CN116108695A - Arrow ground interface virtual verification method, device and medium for operation posts - Google Patents
Arrow ground interface virtual verification method, device and medium for operation posts Download PDFInfo
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Abstract
The invention discloses an arrow ground interface virtual verification method, device and medium for an operation post. The method comprises the following steps: constructing three-dimensional digital virtual environments of different launching field technical states in ground launch testing tasks of a carrier rocket; performing post personnel and equipment operation in a three-dimensional digital virtual environment according to arrow ground interface operation requirements of different launching field technical states; after the operation of post personnel and equipment is finished, qualitative indexes and quantitative indexes generated by the operation of different technical states of the transmitting field are output; and determining the feasibility conclusion of the arrow ground interface operation according to the qualitative index and the quantitative index. The method realizes the organic unification of mutual matching of technical states and related operation activities among rocket systems, spacecraft systems and launching field systems, and can find problems in advance and avoid hidden danger when being applied to novel carrier rockets in the design and research and development stages.
Description
Technical Field
The invention relates to the technical field of rocket launching, in particular to an operation-post-oriented rocket ground interface virtual verification method, device and medium.
Background
The existing rocket ground interface verification method facing the post operation is that after rocket and spacecraft are produced by rocket and spacecraft manufacturers, rough prototype experiments are carried out on interfaces required by the rocket and spacecraft in a system environment without a launch field. At present, CN111710209A proposes a model rocket demonstration system and a demonstration method thereof, but does not propose the content of rocket ground interface verification, and the rocket ground interface verification at present mainly relies on rocket and spacecraft objects, previews the rocket and spacecraft before shooting and under test in an ideal state, simulates various joint operation conditions of the interfaces before shooting and under test, and evaluates required resources and matching conditions under different technical states. Considering that new generation carrier rockets in China are all in a three-vertical test mode, namely vertical hoisting, vertical transferring and vertical testing, various operation interfaces of rockets and spacecrafts in the task process are at the height of tens of meters, so that rocket manufacturers cannot completely restore the real task scene state under the support of a system without a launch field. Therefore, the technical problems that the novel rocket and the spacecraft are in the design construction stage in the research and development production process, the real task site cannot be simulated, interface mismatch, interference and the like occur when the novel rocket and the novel launching site system are first-time synthesized, and the novel rocket synthesis and first-flight success can be influenced when the problems are serious.
Disclosure of Invention
Aiming at the defects of the prior art, the invention provides an arrow ground interface virtual verification method, an arrow ground interface virtual verification device and a arrow ground interface virtual verification medium for operation posts.
According to one aspect of the invention, there is provided an arrow ground interface virtual verification method facing an operation post, comprising:
constructing three-dimensional digital virtual environments of different launching field technical states in ground launch testing tasks of a carrier rocket;
performing post personnel and equipment operation in a three-dimensional digital virtual environment according to arrow ground interface operation requirements of different launching field technical states;
after the operation of post personnel and equipment is finished, qualitative indexes and quantitative indexes generated by the operation of different technical states of the transmitting field are output;
and determining the feasibility conclusion of the arrow ground interface operation according to the qualitative index and the quantitative index.
Optionally, the operation of constructing three-dimensional digital virtual environments of different launch field technical states in the ground launch testing task of the carrier rocket comprises the following steps:
classifying equipment models in ground survey and launch tasks of the carrier rocket, and determining resource categories of the equipment models;
according to the resource category of the equipment model, simplifying the equipment model;
developing a detail level assembly of the simplified equipment model by using a unit 3D visual driving engine, and determining the detail level assembly models of the rocket, the spacecraft and the launching field system;
constructing three-dimensional digital models of the rocket, the spacecraft and the detail level assembly model of the launching field system according to different preset launching field technical states, and constructing three-dimensional digital virtual environments of different launching field technical states, wherein the three-dimensional digital virtual environments comprise a vertical hoisting three-dimensional digital virtual environment, a test three-dimensional digital virtual environment and a launching three-dimensional digital virtual environment.
