CN114626145A - Data collaborative management method, device, equipment and medium - Google Patents
Data collaborative management method, device, equipment and medium Download PDFInfo
- Publication number
- CN114626145A CN114626145A CN202210279118.7A CN202210279118A CN114626145A CN 114626145 A CN114626145 A CN 114626145A CN 202210279118 A CN202210279118 A CN 202210279118A CN 114626145 A CN114626145 A CN 114626145A
- Authority
- CN
- China
- Prior art keywords
- node
- carrier rocket
- management
- data
- working
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
Images
Classifications
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F30/00—Computer-aided design [CAD]
- G06F30/10—Geometric CAD
- G06F30/15—Vehicle, aircraft or watercraft design
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06Q—INFORMATION AND COMMUNICATION TECHNOLOGY [ICT] SPECIALLY ADAPTED FOR ADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL OR SUPERVISORY PURPOSES; SYSTEMS OR METHODS SPECIALLY ADAPTED FOR ADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL OR SUPERVISORY PURPOSES, NOT OTHERWISE PROVIDED FOR
- G06Q10/00—Administration; Management
- G06Q10/10—Office automation; Time management
- G06Q10/103—Workflow collaboration or project management
Abstract
The invention discloses a data collaborative management method, a device, equipment and a medium, wherein the method comprises the following steps: determining each working node in the development of the carrier rocket, wherein the working node is used for indicating one node task in the development of the carrier rocket; configuring a parameter relation related to each working node according to the research and development requirements of the carrier rocket; and performing cooperative management on each professional data in the carrier rocket according to each configured parameter relationship. By adopting the method and the system, the rapid and accurate collaborative management of each professional data in the carrier rocket can be realized.
Description
Technical Field
The invention relates to the technical field of spaceflight, in particular to a data collaborative management method, a data collaborative management device, data collaborative management equipment and a data collaborative management medium.
Background
The carrier rocket development is a complex system engineering, is a multidisciplinary and multi-level design/simulation tightly-coupled collaborative development process, and has the characteristics of multidisciplinary, hierarchical, distributivity and cooperativity in the collaborative design/simulation process.
In the traditional carrier rocket development process, each specialty transmits data based on texts, and the specialty cooperation degree is poor. In a complex collaborative design process, a downstream professional node (also referred to as a node for short) needs to wait for the design output of an upstream professional node, so that in the step-by-step waiting process, the whole project period is easily influenced by the design work delay of a certain node. And project management personnel can not know the project progress in real time and can not take measures in time. Therefore, in the multi-specialty (data) collaborative design process of the launch vehicle, it is necessary to propose a better management scheme.
Disclosure of Invention
The embodiment of the application provides a data collaborative management method, a data collaborative management device and a data collaborative management medium, and can realize rapid and accurate collaborative management of each professional data in a carrier rocket.
In one aspect, an embodiment of the present application provides a data collaborative management method, where the method includes:
determining each working node in the development of the carrier rocket, wherein the working node is used for indicating one node task in the development of the carrier rocket;
configuring a parameter relation related to each working node according to the research and development requirements of the carrier rocket;
and performing cooperative management on each professional data in the carrier rocket according to each configured parameter relationship.
Optionally, before configuring the parameter relationship related to each working node according to the development requirement of the launch vehicle, the method further includes:
designing a corresponding application program according to the research and development service of the carrier rocket, and uploading the application program to a shared library;
configuring parameter relationships associated with each of the working nodes according to the development requirements of the launch vehicle comprises:
and configuring the input-output relationship of each working node according to the research and development requirements of the carrier rocket, and configuring the incidence relationship between each working node and the shared library.
Optionally, before the collaborative management of the professional data in the launch vehicle according to the configured parameter relationships, the method further includes:
configuring corresponding management information in each working node;
the cooperative management of the professional data in the launch vehicle according to the configured parameter relationships comprises:
and performing cooperative management on each professional data in the carrier rocket according to each configured parameter relationship and the management information configured in each working node.
