Process information acquisition method and device of spacecraft ground measurement and control application software system

Abstract

The invention provides a process information acquisition method and device of a spacecraft ground measurement and control application software system, and relates to the technical field of spaceflight measurement and control. The method comprises the following steps: acquiring process configuration information of a pre-configured spacecraft ground measurement and control application software system; and in response to a target process information query instruction triggered for the process configuration information, executing the target process information query instruction to obtain a target process information query result. The device executes the method. According to the process information acquisition method and device of the spacecraft ground measurement and control application software system provided by the embodiment of the invention, the process information of the spacecraft ground measurement and control application software system can be conveniently and efficiently acquired.

Description

Technical Field

[0001] The present invention relates to the field of aerospace measurement and control technology, and in particular to a method and device for acquiring process information of a spacecraft ground measurement and control application software system. Background Art

[0002] With the development of aerospace technology, the on-orbit operation time, measurement and control communication coverage, information transmission volume, and transmission frequency of large spacecraft have been greatly improved compared with the past. Correspondingly, the requirements for spacecraft ground measurement and control application software systems are getting higher and higher. The cluster mode system architecture has gradually replaced the master-slave mode architecture and has become the high-reliability and high-availability strategy used by spacecraft ground measurement and control application software systems. In cluster mode, the number of physical servers used by the system has increased by an order of magnitude compared with the previous master-slave mode. The complex measurement and control application scenarios of aerospace missions have also put forward more functional requirements for spacecraft ground measurement and control application software systems. There are also more and more components in the spacecraft ground measurement and control application software system. According to statistics, the number of process instances of a large spacecraft ground measurement and control application software system exceeds 2,000. In addition, in the process of mission preparation, in order to enable development, testing, joint testing and other work to be carried out in parallel and business data to not conflict with each other, it is also necessary to logically divide the system into different operating networks and environments. The same server cluster is allowed to belong to different networks or environments, which can be automatically identified during process scheduling.

[0003] In summary, the number of processes in the spacecraft ground measurement and control application software system is very large, centralized information configuration and maintenance is very difficult, and it is not easy to obtain process information of the spacecraft ground measurement and control application software system. Summary of the invention

[0004] In view of the problems in the prior art, an embodiment of the present invention provides a method and device for obtaining process information of a spacecraft ground measurement and control application software system, which can at least partially solve the problems in the prior art.

[0005] On the one hand, the present invention provides a method for obtaining process information of a spacecraft ground measurement and control application software system, comprising:

[0006] Obtaining the process configuration information of the pre-configured spacecraft ground measurement and control application software system;

[0007] The process configuration information includes a cluster meta information table, a process scheduling information table and a host allocation information table; the cluster meta information table includes a cluster ID and a cluster name; the process scheduling information table includes a scheduling ID corresponding to each similar function, and each scheduling ID corresponds to the process scheduling configuration information and the cluster ID to which it belongs;

[0008] The host allocation information table includes at least one cluster ID corresponding to each host allocation ID, and each host allocation ID corresponds to host allocation configuration information;

[0009] In response to a target process information query instruction triggered by the process configuration information, the target process information query instruction is executed to obtain a target process information query result.

[0010] The step of obtaining the process configuration information of the pre-configured spacecraft ground measurement and control application software system includes:

[0011] The process configuration information is displayed in a view display mode compiled by SQL statements.

[0012] Wherein, the response to the target process information query instruction triggered by the process configuration information, executing the target process information query instruction to obtain the target process information query result, includes:

[0013] In response to a trigger action executed by a user by browsing the process configuration information, a pre-compiled SQL statement is called to execute the target process information query instruction to obtain the target process information query result.

[0014] Wherein, pre-configuring the process configuration information includes:

[0015] Configure all meta information consisting of each type of meta information table;

[0016] Among them, the metadata information stored in each type of metadata table does not change with the addition of new spacecraft missions;

[0017] Cluster the spacecraft according to their mission function similarities, and obtain a dispatch ID that corresponds to each similar function.

[0018] Traversing all the meta information to determine the progress scheduling configuration information corresponding to each similar function, establishing an association relationship between the progress scheduling configuration information and the scheduling ID, and obtaining the process scheduling information table;

[0019] All the meta information is traversed to determine the host allocation configuration information corresponding to each similar function, and an association relationship between the host allocation configuration information and the host allocation ID that realizes the corresponding similar function is established to obtain the host allocation information table.