Optionally, the resource categories include: the simple model can be directly used for substitution, the internal structure of the model can be deleted, and the surface number can be optimized only.
Optionally, the method further comprises: establishing a quantitative index model and a qualitative index model of post personnel and equipment operation according to monomers of a ground launch testing task of the carrier rocket, wherein the monomers comprise:
launch vehicle, launching tower, movable launching platform, work platform, frock, opening and virtual post personage.
According to another aspect of the present invention, there is provided an arrow ground interface virtual verification apparatus facing an operation post, including:
the construction module is used for constructing three-dimensional digital virtual environments of different launching field technical states in ground launch testing tasks of the carrier rocket;
the operation module is used for operating post personnel and equipment in a three-dimensional digital virtual environment according to arrow ground interface operation requirements of different launching field technical states;
the output module is used for outputting qualitative indexes and quantitative indexes generated by operation of different technical states of the transmitting field after the operation of post personnel and equipment is finished;
and the determining module is used for determining the feasibility conclusion of the arrow ground interface operation according to the qualitative index and the quantitative index.
According to a further aspect of the present invention there is provided a computer readable storage medium storing a computer program for performing the method according to any one of the above aspects of the present invention.
According to still another aspect of the present invention, there is provided an electronic device including: a processor; a memory for storing the processor-executable instructions; the processor is configured to read the executable instructions from the memory and execute the instructions to implement the method according to any of the above aspects of the present invention.
Therefore, the invention builds three-dimensional digital virtual environments of different technical states of launching sites in millimeter-level ground launch vehicle ground survey tasks, adds real-time post personnel and equipment operation tools, drives the actions of facility equipment, combines tools added with post personnel to enter the scenes, completes the operation accessibility analysis of each layer of platform personnel, the coordination and interference analysis of each platform unfolding and laying and the high coordination analysis of the pipelines of a newly added platform filling system and the pipelines of a swinging rod, realizes the organic unification of the technical states of a rocket system, a spacecraft system and the launching sites and the mutual matching and related operation activities, and can find problems in advance and avoid hidden trouble when being applied to novel number launch vehicles in design and research and development stages.
Drawings
Exemplary embodiments of the present invention may be more completely understood in consideration of the following drawings:
FIG. 1 is a flow chart of an arrow ground interface virtual verification method facing an operation post according to an exemplary embodiment of the present invention;
FIG. 2 is a schematic diagram of an arrow ground interface virtual verification device facing an operation post according to an exemplary embodiment of the present invention;
fig. 3 is a structure of an electronic device provided in an exemplary embodiment of the present invention.
Detailed Description
Hereinafter, exemplary embodiments according to the present invention will be described in detail with reference to the accompanying drawings. It should be apparent that the described embodiments are only some embodiments of the present invention and not all embodiments of the present invention, and it should be understood that the present invention is not limited by the example embodiments described herein.
It should be noted that: the relative arrangement of the components and steps, numerical expressions and numerical values set forth in these embodiments do not limit the scope of the present invention unless it is specifically stated otherwise.
It will be appreciated by those of skill in the art that the terms "first," "second," etc. in embodiments of the present invention are used merely to distinguish between different steps, devices or modules, etc., and do not represent any particular technical meaning nor necessarily logical order between them.
It should also be understood that in embodiments of the present invention, "plurality" may refer to two or more, and "at least one" may refer to one, two or more.
It should also be appreciated that any component, data, or structure referred to in an embodiment of the invention may be generally understood as one or more without explicit limitation or the contrary in the context.
In addition, the term "and/or" in the present invention is merely an association relationship describing the association object, and indicates that three relationships may exist, for example, a and/or B may indicate: a exists alone, A and B exist together, and B exists alone. In the present invention, the character "/" generally indicates that the front and rear related objects are an or relationship.
It should also be understood that the description of the embodiments of the present invention emphasizes the differences between the embodiments, and that the same or similar features may be referred to each other, and for brevity, will not be described in detail.