Optionally, the performing collaborative management on each piece of professional data in the launch vehicle according to each configured parameter relationship and the management information configured in each working node includes:
starting the research and development of the carrier rocket, and generating a corresponding project schedule according to the configured parameter relationships and the management information configured in the working nodes;
and executing node tasks corresponding to the working nodes according to the service sequence of the working nodes so as to perform cooperative management on each professional data in the carrier rocket.
Optionally, the method further comprises:
and marking and displaying a first color of a currently executed target working node, and marking and displaying a second color of other working nodes except the target working node, wherein the first color is different from the second color.
Optionally, after the collaborative management of the professional data in the launch vehicle, the method further includes:
and generating a corresponding result database according to the result data obtained after the cooperative management.
Optionally, the method further comprises:
and when a downstream node in each working node has data errors, returning to a previous node corresponding to the downstream node, and re-executing a node task corresponding to the previous node.
In another aspect, an embodiment of the present application provides a data cooperation management apparatus, where the apparatus includes: the device comprises a determining module, a configuration module and a management module, wherein:
the determining module is used for determining each working node in the research and development of the carrier rocket, and the working node is used for indicating one node task in the research and development of the carrier rocket;
the configuration module is used for configuring parameter relationships related to the working nodes according to the research and development requirements of the carrier rocket;
and the management module is used for performing cooperative management on each professional data in the carrier rocket according to each configured parameter relationship.
For the content that is not introduced or described in the embodiments of the present application, reference may be made to the related descriptions in the foregoing method embodiments, and details are not repeated here.
On the other hand, the present application provides a terminal device according to an embodiment of the present application, where the terminal device includes: a processor, a memory, a communication interface, and a bus; the processor, the memory and the communication interface are connected through the bus and complete mutual communication; the memory stores executable program code; the processor runs a program corresponding to the executable program code by reading the executable program code stored in the memory, for executing the data cooperation management method as described above.
On the other hand, the present application provides a computer-readable storage medium storing a program that executes the data cooperation management method described above when the program runs on a terminal device, through an embodiment of the present application.
One or more technical solutions provided in the embodiments of the present application have at least the following technical effects or advantages: determining each working node in the development of a carrier rocket, wherein the working node is used for indicating a node task in the development of the carrier rocket; configuring a parameter relation related to each working node according to the research and development requirements of the carrier rocket; and performing cooperative management on each professional data in the carrier rocket according to each configured parameter relationship. In the scheme, the cooperative management of the professional data in the carrier rocket is realized by configuring the parameter relation related to each working node in the carrier rocket research and development process, so that the technical problems that the project period is influenced and the project progress cannot be known due to gradual waiting in the prior art are solved, and the convenience and the high efficiency of the cooperative management of the professional data are realized.
Drawings
In order to more clearly illustrate the technical solutions in the embodiments of the present invention, the drawings needed to be used in the description of the embodiments are briefly introduced below, and it is obvious that the drawings in the following description are some embodiments of the present invention, and it is obvious for those skilled in the art to obtain other drawings based on the drawings without creative efforts.
Fig. 1 is a schematic flowchart of a data collaborative management method according to an embodiment of the present application.
Fig. 2 is a schematic diagram of a possible launch vehicle development process provided in an embodiment of the present application.
Fig. 3 is a schematic diagram of a possible parameter input-output relationship configuration provided in an embodiment of the present application.
Fig. 4 is a schematic diagram of a possible association relationship configuration provided in an embodiment of the present application.
Fig. 5 is a schematic diagram of one possible application provided in an embodiment of the present application.
Fig. 6 is a schematic diagram of a node initiating a commit task according to an embodiment of the present application.
Fig. 7 is a schematic diagram of an error of a downstream node according to an embodiment of the present application.
Fig. 8 is a schematic diagram of a possible downstream node fallback provided in an embodiment of the present application.
Fig. 9 is a schematic diagram of a possible project schedule provided in an embodiment of the present application.