[0020] The configuration includes all meta information consisting of each type of meta information table, including:

[0021] Configure the network meta-information table, host meta-information table, environment meta-information table, spacecraft meta-information table, mission meta-information table, cluster meta-information table, and process meta-information table.

[0022] The traversing of all the meta information to determine the progress scheduling configuration information corresponding to each similar function includes:

[0023] The cluster meta information table and the process meta information table are traversed to determine the progress scheduling configuration information corresponding to each similar function.

[0024] The traversing of all the meta information to determine the host allocation configuration information corresponding to each similar function includes:

[0025] The network meta information table, the host meta information table, the environment meta information table, the spacecraft meta information table, the task meta information table and the cluster meta information table are traversed to determine the host allocation configuration information corresponding to each similar function.

[0026] On the one hand, the present invention provides a process information acquisition device for a spacecraft ground measurement and control application software system, comprising:

[0027] A first acquisition unit is used to acquire process configuration information of a pre-configured spacecraft ground measurement and control application software system;

[0028] The process configuration information includes a cluster meta information table, a process scheduling information table and a host allocation information table; the cluster meta information table includes a cluster ID and a cluster name; the process scheduling information table includes a scheduling ID corresponding to each similar function, and each scheduling ID corresponds to the process scheduling configuration information and the cluster ID to which it belongs;

[0029] The host allocation information table includes at least one cluster ID corresponding to each host allocation ID, and each host allocation ID corresponds to host allocation configuration information;

[0030] The second acquisition unit is used to respond to the target process information query instruction triggered by the process configuration information, and execute the target process information query instruction to obtain the target process information query result.

[0031] In another aspect, an embodiment of the present invention provides an electronic device, including: a processor, a memory, and a bus, wherein:

[0032] The processor and the memory communicate with each other via the bus;

[0033] The memory stores program instructions that can be executed by the processor, and the processor calls the program instructions to execute the following method:

[0034] Obtaining the process configuration information of the pre-configured spacecraft ground measurement and control application software system;

[0035] The process configuration information includes a cluster meta information table, a process scheduling information table and a host allocation information table; the cluster meta information table includes a cluster ID and a cluster name; the process scheduling information table includes a scheduling ID corresponding to each similar function, and each scheduling ID corresponds to the process scheduling configuration information and the cluster ID to which it belongs;

[0036] The host allocation information table includes at least one cluster ID corresponding to each host allocation ID, and each host allocation ID corresponds to host allocation configuration information;

[0037] In response to a target process information query instruction triggered by the process configuration information, the target process information query instruction is executed to obtain a target process information query result.

[0038] An embodiment of the present invention provides a non-transitory computer-readable storage medium, including:

[0039] The non-transitory computer-readable storage medium stores computer instructions, which cause the computer to execute the following method:

[0040] Obtaining the process configuration information of the pre-configured spacecraft ground measurement and control application software system;

[0041] The process configuration information includes a cluster meta information table, a process scheduling information table and a host allocation information table; the cluster meta information table includes a cluster ID and a cluster name; the process scheduling information table includes a scheduling ID corresponding to each similar function, and each scheduling ID corresponds to the process scheduling configuration information and the cluster ID to which it belongs;

[0042] The host allocation information table includes at least one cluster ID corresponding to each host allocation ID, and each host allocation ID corresponds to host allocation configuration information;

[0043] In response to a target process information query instruction triggered by the process configuration information, the target process information query instruction is executed to obtain a target process information query result.

[0044] The process information acquisition method and device of a spacecraft ground measurement and control application software system provided in an embodiment of the present invention acquire the process configuration information of a pre-configured spacecraft ground measurement and control application software system; wherein the process configuration information includes a cluster meta-information table, a process scheduling information table and a host allocation information table; the cluster meta-information table includes a cluster ID and a cluster name; the process scheduling information table includes a scheduling ID corresponding to each similar function one by one, each scheduling ID corresponds to process scheduling configuration information and its cluster ID; the host allocation information table includes at least one cluster ID corresponding to each host allocation ID, each host allocation ID corresponds to host allocation configuration information; responding to a target process information query instruction triggered by the process configuration information, executing the target process information query instruction to obtain a target process information query result, can conveniently and efficiently acquire the process information of the spacecraft ground measurement and control application software system. BRIEF DESCRIPTION OF THE DRAWINGS

[0045] In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the following briefly introduces the drawings required for use in the embodiments or the prior art descriptions. Obviously, the drawings described below are only some embodiments of the present invention. For ordinary technicians in this field, other drawings can be obtained based on these drawings without creative work. In the drawings:

[0046] Figure 1 It is a flowchart of a method for obtaining process information of a spacecraft ground measurement and control application software system provided by an embodiment of the present invention.