Meanwhile, it should be understood that the sizes of the respective parts shown in the drawings are not drawn in actual scale for convenience of description.
The following description of at least one exemplary embodiment is merely exemplary in nature and is in no way intended to limit the invention, its application, or uses.
Techniques, methods, and apparatus known to one of ordinary skill in the relevant art may not be discussed in detail, but where appropriate, the techniques, methods, and apparatus should be considered part of the specification.
It should be noted that: like reference numerals and letters denote like items in the following figures, and thus once an item is defined in one figure, no further discussion thereof is necessary in subsequent figures.
Embodiments of the invention are operational with numerous other general purpose or special purpose computing system environments or configurations with electronic devices, such as terminal devices, computer systems, servers, etc. Examples of well known terminal devices, computing systems, environments, and/or configurations that may be suitable for use with the terminal device, computer system, server, or other electronic device include, but are not limited to: personal computer systems, server computer systems, thin clients, thick clients, hand-held or laptop devices, microprocessor-based systems, set-top boxes, programmable consumer electronics, network personal computers, small computer systems, mainframe computer systems, and distributed cloud computing technology environments that include any of the foregoing, and the like.
Electronic devices such as terminal devices, computer systems, servers, etc. may be described in the general context of computer system-executable instructions, such as program modules, being executed by a computer system. Generally, program modules may include routines, programs, objects, components, logic, data structures, etc., that perform particular tasks or implement particular abstract data types. The computer system/server may be implemented in a distributed cloud computing environment in which tasks are performed by remote processing devices that are linked through a communications network. In a distributed cloud computing environment, program modules may be located in both local and remote computing system storage media including memory storage devices.
Exemplary method
Fig. 1 is a flow chart of an arrow ground interface virtual verification method facing an operation post according to an exemplary embodiment of the present invention. The embodiment can be applied to an electronic device, as shown in fig. 1, the arrow ground interface virtual verification method 100 facing the operation post includes the following steps:
Optionally, the operation of constructing three-dimensional digital virtual environments of different launch field technical states in the ground launch testing task of the carrier rocket comprises the following steps:
classifying equipment models in ground survey and launch tasks of the carrier rocket, and determining resource categories of the equipment models;
according to the resource category of the equipment model, simplifying the equipment model;
developing a detail level assembly of the simplified equipment model by using a unit 3D visual driving engine, and determining the detail level assembly models of the rocket, the spacecraft and the launching field system;
constructing three-dimensional digital models of the rocket, the spacecraft and the detail level assembly model of the launching field system according to different preset launching field technical states, and constructing three-dimensional digital virtual environments of different launching field technical states, wherein the three-dimensional digital virtual environments comprise a vertical hoisting three-dimensional digital virtual environment, a test three-dimensional digital virtual environment and a launching three-dimensional digital virtual environment.
Optionally, the resource categories include: the simple model can be directly used for substitution, the internal structure of the model can be deleted, and the surface number can be optimized only.
Specifically, the method for constructing the three-dimensional digital virtual environment of the ground survey task of the carrier rocket comprises the following steps:
step 101: and (5) classifying model resources.
The model built by the industrial model standard has the characteristic of high precision, and in order to enable the simulation system to run under the condition of containing a plurality of high-precision models, the high-precision models need to be simplified and deleted necessarily without influencing the precision. Optimization objects can be divided into three classes: the simple model can be directly used for replacing, is a model which is not related to task scenes, and comprises plant outline, outdoor scenes, decoration models and the like; the model inside can be deleted, and most of the models only need outer contours, such as rocket engines, test computers, satellites and the like; only the number of the surface faces can be optimized, and the surface faces are all important models affecting the digital combination training result, including the outer contour of a working platform, the outer contour of a tool and the like.
Step 102: model resource optimization.