FIG. 10 is a diagram of a possible results database provided by an embodiment of the present application.
Fig. 11 is a schematic structural diagram of a data cooperation management apparatus according to an embodiment of the present application.
Fig. 12 is a schematic structural diagram of a terminal device according to an embodiment of the present application.
Detailed Description
The embodiment of the application provides a data collaborative management method, device, equipment and medium, and solves the technical problems that in the prior art, the project period is influenced and the project progress cannot be known due to gradual waiting.
In order to solve the technical problems, the general idea of the embodiment of the application is as follows: determining each working node in the development of the carrier rocket, wherein the working node is used for indicating one node task in the development of the carrier rocket; configuring a parameter relation related to each working node according to the research and development requirements of the carrier rocket; and performing cooperative management on each professional data in the carrier rocket according to each configured parameter relationship.
In order to better understand the technical scheme, the technical scheme is described in detail in the following with reference to the attached drawings of the specification and specific embodiments.
First, it is stated that the term "and/or" appearing herein is merely one type of associative relationship that describes an associated object, meaning that three types of relationships may exist, e.g., a and/or B may mean: a exists alone, A and B exist simultaneously, and B exists alone. In addition, the character "/" herein generally indicates that the former and latter associated objects are in an "or" relationship.
Fig. 1 is a schematic flow chart of a data collaborative management method according to an embodiment of the present application. The method as shown in fig. 1 comprises the following implementation steps:
s101, determining each working node in the research and development of the carrier rocket, wherein the working node is used for indicating one node task in the research and development of the carrier rocket.
The work node can refer to a node task corresponding to one design work in a carrier rocket research and development process.
In an Integrated Development Environment (IDE) platform, the application may complete the design and Development of an application program (APP) according to the overall design Development of a launch vehicle (specifically, may be based on the actual design service of Development, which is simply referred to as Development service), and optionally may also combine with the knowledge accumulation of each specialty itself. Parameterization of input data is realized in the APP, and the developed application program APP is uploaded to a shared (data) base.
The design process can be set up in an object center (Teamcenter) system according to carrier rocket research and development (process), wherein each work node in the process corresponds to one design work. For example, please refer to fig. 2, which shows a schematic diagram of a possible launch vehicle development process. As can be seen in fig. 2, the launch vehicle overall development process includes, but is not limited to, at least one of the following nodes such as: the method comprises the steps of overall original data input, mass distribution and shape and quality parameter calculation, standard trajectory calculation, pneumatic calculation, load calculation, shaking calculation, elastic motion equation coefficient calculation, small disturbance parameter calculation, stability margin calculation, six-degree-of-freedom calculation and other design work nodes.
S102, configuring parameter relations related to the working nodes according to the research and development requirements of the carrier rocket, wherein the parameter relations comprise input and output relations of the working nodes, incidence relations between the working nodes and a shared library and the like.
According to the method and the device, the design content of the node task of each working node can be preliminarily determined by analyzing the research and development requirements of the carrier rocket, so that interface definition under the corresponding node is completed, and corresponding professional parameters are selected. And then configuring the parameter input-output relationship of each working node based on the unified parameters to form a complete carrier rocket overall design process. Furthermore, the method and the device can also configure the incidence relation between each working node and a shared library (specifically, research and development design programs, tool software and the like of the APP in the shared library), realize the integration between design tasks and design tools, namely realize the integration between the node tasks corresponding to each working node and the APP of the application program, and form a knowledge-driven research and development design working mode.
For example, please refer to fig. 3 and fig. 4, which are schematic diagrams illustrating a possible parameter input/output relationship configuration and an association relationship configuration, respectively. As shown in fig. 3, the general development process of the launch vehicle described in the present application needs to involve task configuration under nodes such as mass allocation and form and quality parameter calculation. As shown in fig. 4, the left small box represents each parameter in the launch vehicle development process, and the right small box represents each parameter in the application, and the application needs to configure the input-output relationship between them, for example, input the parameters with the same parameter name from the launch vehicle development process to the application, and so on.