[0047] Figure 2 It is a schematic diagram illustrating process configuration information provided by an embodiment of the present invention.

[0048] Figure 3 It is a structural diagram of a process information acquisition device of a spacecraft ground measurement and control application software system provided by an embodiment of the present invention.

[0049] Figure 4 A schematic diagram of the physical structure of an electronic device provided by an embodiment of the present invention. DETAILED DESCRIPTION

[0050] In order to make the purpose, technical scheme and advantages of the embodiments of the present invention more clear, the embodiments of the present invention are further described in detail below in conjunction with the accompanying drawings. Here, the illustrative embodiments of the present invention and their descriptions are used to explain the present invention, but are not intended to limit the present invention. It should be noted that, in the absence of conflict, the embodiments in this application and the features in the embodiments can be combined with each other arbitrarily.

[0051] Figure 1FIG. 1 is a flow chart of a method for obtaining process information of a spacecraft ground measurement and control application software system provided by an embodiment of the present invention. Figure 1 As shown, the process information acquisition method of the spacecraft ground measurement and control application software system provided by the embodiment of the present invention includes:

[0052] Step S1: obtaining process configuration information of a pre-configured spacecraft ground measurement and control application software system;

[0053] The process configuration information includes a cluster meta information table, a process scheduling information table and a host allocation information table; the cluster meta information table includes a cluster ID and a cluster name; the process scheduling information table includes a scheduling ID corresponding to each similar function, and each scheduling ID corresponds to the process scheduling configuration information and the cluster ID to which it belongs;

[0054] The host allocation information table includes at least one cluster ID corresponding to each host allocation ID, and each host allocation ID corresponds to host allocation configuration information.

[0055] Step S2: responding to the target process information query instruction triggered by the process configuration information, executing the target process information query instruction to obtain the target process information query result.

[0056] In the above step S1, the device obtains the process configuration information of the pre-configured spacecraft ground measurement and control application software system;

[0057] The process configuration information includes a cluster meta information table, a process scheduling information table and a host allocation information table; the cluster meta information table includes a cluster ID and a cluster name; the process scheduling information table includes a scheduling ID corresponding to each similar function, and each scheduling ID corresponds to the process scheduling configuration information and the cluster ID to which it belongs;

[0058] The host allocation information table includes at least one cluster ID corresponding to each host allocation ID, and each host allocation ID corresponds to host allocation configuration information. The device may be a computer device that executes the method, such as a server. It should be noted that the acquisition and analysis of data involved in the embodiment of the present invention is authorized by the user. The contents of the process scheduling information table and the host allocation information table are as follows: Figure 2 shown.

[0059] The step of obtaining the process configuration information of the pre-configured spacecraft ground measurement and control application software system includes:

[0060] The process configuration information is displayed in a view display mode compiled by SQL statements. The view display mode is implemented as follows:

[0061] CREATE VIEW V_COM_SCHEINFO

[0062] As SELECT

[0063] DISTINCT S.Schedule ID,

[0064] S. Process ID,

[0065] P. Process code,

[0066] P. Process name,

[0067] S. Process description,

[0068] S. Process execution path,

[0069] S. Process start time,

[0070] S. Process exit time,

[0071] S. Additional parameters of the process,

[0072] S. Process constraint mark,

[0073] S. Process constraint entry number,

[0074] S. Process constraint offset,

[0075] S. Process type,

[0076] B. Environment ID,

[0077] O. Spacecraft ID,

[0078] O. Spacecraft digital code,

[0079] O. Spacecraft English code,

[0080] O. Chinese name of the spacecraft,

[0081] A.Host name,

[0082] A.Host IP

[0083] FROM

[0084] Host allocation information table B,

[0085] Host Meta Information Table A,

[0086] Process scheduling information table S,

[0087] Spacecraft metadata table O,

[0088] Process meta information table P,

[0089] WHERE ( ( (

[0093] (S. Cluster ID = B. Cluster ID)

[0094] AND(STRPOS(CONCAT(CONCAT(','::text,(B.Host ID)::text),','::text),CONCAT(CONCAT(','::text,(A.Host ID)::text),','::text))>0) )

[0096] AND((B. Spacecraft ID)::numeric(18,0)=O. Spacecraft ID) )

[0098] AND((S.Process ID)::numeric(18,0)=P.Process ID) )

[0100] ORDER BY

[0101] S. Scheduling ID, S. Process ID, P. Process code, P. Process name, S. Process description, S. Process execution path, S. Process start time, S. Process exit time, S. Process additional parameters, S. Process constraint label, S. Process constraint entry number, S. Process constraint offset, B. Environment ID, O. Spacecraft ID, O. Spacecraft digital code, O. Spacecraft English code, O. Spacecraft Chinese name, A. Host name, A. Host IP, S. Process type.