And the classified model resources are replaced by a simple model, the model interior is deleted, the surface number is optimized, and a Level Of Detail (LOD) component is developed by a unit 3D visual driving engine, so that the model shows different effects on various distances, the model resources can be fully optimized, and the running efficiency is improved.
Step 103: and constructing a three-dimensional digital virtual environment of the ground launch testing task of the carrier rocket.
And building LOD models of the finished rocket, spacecraft and launching field system according to the technical states of vertical hoisting, testing and launching to form three-dimensional digital virtual environments of three launching technical states, so that the rocket-ground interface verification work can be conveniently carried out at a later stage.
In particular, three-dimensional digitized virtual environments of different technical states of the transmission field have been constructed, and facility equipment and post personnel of the transmission field, namely the post personnel and equipment operation, can be operated at this time. If the XX layer platform is controlled to rise by 120cm, a control post personnel stands on the tool and stands on the XX layer platform to operate the XX opening, and the control post personnel serves as an evaluation input.
Optionally, the method further comprises: establishing a quantitative index model and a qualitative index model of post personnel and equipment operation according to monomers of a ground launch testing task of the carrier rocket, wherein the monomers comprise:
launch vehicle, launching tower, movable launching platform, work platform, frock, opening and virtual post personage.
Specifically, since the index is classified into a qualitative index and a quantitative index, the evaluation data output is also performed around these two points.
The output results of the qualitative indicators are as follows: the XX layer platform and the XX monomer interfere, the position accessibility of the XX virtual person is not up to standard, and the XX tool cannot be arranged on the XX layer platform because the XX tool interferes with the XX+1 layer platform.
Output results of quantitative indicators are exemplified: the surface of the XX layer platform is 1m away from the XX operation opening, a XX dummy can operate the opening, the surface of the XX layer platform is 2 m away from the XX operation opening, and the XX dummy needs to be matched with a working ladder of 0.8m-1m for tooling.
Further, the evaluation index may be classified into a qualitative index and a quantitative index. Qualitative and quantitative indexes can be embodied on the same single body, and by taking a virtual character as an example, the evaluation indexes of the single body can be divided into three indexes of standing posture, squatting posture and lying posture, sub-indexes are divided into visible height, operation accessibility, difficulty in completion, danger and the like, and a specific operation opening is matched, wherein the visible height in the sub-indexes is a quantitative index, and other sub-indexes are qualitative indexes. Other important construction indexes include transverse distance and longitudinal distance between monomers, interference between monomers, size of monomers, rotatable angle of monomers and the like. The monomer comprises a carrier rocket, a launching tower, a movable launching platform, a working platform, a tool, an opening and the like, and by constructing the evaluation model, a user is assisted to verify feasibility, interference, operation accessibility and the like of an arrow ground interface according to the requirement of a launching task.
And 104, determining the feasibility conclusion of the arrow ground interface operation according to the qualitative index and the quantitative index.
Specifically, according to the output evaluation conclusion of the qualitative index and the quantitative index, the related technicians can easily understand the overall situation of digital training, namely the feasibility conclusion of arrow ground interface operation, and can also discover problems in advance and avoid hidden danger.
Therefore, the invention builds a three-dimensional digital virtual environment of a millimeter-sized ground survey and launch task of the carrier rocket, adds a real-time operation tool, drives the actions of facility equipment, combines an added tool to enter a scene, performs distance measurement and pipeline laying, completes the operation accessibility analysis of each layer of platform personnel, the coordination and interference analysis of each platform unfolding and laying and the high coordination analysis of a newly added platform filling system pipeline and a swinging rod pipeline, realizes the organic unification of the mutual matching of technical states and related operation activities among rocket systems, spacecraft systems and launching yard systems, comprises the coordination of rocket tower interfaces, the coordination of satellite and rocket joint operation interfaces, the coordination of interfaces of rockets and plants, the coordination accessibility of pipeline laying interfaces, interference analysis evaluation and the like, and can find problems in advance and avoid hidden dangers when being applied to novel carrier rockets in the design and research and development stages.