Referring also to fig. 5, a schematic diagram of one possible application is shown. As shown in fig. 5, the application may utilize an application program to implement collaborative management of multi-specialty data in a launch vehicle, for example, to open the application program shown in fig. 5, and the display interface corresponding to the mass distribution and shape and quality parameter calculation node may include, but is not limited to, parameter data of devices such as an instrument bay, a front transition section, an oxygen box, and the like.
S103, performing cooperative management on each professional data in the carrier rocket according to each configured parameter relationship.
The method and the system for managing the working nodes of the mobile terminal can configure corresponding management information in each working node in advance, wherein the management information can be information configured by a system in a self-defined mode and can include but is not limited to information such as personnel arrangement, time arrangement and the like of a research and development task at this time corresponding to the working nodes. For example, designers corresponding to different specialties are selected under each working node, and task completion deadline is set.
Further, the method can start the overall research and development (process) of the carrier rocket according to research and development requirements, and then the system automatically generates a complete project schedule, specifically, the method can automatically generate a corresponding project schedule according to the configured parameter relationships and the configured management information under the working nodes. For example, please refer to FIG. 9, which illustrates a schematic diagram of a possible project schedule. The project schedule shown in fig. 9 includes progress information of the respective work nodes and the like. Further, the method and the device can asynchronously execute the node tasks corresponding to the working nodes according to the execution sequence of the working nodes so as to cooperatively manage the professional data in the carrier rocket.
In the execution process, the method and the device can mark and display a target working node which is currently executed in a first color, and mark and display other working nodes except the target working node in a second color, wherein the first color and the second color are different. For example, the currently executing work node (e.g., the overall original input parameters) may be displayed as "green", the remaining work nodes may be displayed as "orange-yellow", and so on.
In the general design process of the carrier rocket, the application program can be started, and operations such as data downloading, application program application and data uploading are completed in the application program. Before the application program is applied, the application program can be adaptively modified according to actual design task work so as to conveniently complete the design work. After determining that each professional data is correct in the application program, the application can select corresponding working nodes, such as 'A mass distribution and form and mass parameter calculation', 'aerodynamic force calculation data post-processing', 'turning load calculation', 'aerodynamic load calculation data post-processing', and submit corresponding node tasks, so that the node tasks corresponding to the working nodes are completed. The present application may also mark the currently executed working node as "green", and mark the remaining working nodes (i.e., their downstream working nodes, simply referred to as downstream nodes) as "orange yellow".
For example, please refer to FIG. 6, which illustrates a schematic diagram of a possible node-initiated commit task. As shown in fig. 6, in the application, each working node required to be used by the original input parameter can be selected in an interface of an application program, and a node task corresponding to each working node is submitted.
In an optional embodiment, when detecting that any downstream node in the working nodes has a data error, the application may initiate a rollback operation to a previous (working) node corresponding to the downstream node, and re-execute a node task corresponding to the previous node. For example, please refer to fig. 7 and 8, which illustrate a schematic diagram of a possible downstream node error and rollback. As shown in fig. 7 and 8, when detecting that the node "C overall form and quality parameter calculation" finds that there is a fault in the data, the present application may automatically initiate a rollback operation flow to rollback the node task to the node "a quality allocation and form and quality parameter calculation". After the rollback is finished, the color of the node of the C overall form and quality parameter calculation is changed into purple, the color of the node of the A quality distribution and form and quality parameter calculation is changed into orange yellow, the color of the downstream node (the A quality distribution and the form and quality parameter calculation) related to the node is correspondingly changed, and the task state of the corresponding node is also changed simultaneously.