[0102] In the above step S2, the device responds to the target process information query instruction triggered by the process configuration information, executes the target process information query instruction to obtain the target process information query result.

[0103] The responding to the target process information query instruction triggered by the process configuration information, executing the target process information query instruction to obtain the target process information query result, includes:

[0104] In response to the trigger action executed by the user by browsing the process configuration information, the pre-compiled SQL statement is called to execute the target process information query instruction to obtain the target process information query result. An example is as follows:

[0105] When a user starts a process of a specific spacecraft mission in a specific environment on a specific host, he can obtain the list of process information to be started by querying the view conditionally. For example, to obtain the process with the digital code 1234 of the spacecraft in environment 1 on the XDT1 server:

[0106] SELECT * FROM V_COM_SCHEINFO

[0107] WHERE

[0108] Host name = 'XDT1' and spacecraft number = '1234' and environment ID = 1.

[0109] Pre-configuring the process configuration information includes:

[0110] Configure all meta information consisting of each type of meta information table;

[0111] Among them, the metadata information stored in each type of metadata table does not change with the addition of new spacecraft missions;

[0112] Cluster the spacecraft according to their mission function similarities, and obtain a dispatch ID that corresponds to each similar function.

[0113] Traversing all the meta information to determine the progress scheduling configuration information corresponding to each similar function, establishing an association relationship between the progress scheduling configuration information and the scheduling ID, and obtaining the process scheduling information table;

[0114] Traverse all the meta information to determine the host allocation configuration information corresponding to each similar function, establish an association between the host allocation configuration information and the host allocation ID that implements the corresponding similar function, and obtain the host allocation information table. When adding a new spacecraft mission, only a small amount of configuration is required in the host allocation information table to specify the cluster to which it belongs, and there is no need to configure all process information on the host.

[0115] The process of configuring process configuration information is as follows:

[0116] 1. Configure all meta information.

[0117] 2. Configure process scheduling information. This step abstracts processes with similar functions into a functional cluster.

[0118] 3. Configure host allocation information. This step specifies the host, environment, network, and spacecraft on which each functional cluster runs.

[0119] The configuration consists of all meta information of each type of meta information table, including:

[0120] Configure the network meta-information table, host meta-information table, environment meta-information table, spacecraft meta-information table, mission meta-information table, cluster meta-information table, and process meta-information table. The meta-information is described as follows:

[0121] Stores all metadata information. This type of information usually only needs to be configured once. When adding a new task, it can be assumed that this type of information does not change with the new task. It includes the network meta information table, host meta information table, environment meta information table, spacecraft meta information table, mission meta information table, cluster meta information table, and process meta information table; they are described as follows:

[0122] The network meta-information table includes: network ID, network name.

[0123] The environment meta-information table includes: environment ID and environment name.

[0124] The host meta information table includes: host ID, host name, host IP, and network ID.

[0125] The cluster meta information table includes: cluster ID and cluster name.

[0126] The process meta-information table includes: process ID, process code, and process name.

[0127] The spacecraft meta-information table includes: spacecraft ID, mission ID, spacecraft English code, spacecraft Chinese name, and spacecraft digital code.

[0128] The task meta-information table includes: task ID, task English code, task Chinese name, and task digital code.

[0129] The related information is described as follows:

[0130] Store process scheduling information and associate process information with host information. When adding new tasks, mainly change this type of information, including process scheduling information and host allocation information.

[0131] The traversing all the meta information to determine the progress scheduling configuration information corresponding to each similar function includes:

[0132] The cluster meta information table and the process meta information table are traversed to determine the progress scheduling configuration information corresponding to each similar function.