The invention is successfully applied in the stages of space launching field planning demonstration, engineering construction, task guarantee and the like, provides basic conditions for a digital simulation verification method with more complete subsequent establishment of the launching field, and is suitable for the carrier rocket under any spring measuring part in China.
Exemplary apparatus
Fig. 2 is a schematic structural diagram of an arrow ground interface virtual verification device facing an operation post according to an exemplary embodiment of the present invention. As shown in fig. 2, the apparatus 200 includes:
the construction module 210 is configured to construct three-dimensional digital virtual environments of different launch field technical states in the ground launch testing task of the carrier rocket;
the operation module 220 is used for performing post personnel and equipment operation in a three-dimensional digital virtual environment according to arrow ground interface operation requirements of different launching field technical states;
the output module 230 is configured to output qualitative indicators and quantitative indicators generated by operations of different technical states of the transmitting field after operations of personnel and equipment in the post are completed;
the determining module 240 is configured to determine a feasibility conclusion of the arrow ground interface operation according to the qualitative indicator and the quantitative indicator.
Optionally, the building block 210 includes:
the first determining submodule is used for classifying equipment models in ground test and launch tasks of the carrier rocket and determining resource categories of the equipment models;
the simplified operation sub-module is used for simplifying the equipment model according to the resource category of the equipment model;
the second determining submodule is used for developing a detail level assembly of the simplified equipment model by utilizing the unit 3D visual driving engine and determining the detail level assembly models of the rocket, the spacecraft and the launching field system;
the construction sub-module is used for constructing three-dimensional digital models of rocket, spacecraft and launching field system according to different preset launching field technical states, and constructing three-dimensional digital virtual environments of different launching field technical states, wherein the three-dimensional digital virtual environments comprise a vertical hoisting three-dimensional digital virtual environment, a test three-dimensional digital virtual environment and a launching three-dimensional digital virtual environment.
Optionally, the resource categories include: the simple model can be directly used for substitution, the internal structure of the model can be deleted, and the surface number can be optimized only.
Optionally, the apparatus 200 further comprises: the building module is used for building a quantitative index model and a qualitative index model of post personnel and equipment operation according to a monomer of a ground test launch task of the carrier rocket, wherein the monomer comprises:
launch vehicle, launching tower, movable launching platform, work platform, frock, opening and virtual post personage.
Exemplary electronic device
Fig. 3 is a structure of an electronic device provided in an exemplary embodiment of the present invention. As shown in fig. 3, the electronic device 30 includes one or more processors 31 and memory 32.
The processor 31 may be a Central Processing Unit (CPU) or other form of processing unit having data processing and/or instruction execution capabilities, and may control other components in the electronic device to perform desired functions.
In addition, the input device 33 may also include, for example, a keyboard, a mouse, and the like.
The output device 34 can output various information to the outside. The output device 34 may include, for example, a display, speakers, a printer, and a communication network and remote output devices connected thereto, etc.
Of course, only some of the components of the electronic device that are relevant to the present invention are shown in fig. 3 for simplicity, components such as buses, input/output interfaces, etc. being omitted. In addition, the electronic device may include any other suitable components depending on the particular application.
Exemplary computer program product and computer readable storage Medium
In addition to the methods and apparatus described above, embodiments of the invention may also be a computer program product comprising computer program instructions which, when executed by a processor, cause the processor to perform steps in a method according to various embodiments of the invention described in the "exemplary methods" section of this specification.
The computer program product may write program code for performing operations of embodiments of the present invention in any combination of one or more programming languages, including an object oriented programming language such as Java, C++ or the like and conventional procedural programming languages, such as the "C" programming language or similar programming languages. The program code may execute entirely on the user's computing device, partly on the user's device, as a stand-alone software package, partly on the user's computing device, partly on a remote computing device, or entirely on the remote computing device or server.