All research and development design works of carrier rocket overall research and development are completed in sequence based on the unified parameter pool. After the entire design work is completed, the data will form a corresponding result database. In other words, the present application may generate a corresponding result database according to the result data obtained after the collaborative management. Optionally, after each designer of the application finishes submitting all node tasks, the project progress is updated in real time, so that project managers can conveniently know the project progress. For example, please refer to FIG. 10, which shows a schematic diagram of a possible results database. The result database may include, but is not limited to, information such as professional data, intermediate result data calculated, and final result data involved in the launch vehicle development process, for example, the result database shown in fig. 10 includes information such as oxygen liquid flow, oxygen liquid _ minimum air pillow volume, and oxygen liquid _ maximum filling volume.
By implementing the method, each working node in the research and development of the carrier rocket is determined, and the working node is used for indicating one node task in the research and development of the carrier rocket; configuring a parameter relation related to each working node according to the research and development requirements of the carrier rocket; and performing cooperative management on each professional data in the carrier rocket according to each configured parameter relationship. In the scheme, the cooperative management of the professional data in the carrier rocket is realized by configuring the parameter relation related to each working node in the carrier rocket research and development process, so that the technical problems that the project period is influenced and the project progress cannot be known due to gradual waiting in the prior art are solved, and the convenience and the high efficiency of the cooperative management of the professional data are realized.
Based on the same inventive concept, another embodiment of the present application provides a device and a terminal device corresponding to the method for implementing collaborative data management in the embodiment of the present application.
Fig. 11 is a schematic structural diagram of a data collaboration management apparatus according to an embodiment of the present disclosure. The apparatus 20 shown in fig. 11 comprises: a determination module 201, a configuration module 202, and a management module 203, wherein:
the determining module 201 is configured to determine each working node in the development of a launch vehicle, where the working node is used to instruct a node task in the development of the launch vehicle;
the configuration module 202 is configured to configure a parameter relationship related to each working node according to a research and development requirement of the launch vehicle;
the management module 203 is configured to perform collaborative management on each piece of professional data in the launch vehicle according to each configured parameter relationship.
Optionally, the apparatus further comprises a processing module 204, wherein:
the processing module 204 is configured to design a corresponding application program according to the research and development service of the launch vehicle, and upload the application program to a shared library;
the configuration module 202 is specifically configured to configure the input/output relationship of each working node according to the research and development requirements of the launch vehicle, and configure the association relationship between each working node and the shared library.
Optionally, the processing module 204 is further configured to configure corresponding management information in each working node;
the management module 203 is specifically configured to perform cooperative management on each professional data in the launch vehicle according to each configured parameter relationship and the management information configured in each working node.
Optionally, the management module 203 is specifically configured to:
starting the research and development of the carrier rocket, and generating a corresponding project schedule according to the configured parameter relationships and the management information configured in the working nodes;
and executing node tasks corresponding to the working nodes according to the service sequence of the working nodes so as to perform cooperative management on each professional data in the carrier rocket.
Optionally, the processing module 204 is further configured to:
and marking and displaying a first color of a currently executed target working node, and marking and displaying a second color of other working nodes except the target working node, wherein the first color is different from the second color.
Optionally, the processing module 204 is further configured to:
and generating a corresponding result database according to the result data obtained after the cooperative management.
Optionally, the processing module 204 is further configured to:
and when a downstream node in each working node has data errors, returning to a previous node corresponding to the downstream node, and re-executing a node task corresponding to the previous node.
Please refer to fig. 12, which is a schematic structural diagram of a terminal device according to an embodiment of the present application. The terminal device 30 shown in fig. 12 includes: at least one processor 301, a communication interface 302, a user interface 303, and a memory 304, wherein the processor 301, the communication interface 302, the user interface 303, and the memory 304 may be connected by a bus or by other means, and the embodiment of the present invention is exemplified by being connected by the bus 305. Wherein the content of the first and second substances,
The communication interface 302 may be a wired interface (e.g., an ethernet interface) or a wireless interface (e.g., a cellular network interface or using a wireless local area network interface) for communicating with other terminals or websites. In the embodiment of the present invention, the communication interface 302 is specifically configured to obtain corresponding information in a research and development process of a launch vehicle.