[0133] The traversing of all the meta information to determine the host allocation configuration information corresponding to each similar function includes:

[0134] The network meta information table, the host meta information table, the environment meta information table, the spacecraft meta information table, the mission meta information table and the cluster meta information table are traversed to determine the host allocation configuration information corresponding to each similar function. Figure 2 Description.

[0135] The process information acquisition method of the spacecraft ground measurement and control application software system provided by the embodiment of the present invention can logically divide the process information that jointly realizes a certain function into different functional clusters at one time to address the technical problems of the existing large-scale spacecraft ground measurement and control application software system with a large number of servers, a large number of process instances, and difficulty in maintaining scheduling information. When the user maintains the information, he only needs to allocate server information to different functional clusters according to the network, environment, task, and goal, which greatly reduces the duplication of binding content and improves the binding efficiency.

[0136] The process information acquisition method of the spacecraft ground measurement and control application software system provided by the embodiment of the present invention is briefly described as follows:

[0137] 1. An efficient configuration method for process information of ground measurement and control application software systems for large spacecraft. Processes with similar functions are abstracted into a functional cluster for configuration binding, and then host allocation is performed based on the functional cluster granularity. This can greatly reduce the amount of process configuration information and improve the efficiency of process information configuration.

[0138] 2. An efficient way to obtain process information of large spacecraft ground measurement and control application software systems. Based on the configuration information defined in Technical Point 1, a process scheduling information view is defined, and process information can be quickly obtained by simply specifying the server, environment, and spacecraft.

[0139] The beneficial effects of the process information acquisition method of the spacecraft ground measurement and control application software system provided by the embodiment of the present invention are described as follows:

[0140] 1. It realizes the efficient process information configuration process under complex systems, and can realize the fast and efficient configuration of processes in multi-network, multi-environment, multi-host and multi-spacecraft of large-scale spacecraft ground measurement and control application software systems, greatly reducing information redundancy.

[0141] 2. It realizes efficient acquisition of process information under complex startup constraints, and can quickly acquire process information by simply specifying the server, environment, and spacecraft.

[0142] The process information acquisition method of a spacecraft ground measurement and control application software system provided in an embodiment of the present invention acquires the process configuration information of a pre-configured spacecraft ground measurement and control application software system; wherein the process configuration information includes a cluster meta-information table, a process scheduling information table and a host allocation information table; the cluster meta-information table includes a cluster ID and a cluster name; the process scheduling information table includes a scheduling ID corresponding to each similar function one by one, each scheduling ID corresponds to process scheduling configuration information and its cluster ID; the host allocation information table includes at least one cluster ID corresponding to each host allocation ID, each host allocation ID corresponds to host allocation configuration information; responding to a target process information query instruction triggered by the process configuration information, executing the target process information query instruction to obtain a target process information query result, can conveniently and efficiently acquire the process information of the spacecraft ground measurement and control application software system.

[0143] Furthermore, the obtaining of the process configuration information of the pre-configured spacecraft ground measurement and control application software system includes:

[0144] The process configuration information is displayed in a view display mode compiled by SQL statements. The above-mentioned embodiment can be referred to for explanation, which will not be described in detail.

[0145] Further, the response to the target process information query instruction triggered by the process configuration information, executing the target process information query instruction to obtain the target process information query result, includes:

[0146] In response to the trigger action executed by the user by browsing the process configuration information, the pre-compiled SQL statement is called to execute the target process information query instruction to obtain the target process information query result. The above embodiment can be referred to for description and will not be repeated here.

[0147] Further, pre-configuring the process configuration information includes:

[0148] All meta information consisting of each type of meta information table is configured; the above-mentioned embodiment can be referred to for description and will not be described in detail.

[0149] Among them, the metadata information stored in each type of metadata table does not change with the addition of new spacecraft missions; please refer to the above-mentioned embodiment for description and will not be repeated here.

[0150] Clustering is performed according to the similarity of the spacecraft mission functions to obtain a scheduling ID corresponding to each similar function. The above description can be referred to in the embodiment and will not be repeated here.

[0151] Traverse all the meta information to determine the progress scheduling configuration information corresponding to each similar function, establish an association relationship between the progress scheduling configuration information and the scheduling ID, and obtain the process scheduling information table; refer to the above embodiment for description and no further details will be given.

[0152] Traverse all the meta information to determine the host allocation configuration information corresponding to each similar function, establish an association between the host allocation configuration information and the host allocation ID that realizes the corresponding similar function, and obtain the host allocation information table.