Furthermore, embodiments of the present invention may also be a computer-readable storage medium, having stored thereon computer program instructions which, when executed by a processor, cause the processor to perform the steps in a method of mining history change records according to various embodiments of the present invention described in the "exemplary methods" section above in this specification.
The computer readable storage medium may employ any combination of one or more readable media. The readable medium may be a readable signal medium or a readable storage medium. The readable storage medium can include, for example, but is not limited to, an electronic, magnetic, optical, electromagnetic, infrared, or semiconductor system, or device, or a combination of any of the foregoing. More specific examples (a non-exhaustive list) of the readable storage medium would include the following: an electrical connection having one or more wires, a portable disk, a hard disk, random Access Memory (RAM), read-only memory (ROM), erasable programmable read-only memory (EPROM or flash memory), optical fiber, portable compact disk read-only memory (CD-ROM), an optical storage device, a magnetic storage device, or any suitable combination of the foregoing.
The basic principles of the present invention have been described above in connection with specific embodiments, however, it should be noted that the advantages, benefits, effects, etc. mentioned in the present invention are merely examples and not intended to be limiting, and these advantages, benefits, effects, etc. are not to be considered as essential to the various embodiments of the present invention. Furthermore, the specific details disclosed herein are for purposes of illustration and understanding only, and are not intended to be limiting, as the invention is not necessarily limited to practice with the above described specific details.
In this specification, each embodiment is described in a progressive manner, and each embodiment is mainly described in a different manner from other embodiments, so that the same or similar parts between the embodiments are mutually referred to. For system embodiments, the description is relatively simple as it essentially corresponds to method embodiments, and reference should be made to the description of method embodiments for relevant points.
The block diagrams of the devices, systems, apparatuses, systems according to the present invention are merely illustrative examples and are not intended to require or imply that the connections, arrangements, configurations must be made in the manner shown in the block diagrams. As will be appreciated by one of skill in the art, the devices, systems, apparatuses, systems may be connected, arranged, configured in any manner. Words such as "including," "comprising," "having," and the like are words of openness and mean "including but not limited to," and are used interchangeably therewith. The terms "or" and "as used herein refer to and are used interchangeably with the term" and/or "unless the context clearly indicates otherwise. The term "such as" as used herein refers to, and is used interchangeably with, the phrase "such as, but not limited to.
The method and system of the present invention may be implemented in a number of ways. For example, the methods and systems of the present invention may be implemented by software, hardware, firmware, or any combination of software, hardware, firmware. The above-described sequence of steps for the method is for illustration only, and the steps of the method of the present invention are not limited to the sequence specifically described above unless specifically stated otherwise. Furthermore, in some embodiments, the present invention may also be embodied as programs recorded in a recording medium, the programs including machine-readable instructions for implementing the methods according to the present invention. Thus, the present invention also covers a recording medium storing a program for executing the method according to the present invention.
It is also noted that in the systems, devices and methods of the present invention, components or steps may be disassembled and/or assembled. Such decomposition and/or recombination should be considered as equivalent aspects of the present invention. The previous description of the disclosed aspects is provided to enable any person skilled in the art to make or use the present invention. Various modifications to these aspects will be readily apparent to those skilled in the art, and the generic principles defined herein may be applied to other aspects without departing from the scope of the invention. Thus, the present invention is not intended to be limited to the aspects shown herein but is to be accorded the widest scope consistent with the principles and novel features disclosed herein.
The foregoing description has been presented for purposes of illustration and description. Furthermore, this description is not intended to limit embodiments of the invention to the form disclosed herein. Although a number of example aspects and embodiments have been discussed above, a person of ordinary skill in the art will recognize certain variations, modifications, alterations, additions, and subcombinations thereof.
Claims (10)
1. An arrow ground interface virtual verification method facing to an operation post is characterized by comprising the following steps:
constructing three-dimensional digital virtual environments of different launching field technical states in ground launch testing tasks of a carrier rocket;
performing post personnel and equipment operation in the three-dimensional digital virtual environment according to arrow ground interface operation requirements of different launching field technical states;
after the post personnel and equipment are operated, qualitative indexes and quantitative indexes generated by operation of different emission field technical states are output;
and determining the feasibility conclusion of the arrow ground interface operation according to the qualitative index and the quantitative index.