The user interface 303 may specifically be a touch panel, including a touch screen and a touch screen, for detecting an operation instruction on the touch panel, and the user interface 303 may also be a physical button or a mouse. The user interface 303 may also be a display screen for outputting, displaying images or data.
The Memory 304 may include Volatile Memory (Volatile Memory), such as Random Access Memory (RAM); the Memory may also include a Non-Volatile Memory (Non-Volatile Memory), such as a Read-Only Memory (ROM), a Flash Memory (Flash Memory), a Hard Disk (Hard Disk Drive, HDD), or a Solid-State Drive (SSD); the memory 304 may also comprise a combination of the above-described types of memory. The memory 304 is used for storing a set of program codes, and the processor 301 is used for calling the program codes stored in the memory 304 and executing the following operations:
determining each working node in the development of the carrier rocket, wherein the working node is used for indicating one node task in the development of the carrier rocket;
configuring a parameter relation related to each working node according to the research and development requirements of the carrier rocket;
and performing cooperative management on each professional data in the carrier rocket according to each configured parameter relationship.
Optionally, before configuring the parameter relationship associated with each working node according to the development requirement of the launch vehicle, the processor 301 is further configured to:
designing a corresponding application program according to the research and development service of the carrier rocket, and uploading the application program to a shared library;
configuring parameter relationships associated with each of the working nodes according to the development requirements of the launch vehicle comprises:
and configuring the input-output relationship of each working node according to the research and development requirements of the carrier rocket, and configuring the incidence relationship between each working node and the shared library.
Optionally, before the cooperative management of the professional data in the launch vehicle according to the configured parameter relationships, the processor 301 is further configured to:
configuring corresponding management information in each working node;
the cooperative management of the professional data in the launch vehicle according to the configured parameter relationships comprises:
and performing cooperative management on each professional data in the carrier rocket according to each configured parameter relation and the management information configured in each working node.
Optionally, the performing collaborative management on each professional data in the launch vehicle according to each configured parameter relationship and the management information configured in each working node includes:
starting the research and development of the carrier rocket, and generating a corresponding project schedule according to the configured parameter relationships and the management information configured in the working nodes;
and executing node tasks corresponding to the working nodes according to the service sequence of the working nodes so as to perform cooperative management on each professional data in the carrier rocket.
Optionally, the processor 301 is further configured to:
and marking and displaying a first color of a currently executed target working node, and marking and displaying a second color of other working nodes except the target working node, wherein the first color is different from the second color.
Optionally, after the cooperative management of the professional data in the launch vehicle, the processor 301 is further configured to:
and generating a corresponding result database according to the result data obtained after the cooperative management.
Optionally, the processor 301 is further configured to:
and when a downstream node in each working node has data errors, returning to a previous node corresponding to the downstream node, and re-executing a node task corresponding to the previous node.
Since the terminal device described in this embodiment is a terminal device used for implementing the method in this embodiment, based on the method described in this embodiment, a person skilled in the art can understand the specific implementation manner of the terminal device in this embodiment and various variations thereof, so that a detailed description of how to implement the method in this embodiment by the terminal device is omitted here. The terminal device adopted by a person skilled in the art to implement the method in the embodiment of the present application is within the scope of the protection intended by the present application.
One or more technical solutions provided in the embodiments of the present application have at least the following technical effects or advantages: determining each working node in the development of a carrier rocket, wherein the working node is used for indicating a node task in the development of the carrier rocket; configuring a parameter relation related to each working node according to the research and development requirements of the carrier rocket; and performing cooperative management on each professional data in the carrier rocket according to each configured parameter relationship. In the scheme, the cooperative management of the professional data in the carrier rocket is realized by configuring the parameter relation related to each working node in the carrier rocket research and development process, so that the technical problems that the project period is influenced and the project progress cannot be known due to gradual waiting in the prior art are solved, and the convenience and the high efficiency of the cooperative management of the professional data are realized.
