration method for the space measurement and control station, the specific implementation mode is consistent with the method implementation mode, the same beneficial effects can be achieved, and the details are not repeated here.
Fig. 3 illustrates a physical structure diagram of an electronic device, which may include, as shown in fig. 3: a processor (processor)310, a communication Interface (communication Interface)320, a memory (memory)330 and a communication bus 340, wherein the processor 310, the communication Interface 320 and the memory 330 communicate with each other via the communication bus 340. The processor 310 may invoke logic instructions in the memory 330 to perform a space measurement and control station configuration method, the method comprising: acquiring configuration information of a plurality of measurement and control devices, tracking configuration information of a plurality of satellites and measurement and control plan information; determining target measurement and control equipment configuration information from the plurality of measurement and control equipment configuration information and determining target satellite tracking configuration information from the plurality of satellite tracking configuration files based on the measurement and control plan information; determining a target configuration file based on the target measurement and control equipment configuration information and the target satellite tracking configuration information; and sending the target configuration file to a target measurement and control station.
In addition, the logic instructions in the memory 330 may be implemented in the form of software functional units and stored in a computer readable storage medium when the software functional units are sold or used as independent products. Based on such understanding, the technical solution of the present invention may be embodied in the form of a software product, which is stored in a storage medium and includes instructions for causing a computer device (which may be a personal computer, a server, or a network device) to execute all or part of the steps of the method according to the embodiments of the present invention. And the aforementioned storage medium includes: a U-disk, a removable hard disk, a Read-Only Memory (ROM), a Random Access Memory (RAM), a magnetic disk or an optical disk, and other various media capable of storing program codes.
In another aspect, the present invention also provides a computer program product, the computer program product including a computer program stored on a non-transitory computer-readable storage medium, the computer program including program instructions, when the program instructions are executed by a computer, the computer being capable of executing the method for configuring an space measurement and control station provided by the above methods, the method including: acquiring configuration information of a plurality of measurement and control devices, tracking configuration information of a plurality of satellites and measurement and control plan information; determining target measurement and control equipment configuration information from the plurality of measurement and control equipment configuration information and determining target satellite tracking configuration information from the plurality of satellite tracking configuration files based on the measurement and control plan information; determining a target configuration file based on the target measurement and control equipment configuration information and the target satellite tracking configuration information; and sending the target configuration file to a target measurement and control station.
In yet another aspect, the present invention further provides a non-transitory computer readable storage medium, on which a computer program is stored, the computer program being implemented by a processor to perform the method for configuring an aerospace measurement and control station provided in the foregoing aspects, the method including: acquiring configuration information of a plurality of measurement and control devices, tracking configuration information of a plurality of satellites and measurement and control plan information; determining target measurement and control equipment configuration information from the plurality of measurement and control equipment configuration information and determining target satellite tracking configuration information from the plurality of satellite tracking configuration files based on the measurement and control plan information; determining a target configuration file based on the target measurement and control equipment configuration information and the target satellite tracking configuration information; and sending the target configuration file to a target measurement and control station.
The above-described embodiments of the apparatus are merely illustrative, and the units described as separate parts may or may not be physically separate, and parts displayed as units may or may not be physical units, may be located in one place, or may be distributed on a plurality of network units. Some or all of the modules may be selected according to actual needs to achieve the purpose of the solution of the present embodiment. One of ordinary skill in the art can understand and implement it without inventive effort.
Through the above description of the embodiments, those skilled in the art will clearly understand that each embodiment can be implemented by software plus a necessary general hardware platform, and certainly can also be implemented by hardware. With this understanding in mind, the above-described technical solutions may be embodied in the form of a software product, which can be stored in a computer-readable storage medium such as ROM/RAM, magnetic disk, optical disk, etc., and includes instructions for causing a computer device (which may be a personal computer, a server, or a network device, etc.) to execute the methods described in the embodiments or some parts of the embodiments.
Finally, it should be noted that: the above examples are only intended to illustrate the technical solution of the present invention, but not to limit it; although the present invention has been described in detail with reference to the foregoing embodiments, it will be understood by those of ordinary skill in the art that: the technical solutions described in the foregoing embodiments may still be modified, or some technical features may be equivalently replaced; and such modifications or substitutions do not depart from the spirit and scope of the corresponding technical solutions of the embodiments of the present invention.
Claims (10)
1. A configuration method of an aerospace measurement and control station is characterized by comprising the following steps:
acquiring configuration information of a plurality of measurement and control devices, tracking configuration information of a plurality of satellites and measurement and control plan information;
determining target measurement and control equipment configuration information from the plurality of measurement and control equipment configuration information and determining target satellite tracking configuration information from the plurality of satellite tracking configuration files based on the measurement and control plan information;
determining a target configuration file based on the target measurement and control equipment configuration information and the target satellite tracking configuration information;
and sending the target configuration file to a target measurement and control station.
2. The configuration method of the space measurement and control station according to claim 1, wherein the determining a target configuration file based on the target measurement and control device configuration information and the target satellite tracking configuration information includes:
and fusing the configuration information of the target measurement and control equipment and the tracking configuration information of the target satellite to obtain the target configuration file.
3. The method according to claim 2, wherein the fusing the target measurement and control device configuration information and the target satellite tracking configuration information to obtain the target configuration file comprises:
and replacing the target satellite tracking configuration information with the corresponding position in the target measurement and control equipment configuration information to obtain the target configuration file.
4. The configuration method of any one of claims 1 to 3, wherein the determining a target configuration file based on the target measurement and control device configuration information and the target satellite tracking configuration information comprises:
determining the target configuration file based on guiding data, the target measurement and control equipment configuration information and the target satellite tracking configuration information, wherein the guiding data comprises: at least one of a number of satellite orbits, satellite ephemeris data, and antenna pointing angle data.
5. The configuration method of any one of claims 1 to 3, wherein the configuration information of the measurement and control device includes: at least one of a signal strength parameter, a channel characteristic parameter, and a device support parameter.
6. The configuration method of any one of claims 1 to 3, wherein the satellite tracking configuration information comprises: at least one of a satellite code number, a satellite identification, satellite channel parameters and configurations, and a template satellite code number.
7. The configuration method of the aerospace measurement and control station according to any one of claims 1-3, wherein the measurement and control plan information comprises: and the observation station tracks at least one of the time period of the satellite, the mapping relation of the sky-ground channel and the ground data transmission information.
8. A configuration device for an aerospace measurement and control station is characterized by comprising:
the acquisition module is used for acquiring configuration information of a plurality of measurement and control devices, tracking configuration information of a plurality of satellites and measurement and control plan information;
the first determining module is used for determining target measurement and control equipment configuration information from the plurality of measurement and control equipment configuration information and determining target satellite tracking configuration information from the plurality of satellite tracking configuration files based on the measurement and control plan information;
the second determination module is used for determining a target configuration file based on the configuration information of the target measurement and control equipment and the tracking configuration information of the target satellite;
and the sending module is used for sending the target configuration file to a target measurement and control station.
9. An electronic device comprising a memory, a processor and a computer program stored on the memory and executable on the processor, wherein the steps of the configuration method of an aerospace measurement and control station according to any one of claims 1 to 7 are implemented when the program is executed by the processor.
10. A non-transitory computer readable storage medium having stored thereon a computer program, wherein the computer program, when executed by a processor, implements the steps of the configuration method of an aerospace measurement and control station according to any one of claims 1 to 7.
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