2. The method of claim 1, wherein the operation of constructing three-dimensional digitized virtual environments of different launch field technological states in a launch vehicle ground survey mission comprises:
classifying equipment models in the ground survey and launch tasks of the carrier rocket, and determining the resource category of the equipment models;
according to the resource category of the equipment model, simplifying the equipment model;
developing a detail level assembly of the simplified equipment model by using a unit 3D visual driving engine, and determining the detail level assembly models of the rocket, the spacecraft and the launching field system;
and constructing three-dimensional digital models of the rocket, the spacecraft and the detail level assembly model of the launching field system according to the preset different launching field technical states, and constructing the three-dimensional digital virtual environments of the different launching field technical states, wherein the three-dimensional digital virtual environments comprise a vertical hoisting three-dimensional digital virtual environment, a test three-dimensional digital virtual environment and a launching three-dimensional digital virtual environment.
3. The method of claim 2, wherein the resource categories comprise: the simple model can be directly used for substitution, the internal structure of the model can be deleted, and the surface number can be optimized only.
4. The method as recited in claim 1, further comprising: establishing a quantitative index model and a qualitative index model of post personnel and equipment operation according to monomers of ground survey and launch tasks of a carrier rocket, wherein the monomers comprise:
launch vehicle, launching tower, movable launching platform, work platform, frock, opening and virtual post personage.
5. An arrow ground interface virtual verification device facing an operation post, which is characterized by comprising:
the construction module is used for constructing three-dimensional digital virtual environments of different launching field technical states in ground launch testing tasks of the carrier rocket;
the operation module is used for operating post personnel and equipment in the three-dimensional digital virtual environment according to arrow ground interface operation requirements of different launching field technical states;
the output module is used for outputting qualitative indexes and quantitative indexes generated by the operation of different technical states of the transmitting field after the operation of the post personnel and the equipment is finished;
and the determining module is used for determining the feasibility conclusion of the arrow ground interface operation according to the qualitative index and the quantitative index.
6. The apparatus of claim 5, wherein the building block comprises:
the first determining submodule is used for classifying equipment models in the ground test and launch tasks of the carrier rocket and determining resource categories of the equipment models;
a simplified operation sub-module, configured to perform a simplified operation on the device model according to the resource class of the device model;
the second determining submodule is used for developing a detail level assembly of the simplified equipment model by utilizing a unit 3D visual driving engine and determining the detail level assembly models of the rocket, the spacecraft and the launching field system;
the construction submodule is used for constructing the three-dimensional digital model of the rocket, the spacecraft and the detail level assembly model of the launching field system according to different preset launching field technical states, and constructing the three-dimensional digital virtual environments of the different launching field technical states, wherein the three-dimensional digital virtual environments comprise a vertical hoisting three-dimensional digital virtual environment, a test three-dimensional digital virtual environment and a launching three-dimensional digital virtual environment.
7. The apparatus of claim 6, wherein the resource categories comprise: the simple model can be directly used for substitution, the internal structure of the model can be deleted, and the surface number can be optimized only.
8. The apparatus as recited in claim 5, further comprising: the establishment module is used for establishing a quantitative index model and a qualitative index model of post personnel and equipment operation according to a monomer of a ground test launch task of the carrier rocket, wherein the monomer comprises the following components:
launch vehicle, launching tower, movable launching platform, work platform, frock, opening and virtual post personage.
9. A computer readable storage medium, characterized in that the storage medium stores a computer program for executing the method of any of the preceding claims 1-4.
10. An electronic device, the electronic device comprising:
a processor;
a memory for storing the processor-executable instructions;
the processor is configured to read the executable instructions from the memory and execute the instructions to implement the method of any of the preceding claims 1-4.
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