[0153] Furthermore, the configuration includes all meta information consisting of each type of meta information table, including:

[0154] The network meta information table, host meta information table, environment meta information table, spacecraft meta information table, mission meta information table, cluster meta information table and process meta information table are configured. Please refer to the above embodiment for description, and no further details will be given.

[0155] Furthermore, the traversing of all the meta information to determine the progress scheduling configuration information corresponding to each similar function includes:

[0156] The cluster meta information table and the process meta information table are traversed to determine the progress scheduling configuration information corresponding to each similar function. The above-mentioned embodiments can be referred to for explanation and will not be described in detail.

[0157] Furthermore, the traversing of all the meta information to determine the host allocation configuration information corresponding to each similar function includes:

[0158] The network meta information table, the host meta information table, the environment meta information table, the spacecraft meta information table, the task meta information table and the cluster meta information table are traversed to determine the host allocation configuration information corresponding to each similar function.

[0159] Figure 3 FIG. 1 is a schematic diagram of a process information acquisition device of a spacecraft ground measurement and control application software system provided by an embodiment of the present invention. Figure 3 As shown, the process information acquisition device of the spacecraft ground measurement and control application software system provided by the embodiment of the present invention includes a first acquisition unit 301 and a second acquisition unit 302, wherein:

[0160] The first acquisition unit 301 is used to acquire the process configuration information of a pre-configured spacecraft ground measurement and control application software system; wherein the process configuration information includes a cluster meta-information table, a process scheduling information table and a host allocation information table; the cluster meta-information table includes a cluster ID and a cluster name; the process scheduling information table includes a scheduling ID corresponding to each similar function, each scheduling ID corresponds to the process scheduling configuration information and the cluster ID to which it belongs; the host allocation information table includes at least one cluster ID corresponding to the host allocation ID, each host allocation ID corresponds to the host allocation configuration information; the second acquisition unit 302 is used to respond to a target process information query instruction triggered by the process configuration information, and execute the target process information query instruction to obtain a target process information query result.

[0161] Specifically, the first acquisition unit 301 in the device is used to obtain the process configuration information of a pre-configured spacecraft ground measurement and control application software system; wherein the process configuration information includes a cluster meta-information table, a process scheduling information table and a host allocation information table; the cluster meta-information table includes a cluster ID and a cluster name; the process scheduling information table includes a scheduling ID corresponding to each similar function, each scheduling ID corresponds to the process scheduling configuration information and the cluster ID to which it belongs; the host allocation information table includes at least one cluster ID corresponding to the host allocation ID, each host allocation ID corresponds to the host allocation configuration information; the second acquisition unit 302 is used to respond to a target process information query instruction triggered by the process configuration information, and execute the target process information query instruction to obtain a target process information query result.

[0162] The process information acquisition device of the spacecraft ground measurement and control application software system provided by the embodiment of the present invention acquires the process configuration information of the pre-configured spacecraft ground measurement and control application software system; wherein the process configuration information includes a cluster meta-information table, a process scheduling information table and a host allocation information table; the cluster meta-information table includes a cluster ID and a cluster name; the process scheduling information table includes a scheduling ID corresponding to each similar function one by one, each scheduling ID corresponds to the process scheduling configuration information and the cluster ID to which it belongs; the host allocation information table includes at least one cluster ID corresponding to the host allocation ID respectively, each host allocation ID corresponds to the host allocation configuration information; responds to a target process information query instruction triggered by the process configuration information, executes the target process information query instruction to obtain the target process information query result, and can conveniently and efficiently acquire the process information of the spacecraft ground measurement and control application software system.

[0163] The embodiment of the present invention provides an embodiment of a process information acquisition device of a spacecraft ground measurement and control application software system, which can be specifically used to execute the processing flow of the above-mentioned method embodiments. Its functions are not repeated here, and reference can be made to the detailed description of the above-mentioned method embodiments.

[0164] Figure 4 A schematic diagram of the physical structure of an electronic device provided in an embodiment of the present invention, such as Figure 4 As shown, the electronic device includes: a processor (processor) 401, a memory (memory) 402 and a bus 403;

[0165] The processor 401 and the memory 402 communicate with each other via a bus 403;

[0166] The processor 401 is used to call the program instructions in the memory 402 to execute the methods provided by the above method embodiments, for example, including:

[0167] Obtaining the process configuration information of the pre-configured spacecraft ground measurement and control application software system;

[0168] The process configuration information includes a cluster meta information table, a process scheduling information table and a host allocation information table; the cluster meta information table includes a cluster ID and a cluster name; the process scheduling information table includes a scheduling ID corresponding to each similar function, and each scheduling ID corresponds to the process scheduling configuration information and the cluster ID to which it belongs;

[0169] The host allocation information table includes at least one cluster ID corresponding to each host allocation ID, and each host allocation ID corresponds to host allocation configuration information;

[0170] In response to a target process information query instruction triggered by the process configuration information, the target process information query instruction is executed to obtain a target process information query result.

[0171] This embodiment discloses a computer program product, which includes a computer program stored on a non-transitory computer-readable storage medium. The computer program includes program instructions. When the program instructions are executed by a computer, the computer can perform the methods provided by the above method embodiments, for example, including:

[0172] Obtaining the process configuration information of the pre-configured spacecraft ground measurement and control application software system;

[0173] The process configuration information includes a cluster meta information table, a process scheduling information table and a host allocation information table; the cluster meta information table includes a cluster ID and a cluster name; the process scheduling information table includes a scheduling ID corresponding to each similar function, and each scheduling ID corresponds to the process scheduling configuration information and the cluster ID to which it belongs;

[0174] The host allocation information table includes at least one cluster ID corresponding to each host allocation ID, and each host allocation ID corresponds to host allocation configuration information;

[0175] In response to a target process information query instruction triggered by the process configuration information, the target process information query instruction is executed to obtain a target process information query result.

[0176] This embodiment provides a computer-readable storage medium, wherein the computer-readable storage medium stores a computer program, wherein the computer program enables the computer to execute the methods provided by the above method embodiments, for example, including:

[0177] Obtaining the process configuration information of the pre-configured spacecraft ground measurement and control application software system;

[0178] The process configuration information includes a cluster meta information table, a process scheduling information table and a host allocation information table; the cluster meta information table includes a cluster ID and a cluster name; the process scheduling information table includes a scheduling ID corresponding to each similar function, and each scheduling ID corresponds to the process scheduling configuration information and the cluster ID to which it belongs;

[0179] The host allocation information table includes at least one cluster ID corresponding to each host allocation ID, and each host allocation ID corresponds to host allocation configuration information;

[0180] In response to a target process information query instruction triggered by the process configuration information, the target process information query instruction is executed to obtain a target process information query result.

[0181] Those skilled in the art will appreciate that embodiments of the present invention may be provided as methods, systems, or computer program products. Therefore, the present invention may take the form of a complete hardware embodiment, a complete software embodiment, or an embodiment combining software and hardware. Moreover, the present invention may take the form of a computer program product implemented on one or more computer-usable storage media (including but not limited to disk storage, CD-ROM, optical storage, etc.) containing computer-usable program code.

[0182] The present invention is described with reference to flowcharts and / or block diagrams of methods, devices (systems), and computer program products according to embodiments of the present invention. It should be understood that each process and / or block in the flowchart and / or block diagram, as well as the combination of processes and / or blocks in the flowchart and / or block diagram, can be implemented by computer program instructions. These computer program instructions can be provided to a processor of a general-purpose computer, a special-purpose computer, an embedded processor, or other programmable data processing device to produce a machine, so that the instructions executed by the processor of the computer or other programmable data processing device generate instructions for implementing the processes in the flowchart and / or block diagram. Figure 1 A process or multiple processes and / or boxes Figure 1 A device that provides the functions specified in a block or multiple blocks.

[0183] These computer program instructions may also be stored in a computer-readable memory capable of directing a computer or other programmable data processing device to operate in a specific manner, so that the instructions stored in the computer-readable memory produce an article of manufacture comprising an instruction device, which implements the process Figure 1 A process or multiple processes and / or boxes Figure 1 A function specified in one or more boxes.

[0184] These computer program instructions can also be loaded onto a computer or other programmable data processing device so that a series of operating steps are executed on the computer or other programmable device to produce a computer-implemented process, thereby providing instructions for implementing the process. Figure 1 A process or multiple processes and / or boxes Figure 1 The steps for the functions specified in one or more boxes.

[0185] In the description of this specification, the description with reference to the terms "one embodiment", "a specific embodiment", "some embodiments", "for example", "example", "specific example", or "some examples" 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 present invention. In this specification, the schematic representation of the above terms does 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.

[0186] The specific embodiments described above further illustrate the objectives, technical solutions and beneficial effects of the present invention in detail. It should be understood that the above description is only a specific embodiment of the present invention and is not intended to limit the scope of protection of the present invention. Any modifications, equivalent substitutions, improvements, etc. made within the spirit and principles of the present invention should be included in the scope of protection of the present invention.

Claims

1. A method for obtaining process information of a spacecraft ground measurement and control application software system, characterized in that: include: Obtaining the process configuration information of the pre-configured spacecraft ground measurement and control application software system; The process configuration information includes a cluster meta information table, a process scheduling information table and a host allocation information table; the cluster meta information table includes a cluster ID and a cluster name; the process scheduling information table includes a scheduling ID corresponding to each similar function, and each scheduling ID corresponds to the process scheduling configuration information and the cluster ID to which it belongs; The host allocation information table includes at least one cluster ID corresponding to each host allocation ID, and each host allocation ID corresponds to host allocation configuration information; In response to a target process information query instruction triggered by the process configuration information, the target process information query instruction is executed to obtain a target process information query result.

2. The process information acquisition method of the spacecraft ground measurement and control application software system according to claim 1 is characterized in that: The step of obtaining the process configuration information of the pre-configured spacecraft ground measurement and control application software system includes: The process configuration information is displayed in a view display mode compiled by SQL statements.

3. The process information acquisition method of the spacecraft ground measurement and control application software system according to claim 2 is characterized in that: The responding to the target process information query instruction triggered by the process configuration information, executing the target process information query instruction to obtain the target process information query result, includes: In response to a trigger action executed by a user by browsing the process configuration information, a pre-compiled SQL statement is called to execute the target process information query instruction to obtain the target process information query result.

4. The process information acquisition method of the spacecraft ground measurement and control application software system according to any one of claims 1 to 3, characterized in that: Pre-configuring the process configuration information includes: Configure all meta information consisting of each type of meta information table; Among them, the metadata information stored in each type of metadata table does not change with the addition of new spacecraft missions; Cluster the spacecraft according to their mission function similarities, and obtain a dispatch ID that corresponds to each similar function. Traversing all the meta information to determine the progress scheduling configuration information corresponding to each similar function, establishing an association relationship between the progress scheduling configuration information and the scheduling ID, and obtaining the process scheduling information table; All the meta information is traversed to determine the host allocation configuration information corresponding to each similar function, and an association relationship between the host allocation configuration information and the host allocation ID that realizes the corresponding similar function is established to obtain the host allocation information table.

5. The process information acquisition method of the spacecraft ground measurement and control application software system according to claim 4 is characterized in that: The configuration consists of all meta information of each type of meta information table, including: Configure the network meta-information table, host meta-information table, environment meta-information table, spacecraft meta-information table, mission meta-information table, cluster meta-information table, and process meta-information table.

6. The process information acquisition method of the spacecraft ground measurement and control application software system according to claim 5 is characterized in that: The traversing all the meta information to determine the progress scheduling configuration information corresponding to each similar function includes: The cluster meta information table and the process meta information table are traversed to determine the progress scheduling configuration information corresponding to each similar function.

7. The process information acquisition method of the spacecraft ground measurement and control application software system according to claim 5 is characterized in that: The traversing of all the meta information to determine the host allocation configuration information corresponding to each similar function includes: The network meta information table, the host meta information table, the environment meta information table, the spacecraft meta information table, the task meta information table and the cluster meta information table are traversed to determine the host allocation configuration information corresponding to each similar function.

8. A process information acquisition device for a spacecraft ground measurement and control application software system, characterized in that: include: A first acquisition unit is used to acquire process configuration information of a pre-configured spacecraft ground measurement and control application software system; The process configuration information includes a cluster meta information table, a process scheduling information table and a host allocation information table; the cluster meta information table includes a cluster ID and a cluster name; the process scheduling information table includes a scheduling ID corresponding to each similar function, and each scheduling ID corresponds to the process scheduling configuration information and the cluster ID to which it belongs; The host allocation information table includes at least one cluster ID corresponding to each host allocation ID, and each host allocation ID corresponds to host allocation configuration information; The second acquisition unit is used to respond to the target process information query instruction triggered by the process configuration information, and execute the target process information query instruction to obtain the target process information query result.

9. An electronic device comprising a memory, a processor, and a computer program stored in the memory and executable on the processor, characterized in that: When the processor executes the computer program, the steps of the method according to any one of claims 1 to 7 are implemented.

10. A 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 method according to any one of claims 1 to 7 are implemented.

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