As will be appreciated by one skilled in the art, embodiments of the present invention may be provided as a method, system, or computer program product. Accordingly, the present invention may take the form of an entirely hardware embodiment, an entirely software embodiment or an embodiment combining software and hardware aspects. Furthermore, the present invention may take the form of a computer program product embodied on one or more computer-usable storage media (including, but not limited to, disk storage, CD-ROM, optical storage, and the like) having computer-usable program code embodied therein.
The present invention is described with reference to flowchart illustrations and/or block diagrams of methods, apparatus (systems), and computer program products according to embodiments of the invention. It will be understood that each flow and/or block of the flow diagrams and/or block diagrams, and combinations of flows and/or blocks in the flow diagrams and/or block diagrams, can be implemented by computer program instructions. These computer program instructions may be provided to a processor of a general purpose computer, special purpose computer, embedded processor, or other programmable data processing apparatus to produce a machine, such that the instructions, which execute via the processor of the computer or other programmable data processing apparatus, create means for implementing the functions specified in the flowchart flow or flows and/or block diagram block or blocks.
These computer program instructions may also be stored in a computer-readable memory that can direct a computer or other programmable data processing apparatus to function in a particular manner, such that the instructions stored in the computer-readable memory produce an article of manufacture including instruction means which implement the function specified in the flowchart flow or flows and/or block diagram block or blocks.
These computer program instructions may also be loaded onto a computer or other programmable data processing apparatus to cause a series of operational steps to be performed on the computer or other programmable apparatus to produce a computer implemented process such that the instructions which execute on the computer or other programmable apparatus provide steps for implementing the functions specified in the flowchart flow or flows and/or block diagram block or blocks.
While preferred embodiments of the present invention have been described, additional variations and modifications in those embodiments may occur to those skilled in the art once they learn of the basic inventive concepts. Therefore, it is intended that the appended claims be interpreted as including the preferred embodiment and all changes and modifications that fall within the scope of the invention.
It will be apparent to those skilled in the art that various changes and modifications may be made in the present invention without departing from the spirit and scope of the invention. Thus, if such modifications and variations of the present invention fall within the scope of the claims of the present invention and their equivalents, the present invention is also intended to include such modifications and variations.
Claims (10)
1. A data collaborative management method is characterized by comprising the following steps:
determining each working node in the development of the carrier rocket, wherein the working node is used for indicating one node task in the development of the carrier rocket;
configuring a parameter relation related to each working node according to the research and development requirements of the carrier rocket;
and performing cooperative management on each professional data in the carrier rocket according to each configured parameter relationship.
2. The method of claim 1, wherein prior to configuring the parametric relationships associated with each of the working nodes based on the development requirements of the launch vehicle, the method further comprises:
designing a corresponding application program according to the research and development service of the carrier rocket, and uploading the application program to a shared library;
configuring parameter relationships associated with each of the working nodes according to the development requirements of the launch vehicle comprises:
and configuring the input-output relationship of each working node according to the research and development requirements of the carrier rocket, and configuring the incidence relationship between each working node and the shared library.
3. The method of claim 1, wherein before cooperatively managing the specialized data in the launch vehicle according to the configured parameter relationships, the method further comprises:
configuring corresponding management information in each working node;
the cooperative management of the professional data in the launch vehicle according to the configured parameter relationships comprises:
and performing cooperative management on each professional data in the carrier rocket according to each configured parameter relationship and the management information configured in each working node.
4. The method according to claim 3, wherein the cooperatively managing the professional data in the launch vehicle according to the configured parameter relationships and the management information configured in the working nodes comprises:
starting the research and development of the carrier rocket, and generating a corresponding project schedule according to the configured parameter relationships and the management information configured in the working nodes;
and executing node tasks corresponding to the working nodes according to the service sequence of the working nodes so as to perform cooperative management on each professional data in the carrier rocket.
5. The method of claim 4, further comprising:
and marking and displaying a first color of a currently executed target working node, and marking and displaying a second color of other working nodes except the target working node, wherein the first color is different from the second color.
6. The method of claim 4, wherein after the coordinated management of the specialized data in the launch vehicle, the method further comprises:
and generating a corresponding result database according to the result data obtained after the cooperative management.
7. The method according to any one of claims 1-6, further comprising:
and when a downstream node in each working node has data errors, returning to a previous node corresponding to the downstream node, and re-executing a node task corresponding to the previous node.
8. A data cooperation management apparatus, characterized in that the apparatus comprises: the device comprises a determining module, a configuration module and a management module, wherein:
the determining module is used for determining each working node in the research and development of the carrier rocket, and the working node is used for indicating one node task in the research and development of the carrier rocket;
the configuration module is used for configuring parameter relationships related to the working nodes according to the research and development requirements of the carrier rocket;
and the management module is used for performing cooperative management on each professional data in the carrier rocket according to each configured parameter relationship.
9. A terminal device, characterized in that the terminal device comprises: a processor, a memory, a communication interface, and a bus; the processor, the memory and the communication interface are connected through the bus and complete mutual communication; the memory stores executable program code; the processor executes a program corresponding to the executable program code by reading the executable program code stored in the memory, for executing the data collaborative management method according to any one of claims 1 to 7.
10. A computer-readable storage medium characterized by storing a program that executes the data cooperation management method according to any one of claims 1 to 7 when the program is run on a terminal device.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202210279118.7A CN114626145A (en) | 2022-03-21 | 2022-03-21 | Data collaborative management method, device, equipment and medium |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202210279118.7A CN114626145A (en) | 2022-03-21 | 2022-03-21 | Data collaborative management method, device, equipment and medium |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN114626145A true CN114626145A (en) | 2022-06-14 |
Family
ID=81904836
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202210279118.7A Pending CN114626145A (en) | 2022-03-21 | 2022-03-21 | Data collaborative management method, device, equipment and medium |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN114626145A (en) |
-
2022
- 2022-03-21 CN CN202210279118.7A patent/CN114626145A/en active Pending
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US9754059B2 (en) | Graphical design verification environment generator | |
| JP4464665B2 (en) | High speed chip management system | |
| JP6122621B2 (en) | Simulation and visualization of project planning and management | |
| US11922101B2 (en) | Integrated circuits as a service | |
| US10885002B2 (en) | Recipe management system | |
| US20170139685A1 (en) | Visual software modeling method to construct software views based on a software meta view | |
| JP6600011B2 (en) | Efficient waveform generation for emulation | |
| CN106066899A (en) | The method and system of the architectural characteristic of simulating reinforced concrete in finite element analysis | |
| CN112148276A (en) | Visual programming for deep learning | |
| CN113919158A (en) | Simulation method and device for flight control panel and storage medium | |
| CN108228965B (en) | Simulation verification method, device and equipment for memory cell | |
| US8024158B2 (en) | Management system and management method of CAD data used for a structural analysis | |
| Werner et al. | Cloud-based remote virtual prototyping platform for embedded control applications: Cloud-based infrastructure for large-scale embedded hardware-related programming laboratories | |
| CN114626145A (en) | Data collaborative management method, device, equipment and medium | |
| Júlvez et al. | MATLAB tools for the analysis of Petri net models | |
| CN112764742A (en) | Data processing method and device | |
| Dhiman | Reassessment of Software Development Life Cycle Models | |
| CN114154249A (en) | Rocket parameter management method, device, terminal equipment and medium | |
| Caron | Leveraging tradeoff, bridging the gap among disciplines | |
| US20140196002A1 (en) | Tool and method thereof for efficient design of information technology systems | |
| CN114021259A (en) | Quality control method, system, medium and terminal of piping professional model | |
| CN117882050A (en) | Method and system for generating engineering program compatible with specific engineering environment | |
| CN113805873A (en) | Codeless workflow definition method, terminal device and computer-readable storage medium | |
| O'Connor | Horizon: A system modeling and simulation framework for systems engineering utility analysis | |
| CN112947921A (en) | Method, device, equipment and storage medium for rapidly building CRUD page |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination |