CN116502770B - Method, device, equipment and readable storage medium for generating space capsule assembly scheme - Google Patents
Method, device, equipment and readable storage medium for generating space capsule assembly scheme Download PDFInfo
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Abstract
The application discloses a method, a device, equipment and a readable storage medium for generating a space capsule assembly scheme, which relate to the technical field of environment-friendly building and comprise the following steps: acquiring the assembly requirement of a space capsule to be built, and generating an initial assembly scheme according to the assembly requirement; acquiring environmental data of an area to be built, and optimizing the initial assembly scheme according to the environmental data; constructing an environment model according to the environment data, and simulating the assembly effect of the optimized initial assembly scheme in the environment model; and generating a target assembly scheme according to the assembly effect and the optimized initial assembly scheme. The method and the device realize the acquisition of the assembly requirements of the space capsule to be built, generate an initial assembly scheme according to the assembly requirements, acquire the environmental data of the area to be built, optimize and adjust the initial assembly scheme by combining the environmental data, simulate the simulation and adjust the scheme in an environmental model, and generate a final target assembly scheme.
Description
Technical Field
The application relates to the technical field of environment-friendly buildings, in particular to a method, a device, equipment and a readable storage medium for generating a space capsule assembly scheme.
Background
Fabricated structures began to be of interest at the beginning of the 20 th century, and were realized by the end of the sixties. The building speed of the assembled building is high, the production cost is low, and the assembled building is rapidly popularized all over the world.
The appearance of the early assembled building is relatively rigid, later people make improvement in design, the flexibility and diversity of design schemes are increased, the assembled building can be built in batches, the model is rich, the assembled building similar to a space capsule structure is included, the structure of the space capsule assembled building is novel, the science and technology sense is high, and the assembled building is suitable for being used as a guest house to be arranged in various scenic spots and playing scenes.
However, the space capsule fabricated building still has a fixed structure fixed in a fabricated manner, and its assembly components and overall structure can be designed into different forms in appearance, but its functional aspects cannot be well adapted to different environments, for example, the space capsule fabricated building may be affected by the topography, water area, forest, etc. in the environment, resulting in poor effect of the space capsule fabricated building being disposed in some environments, for example, poor lighting, poor stability, etc.
Disclosure of Invention
In view of this, the present application provides a method, apparatus, device and readable storage medium for generating a space capsule assembly scheme, aiming at improving the adaptability of a space capsule assembly house to different environments.
To achieve the above object, the present application provides a method for generating a space capsule assembly scheme, the method for generating a space capsule assembly scheme comprising the steps of:
acquiring the assembly requirement of a space capsule to be built, and generating an initial assembly scheme according to the assembly requirement;
acquiring environmental data of an area to be built, and optimizing the initial assembly scheme according to the environmental data;
constructing an environment model according to the environment data, and simulating the assembly effect of the optimized initial assembly scheme in the environment model;
and generating a target assembly scheme according to the assembly effect and the optimized initial assembly scheme.
Illustratively, the environmental data includes geographic environmental data and climate environmental data, and the step of optimizing the initial assembly plan based on the environmental data includes:
determining the geological structure characteristics of the region to be built according to the geographical environment data, and determining the weather characteristics of the region to be built according to the weather environment data;
Adding an assembly component applicable to the area to be built to the initial assembly scheme according to the geological structure characteristics and the weather characteristics;
and updating the structure of the space capsule corresponding to the initial assembly scheme according to the preset weight, the geological structure characteristics and the weather characteristics.
Illustratively, the step of adding a fitting assembly suitable for the area to be built to the initial fitting scheme according to the geologic formation characteristics and the weather characteristics comprises:
according to the weather environment data, the weather conditions of the area to be built in a preset evaluation period are counted, wherein the evaluation period comprises a period of one year or more;
adding assembly components of the corresponding energy utilization structure to the initial assembly scheme according to the weather conditions; the energy utilization structure at least comprises a light energy power generation structure and a rainwater utilization structure;
determining the influence degree and influence effect of the weather conditions on the geologic structure characteristics;
and adding assembly components of the reinforcing structure to the initial assembly scheme according to the geological structure characteristics, the influence degree and the influence effect.
The step of updating the structure of the space capsule corresponding to the initial assembly scheme according to the preset weight, the geological structure feature and the weather feature comprises the following steps:
determining a first lighting direction of the space capsule corresponding to the initial assembly scheme according to the geological structure characteristics, and adjusting an effective lighting area in the initial assembly scheme according to the first lighting direction and the geological structure characteristics to obtain a first adjustment result;
determining a second lighting direction of the space capsule according to the weather characteristics, and adjusting an effective lighting area in the initial assembly scheme according to the second lighting direction and the weather characteristics to obtain a second adjustment result;
integrating the first lighting direction, the second lighting direction, the first adjusting result and the second adjusting result according to preset weights, and determining an adjusting scheme of a lighting structure of the space capsule;
and updating the lighting structure of the space capsule according to the adjustment scheme.
Illustratively, the step of generating a target assembly plan according to the assembly effect and the optimized initial assembly plan includes:
Determining the safety risk of the space capsule corresponding to the optimized initial assembly scheme in the environment model according to the assembly effect;
according to the safety risk, adjusting assembly components required in the optimized initial assembly scheme and adjusting assembly steps in the optimized initial scheme;
and generating a target assembly scheme according to the optimized initial assembly scheme, the assembly component and the assembly step.
Illustratively, the step of generating the target assembly plan according to the assembly effect and the optimized initial assembly plan includes:
repeatedly generating a plurality of groups of target assembly schemes, and outputting the target assembly schemes to related personnel so that the related personnel can select corresponding schemes meeting requirements from the plurality of groups of target assembly schemes;
the multi-group target assembly scheme at least comprises assembly components required by assembly, and assembly sequence and assembly positions of the assembly components, wherein the assembly components are building components made of environment-friendly materials.
Illustratively, the outputting to the relevant person comprises:
determining estimated cost of each group of target assembly schemes according to a preset cost estimation model;
Determining the overall stability of the space capsule after the assembly of each group of target assembly schemes according to a preset strength prediction model;
and according to the estimated cost and the overall stability, evaluating the target assembly schemes of each group, and outputting the estimated preset number of group schemes to related personnel.
Illustratively, to achieve the above object, the present application also provides an apparatus for generating a space capsule assembly plan, the apparatus comprising:
the first acquisition module is used for acquiring the assembly requirement of the space capsule to be built and generating an initial assembly scheme according to the assembly requirement;
the second acquisition module is used for acquiring environmental data of the area to be built, optimizing the initial assembly scheme according to the environmental data, and simulating the assembly effect of the optimized initial assembly scheme;
the simulation module is used for constructing an environment model according to the environment data and simulating the assembly effect of the optimized initial assembly scheme in the environment model;
and the generating module is used for generating a target assembly scheme according to the assembly effect and the optimized initial assembly scheme.
Illustratively, to achieve the above object, the present application also provides an apparatus for generating a space capsule assembly plan, the apparatus comprising: the system comprises a memory, a processor and a generated space capsule assembly scheme program stored on the memory and executable on the processor, wherein the generated space capsule assembly scheme program is configured to realize the steps of the generated space capsule assembly scheme method.
Illustratively, to achieve the above object, the present application also provides a computer-readable storage medium having stored thereon a generating space capsule fitting scheme program which, when executed by a processor, implements the steps of the generating space capsule fitting scheme method as described above.
Compared with the situation that the space capsule assembled house still has a fixed structure fixed in an assembled mode in the related technology, the function aspect of the fixed structure can not be well adapted to different environments, and the effect of the space capsule assembled house arranged in certain environments is poor, in the application, the fixed structure is used for acquiring the assembly requirement of a space capsule to be built, and an initial assembly scheme is generated according to the assembly requirement; acquiring environmental data of an area to be built, and optimizing the initial assembly scheme according to the environmental data; constructing an environment model according to the environment data, and simulating the assembly effect of the optimized initial assembly scheme in the environment model; according to the assembly effect and the optimized initial assembly scheme, a target assembly scheme is generated, namely, the assembly requirement of the space capsule to be built is acquired, so that the initial assembly scheme is generated according to the assembly requirement, at the moment, environment data of a corresponding area to be built is required to be acquired, the initial assembly scheme is optimized according to the environment data, the optimized initial assembly scheme is simulated in an environment model constructed by the environment data, the assembly effect is obtained, and further the target assembly scheme can be further generated according to the assembly effect and the optimized initial assembly scheme, namely, the target assembly scheme of the space capsule is adjusted according to different environment data, so that the assembly effect of the space capsule can adapt to different environments, and the flexible assembly effect of the space capsule aiming at different environments is improved, and the adaptability of the space capsule to different environments is improved.
Drawings
FIG. 1 is a flow chart of a first embodiment of a method of generating a space capsule assembly scheme of the present application;
fig. 2 is a schematic diagram of a refinement flow of step S120 in the first embodiment of the method for generating a space capsule assembly scheme in the present application;
fig. 3 is a schematic structural diagram of a hardware running environment according to an embodiment of the present application.
The realization, functional characteristics and advantages of the present application will be further described with reference to the embodiments, referring to the attached drawings.
Detailed Description
It should be understood that the specific embodiments described herein are for purposes of illustration only and are not intended to limit the present application.
The application provides a method for generating a space capsule assembly scheme, and referring to fig. 1, fig. 1 is a schematic flow chart of a first embodiment of the method for generating a space capsule assembly scheme.
The present embodiments provide embodiments of a method of generating a space capsule assembly scheme, it being noted that although a logical sequence is shown in the flow chart, in some cases the steps shown or described may be performed in a different order than that shown or described herein. For convenience of description, each step of executing the main body description generating method of the space capsule assembly scheme is omitted below, and the generating method of the space capsule assembly scheme includes:
Step S110: acquiring the assembly requirement of a space capsule to be built, and generating an initial assembly scheme according to the assembly requirement;
the assembly requirements of the space capsule to be built can be obtained from related personnel, and corresponding initial assembly schemes are formulated according to the requirements of the related personnel.
The initial assembly scheme comprises the structural model of the space capsule, assembly components required for building the space capsule, assembly drawings (comprising the positions, the number, the model and the like of the assembly components) of the assembly components and the like.
The assembly requirement may be, for example, a dome assembly type space capsule or a square space capsule or a space capsule of other structural type, which is proposed by a relevant person, wherein the assembly requirement mainly comprises the requirements of the type, the size, the layout structure and the like of the space capsule to be built.
According to the assembly requirements, an initial assembly plan may be generated, for example, the plan may include assembly components of the required dimensions (including wall thickness, window layout, etc.) in the assembly requirements, an assembly step of forming the assembly of the space capsule, an initial assembly plan of assembling the required components, etc.
The initial assembly scheme is only the simplest scheme generated according to assembly requirements, and is not necessarily applicable to a scene to be built.
After the initial assembly plan is generated, adjustments to the initial assembly plan are still required.
If the related personnel do not provide the assembly requirement, the target assembly scheme output in the past can be directly used as a recommended scheme and output to the corresponding user.
Step S120: acquiring environmental data of an area to be built, and optimizing the initial assembly scheme according to the environmental data;
the environmental data of the area to be built is the environmental data of the area where the space capsule is to be built, for example, the area to be built is a region near a lawn, a lake or a water area with lower gradient in a scenic spot.
The environmental data comprises geological structure characteristics and weather characteristics of the area to be built.
Thus, based on the environmental data, an initial assembly scheme may be initially optimized.
For example, when the area to be built is an area with a certain gradient, if the space capsule is assembled on the area with a certain gradient according to the gradient structure of the area, a certain inclination angle of the space capsule can be caused, therefore, a foundation structure similar to a platform is required to be arranged at the bottom of the space capsule during construction operation, and therefore, a part of compensation structure is required to be additionally added in the initial assembly scheme so that the space capsule can adapt to the area with the gradient.
For example, when the area to be built is an area close to a forest, because mosquitoes in summer are more in the forest, the situation of the area to be built needs to be considered when the area to be built is in different seasons, and structures such as an anti-mosquito screen window are added in an initial assembly scheme.
For example, when the area to be built is an area with cold or hot climate, the thickness of the wall panels of the assembled house needs to be considered when the initial assembly scheme is generated, and the thermal insulation capacity (the space capsule adopts thermal insulation wall fittings) or the heat dissipation capacity (the ventilation system of the space capsule is guaranteed to be good) of the space capsule is increased.
For example, when the area to be built is a mountain area, disaster conditions such as landslide, debris flow and the like exist in seasons with more rainwater, and stability of the foundation of the space capsule, stability and external impact resistance of the whole space capsule need to be ensured, so that corresponding reinforcing structures and the like need to be added.
In summary, the initial assembly scheme needs to be optimized by supplementing or deleting accessories according to different environmental data, and meanwhile, when the initial assembly scheme is optimized, the sequence of completing the assembly of the space capsule in the initial assembly scheme needs to be optimized due to the condition of adding part of structures or replacing part of accessories.
Step S130: constructing an environment model according to the environment data, and simulating the assembly effect of the optimized initial assembly scheme in the environment model;
after optimizing the initial assembly scheme, a corresponding environment model is constructed according to the environment data, and the environment model can be a corresponding simulation model, a mathematical model or a physical model, and is mainly used for simulating the climate conditions (wind force, rainwater quantity, sunlight irradiation quantity/intensity and the like) in the current region to be constructed according to the environment data, and simulating the geological structure characteristics in the current region to be constructed, for example, the geological structure of a hillside region is soft sandy soil, so that a certain sliding condition can be generated under a certain external force condition, or a certain downward collapse possibility exists on the plain grassland.
The environmental model is constructed according to the annual climate data in the area to be constructed, such as annual precipitation, disaster/extreme weather conditions, rainwater concentration months, sunny months, strong wind months, strongest wind power, maximum precipitation, and the like, which can affect the topography and environment of the area to be constructed.
When the environment model is built, the related data such as the space condition, the surface characteristics and the like of the current region to be built can be analyzed by building a three-dimensional geological model, and a three-dimensional model is built, and corresponding external force conditions (such as conditions of rain wash, strong wind blowing and the like) are applied to the model, so that the surface state of the model is changed, and the environment characteristics of the region to be built are represented.
The environmental model simulates the assembly effect of the optimized initial assembly scheme, and mainly shows the stability of the space capsule on the model, for example, part of parts of the space capsule adopt a weaker structure, and under strong wind blowing, the space capsule can be damaged, for example, the foundation of the space capsule is not enough in strength built on a hillside, and unstable safety risks and the like can be generated.
Step S140: and generating a target assembly scheme according to the assembly effect and the optimized initial assembly scheme.
According to the assembly effect, whether the initial assembly scheme is stable under the environment model or not according to the current optimized initial assembly scheme can be determined; if the initial assembly scheme is unstable, the fact that the initial assembly scheme is unstable can be directly determined, and the initial assembly scheme after optimization is further adjusted and optimized according to the unstable condition and the unstable factor, so that the target assembly scheme is generated. If stable, the initial assembly plan can be directly taken as the target assembly plan.
Illustratively, the step of generating a target assembly plan according to the assembly effect and the optimized initial assembly plan includes:
step a: determining the safety risk of the space capsule corresponding to the optimized initial assembly scheme in the environment model according to the assembly effect;
According to the assembly effect, the safety risk of the space capsule corresponding to the optimized initial assembly scheme in the environment model can be determined, namely whether the space capsule formed according to the optimized initial assembly scheme generates an unstable phenomenon in the current environment model is simulated through the environment model.
The unstable phenomenon includes unstable structure (the space capsule is not enough in structural strength, and the space capsule structure is damaged or water is permeated in strong wind days or strong precipitation weather), unstable foundation (the space capsule must be additionally provided with a foundation structure for compensating the levelness of the space capsule in the current to-be-built area or a stable structure arranged in a special area, etc., for example, a fixed structure for ensuring that the space capsule cannot shift is required to be additionally provided with a part for ensuring the stability of the space capsule at the contact part of the space capsule and the sand, for example, the firmness of grasslands is required to be ensured near the grasslands, and the space capsule is prevented from falling into the grasslands).
In summary, the safety risk is the risk of instability of the space capsule in the current environment, and the reinforcing structure needs to be added or the original part of the assembly components need to be replaced by other types/sizes of assembly components.
Step b: according to the safety risk, adjusting assembly components required in the optimized initial assembly scheme and adjusting assembly steps in the optimized initial scheme;
and adjusting the assembly components required in the optimized initial assembly scheme according to the safety risk, so as to adjust the assembly steps in the optimized initial assembly scheme, wherein the process of adjusting the assembly components required in the optimized initial assembly scheme is the condition of adding the assembly components or replacing the assembly components.
In the case of the additional assembly components, corresponding assembly steps are required to be additionally added, so that when the optimized initial assembly scheme is adjusted, the required assembly components are required to be changed, and the assembly steps in the scheme are also required to be adjusted.
Step c: and generating a target assembly scheme according to the optimized initial assembly scheme, the assembly component and the assembly step.
And generating a final target assembly scheme according to the initial assembly scheme, the assembly components and the assembly steps, wherein the initial assembly scheme is directly taken as the target assembly scheme if the assembly components and the assembly steps to be adjusted are not needed.
Compared with the situation that the space capsule assembled house still has a fixed structure fixed in an assembled mode in the related technology, the function aspect of the fixed structure can not be well adapted to different environments, and the effect of the space capsule assembled house arranged in certain environments is poor, in the application, the fixed structure is used for acquiring the assembly requirement of a space capsule to be built, and an initial assembly scheme is generated according to the assembly requirement; acquiring environmental data of an area to be built, and optimizing the initial assembly scheme according to the environmental data; constructing an environment model according to the environment data, and simulating the assembly effect of the optimized initial assembly scheme in the environment model; according to the assembly effect and the optimized initial assembly scheme, a target assembly scheme is generated, namely, the assembly requirement of the space capsule to be built is acquired, so that the initial assembly scheme is generated according to the assembly requirement, at the moment, environment data of a corresponding area to be built is required to be acquired, the initial assembly scheme is optimized according to the environment data, the optimized initial assembly scheme is simulated in an environment model constructed by the environment data, the assembly effect is obtained, and further the target assembly scheme can be further generated according to the assembly effect and the optimized initial assembly scheme, namely, the target assembly scheme of the space capsule is adjusted according to different environment data, so that the assembly effect of the space capsule can adapt to different environments, and the flexible assembly effect of the space capsule aiming at different environments is improved, and the adaptability of the space capsule to different environments is improved.
Exemplary, based on the first embodiment described above in the present application, another embodiment of the present application is provided, in this embodiment, referring to fig. 2, the step of obtaining environmental data of an area to be built, and optimizing the initial assembly scheme according to the environmental data includes:
step S210: determining the geological structure characteristics of the region to be built according to the geographical environment data, and determining the weather characteristics of the region to be built according to the weather environment data;
the environmental data comprises geographic environmental data and climatic environmental data, the geological structure characteristics of the region to be built can be determined according to the geographic environmental data, and the weather characteristics of the region to be built can be determined according to the climatic environmental data.
The geographical environment data are longitude and latitude data, altitude data, local soil layer data and the like of the area to be built, so that the geological structure characteristics of the area to be built can be determined according to the geographical environment data, and the geological structure characteristics mainly include the surface characteristics of the area to be built, the hardness of the land, the position characteristics, the water area characteristics in the area to be built and the like, and are used for describing the geographical structure characteristics of the area to be built, such as the geographical characteristics of specific positions of sloping fields, half-mountain waist positions, lake sides, forest parks and the like.
The weather environment data includes weather characteristics of the region to be built in recent years, and weather characteristics of the region to be built due to the geographical position of the weather environment data, such as temperate continental climate, tropical climate, and the like, and such as dry climate (less rainwater) or humid climate (more rainwater), so that the weather characteristics of the region to be built can be determined according to the weather environment data.
Step S220: adding an assembly component applicable to the area to be built to the initial assembly scheme according to the geological structure characteristics and the weather characteristics;
depending on the geologic features and weather features, the use of assembly sets with the area to be built may be added to the initial assembly scheme.
Wherein, the added assembly components are mainly the assembly components which are added for enabling the space capsule to be matched with different environments.
Illustratively, in rainy areas, water seepage prevention structures are additionally arranged, in areas with longer sunlight irradiation duration or higher sunlight irradiation intensity, multi-layer shading structures are additionally arranged, and the like.
Illustratively, the step of adding a fitting assembly suitable for the area to be built to the initial fitting scheme according to the geologic formation characteristics and the weather characteristics comprises:
Step d: according to the weather environment data, the weather conditions of the area to be built in a preset evaluation period are counted, wherein the evaluation period comprises a period of one year or more;
according to the weather environment data, the weather conditions of the area to be built in a preset evaluation period can be counted, wherein the evaluation period comprises a period of one year or more, namely, when the weather conditions are evaluated according to the weather environment data, the weather conditions of the area to be built in a whole year can be evaluated, so that the rainy season and the non-rainy season of the area to be built in the year can be divided, if the number of days of the rainy season is larger than the number of days of the non-rainy season, the area to be built can be used as an area with more rainwater, and the structure corresponding to the area with more rainwater can be increased. The same applies to the non-rainy season region, and the description thereof is omitted.
Step e: adding assembly components of the corresponding energy utilization structure to the initial assembly scheme according to the weather conditions; the energy utilization structure at least comprises a light energy power generation structure and a rainwater utilization structure;
according to the weather conditions, the assembly components of the corresponding energy utilization structures can be added to an initial assembly scheme, wherein the energy utilization structures at least comprise a light energy power generation structure and a rainwater utilization structure.
That is, according to weather conditions, it may be divided into a region where rainwater is abundant, a dry region, a sunny region, etc., and thus, a corresponding energy utilization structure may be added in an initial assembly scheme, thereby reducing energy consumption and resource consumption of the space capsule by naturally collecting energy and utilizing the corresponding natural energy, for example, a light energy generation structure may be used to convert light energy into electric energy supplied to the space capsule, or rainwater may be used to flush toilet, etc., using a rainwater collection structure.
In summary, when adding the structure for the initial assembly scheme according to the weather condition, the structure for guaranteeing the comfort level of the space inside the space capsule, such as corresponding water seepage prevention measures, sun protection or wind prevention, can be added, and the structure for environmental protection, resource utilization and the like can be added.
Step f: determining the influence degree and influence effect of the weather conditions on the geologic structure characteristics;
weather conditions have a certain influence on the geologic structure characteristics, the influence not only means that natural environment climate damages the geologic structure characteristics, but also comprises environmental factors influencing the space capsule, for example, after the space capsule is built on sand, if strong wind is often present in the area where the space capsule is located, sand dust can be generated to influence the neatness of the space inside the space capsule, for example, in a flat ground or in a certain concave area, rainwater is easily accumulated in rainy days, so that the space inside the space capsule is influenced by external rainwater, for example, the space capsule is built in mountains, and the condition that the original road around the space capsule cannot normally pass under the scouring of rainwater is caused, so that the user inside the space capsule cannot normally go out is caused.
In summary, weather conditions may have a certain influence on the geologic features, for example, the conditions such as road unblocking or dust raising seriously, the greater the influence degree, the stronger the influence effect on the geologic features, and the main influence is that the traveling and living conditions of users in the space capsule are influenced.
Step g: and adding assembly components of the reinforcing structure to the initial assembly scheme according to the geological structure characteristics, the influence degree and the influence effect.
Accordingly, there is a need to add assembly components of a reinforcing structure to an initial assembly scheme based on geologic structural features, degree of influence, and effect of influence.
Wherein, can correspond different influence effects, increase corresponding structure, for example when waiting to build the region and be the low-lying region of easily accumulating the rainwater, increase the structure (support post, altitude platform etc.) of corresponding adjustment space capsule place plane height to avoid the condition that the gate part of space capsule was submerged by the rainwater, simultaneously, need increase corresponding waterproof strength's structure.
In addition, the conditions of temperature, humidity, sunlight direction, average sunlight length and the like in the area to be built are considered, and the corresponding structure of the space capsule is adjusted through parameters related to weather conditions such as temperature, humidity, sunlight direction, average sunlight length and the like.
Step S230: and updating the structure of the space capsule corresponding to the initial assembly scheme according to the preset weight, the geological structure characteristics and the weather characteristics.
And updating the structure of the space capsule corresponding to the initial assembly scheme according to the preset weight, the geological structure characteristics and the weather characteristics.
The preset weights comprise a first weight corresponding to the correlation of the geologic structure characteristics and a second weight corresponding to the correlation of the weather characteristics.
The method comprises the steps of respectively influencing the preset weights, updating the structure of a space capsule corresponding to an initial assembly scheme according to the geologic structure characteristics, and updating the structure of the space capsule corresponding to the initial assembly scheme according to the weather characteristics, namely, according to the preset weights, integrating the geologic structure characteristics and the weather characteristics, and adjusting the influence duty ratio of the geologic structure characteristics and the weather characteristics on the structure of the updated space capsule so as to update the structure of the space capsule corresponding to the initial assembly scheme.
The step of updating the structure of the space capsule corresponding to the initial assembly scheme according to the preset weight, the geological structure feature and the weather feature comprises the following steps:
Step h: determining a first lighting direction of the space capsule corresponding to the initial assembly scheme according to the geological structure characteristics, and adjusting an effective lighting area in the initial assembly scheme according to the first lighting direction and the geological structure characteristics to obtain a first adjustment result;
the space capsule structure at least comprises a lighting structure, for example, the geographic position of the region to be built and weather characteristics can be comprehensively considered, and the effective lighting area of the space capsule can be adjusted, for example, the effective lighting area is increased or the lighting area is reduced.
In addition, the rain-proof structure, the shading structure and the like can be adaptively adjusted, the geographic position of the area to be built, weather characteristics and corresponding preset weights are comprehensively considered, and a scheme for changing the structure is made and is not repeated here.
According to the geological structure characteristics, the first lighting direction of the space capsule corresponding to the current initial assembly scheme can be determined, for example, the geological structure characteristics are plain, namely, the longitude and latitude positions of the current region to be built are required to be determined, and the lighting direction of the region is determined, so that the lighting direction of the space capsule in the region can be determined, and for example, the geological structure characteristics are slope, namely, the lighting direction of the space capsule is determined according to the longitude and latitude positions of the current region to be built, the gradient and the direction of the slope.
According to the first lighting direction and the geological structure characteristics, the effective lighting area of the space capsule can be adjusted in the first lighting direction in an adaptive mode by matching with the geological structure characteristics.
The geological structure features can determine a lighting area which can be formed in a first lighting direction, for example, the current slope direction coincides with the sunlight direction of the area to be built, and the lighting area can be additionally formed in the main direction of the sunlight direction and the direction of the overlapping side edge direction of the slope according to the slope direction of the slope and the slope of the slope, so that a first adjustment result is obtained.
The direction of the current slope is the main direction of a large area of the slope, for example, the slope in a triangular pyramid shape, the direction from the foot of the slope to the top of the slope can be directly determined as the main direction, and the direction perpendicular to the main direction on the slope of the slope is the side direction.
Step i: determining a second lighting direction of the space capsule according to the weather characteristics, and adjusting an effective lighting area in the initial assembly scheme according to the second lighting direction and the weather characteristics to obtain a second adjustment result;
according to the weather characteristics, the second lighting direction of the space capsule can be determined, for example, in the area of the weather such as spring, the lighting direction of a part can be arranged at the bottom of the space capsule, so that the sunlight irradiation area inside the space capsule is increased.
According to weather features and the second lighting direction, the effective lighting area in the initial assembly scheme can be adjusted, and a second adjustment result is obtained.
The weather characteristics indicate the conditions of daily sunshine duration of the area to be built, high proportion of sunny days per year, fifty percent and the like, so that the effective lighting area can be adaptively increased in the area to be built.
Step j: integrating the first lighting direction, the second lighting direction, the first adjusting result and the second adjusting result according to preset weights, and determining an adjusting scheme of a lighting structure of the space capsule;
according to preset weight, the whole first lighting direction, the second lighting direction, the first adjusting result and the second adjusting result are equal to the first lighting direction and the second lighting direction, an adjusting scheme of the lighting structure of the space capsule is determined, and the first adjusting result and the second adjusting result (mainly the size of the effective area in the two adjusting results) are combined to determine the adjusting scheme of the lighting structure of the space capsule.
When the first lighting direction and the second lighting direction are integrated to determine the adjusting scheme of the lighting structure of the space capsule, the first weight is used for limiting the integrated consideration duty ratio of the first lighting direction, the second weight is used for limiting the integrated consideration duty ratio of the second lighting direction, the two lighting directions are defined, and the two lighting directions are combined into the same lighting direction, wherein the first weight and the second weight are used for changing the amplitude of the corresponding lighting directions, so that the lighting direction in the finally determined adjusting result is obtained.
When the first adjustment result and the second adjustment result are integrated, namely the effective lighting area in the first adjustment result and the effective lighting area in the second adjustment result are integrated, a first product of the first weight and the effective lighting area in the first adjustment result can be calculated respectively, a second product of the second weight and the effective lighting area in the second adjustment result is calculated, and an average value of the sum of the first product and the second product is calculated, so that the average value is used as the finally determined effective lighting area of the space capsule.
The final adjustment scheme is determined and obtained by combining the lighting direction obtained by comprehensive consideration and the effective lighting area obtained by comprehensive consideration.
Step k: and updating the lighting structure of the space capsule according to the adjustment scheme.
According to the adjustment scheme, the lighting structure of the space capsule is adjusted, in the adjustment process, assembly components which need to be added or replaced are determined according to the adjustment scheme, for example, window frame components with different area sizes are replaced, and the like, so that after the assembly components are determined, the lighting structure of the space capsule is updated, and the optimized assembly scheme can be correspondingly generated.
In this embodiment, according to the geographical environment data, determining the geological structure characteristics of the region to be built, and according to the climatic environment data, determining the weather characteristics of the region to be built; adding an assembly component applicable to the area to be built to the initial assembly scheme according to the geological structure characteristics and the weather characteristics; according to the preset weight, the geologic structure characteristics and the weather characteristics, the structure of the space capsule corresponding to the initial assembly scheme is updated, namely, the geologic structure characteristics of the area to be built are determined according to the geographic environment data, and the weather characteristics of the area to be built are determined according to the weather environment data, so that the weather characteristics and the geologic structure characteristics can be synthesized, the assembly component suitable for the area to be built is added to the initial assembly scheme, and the structure of the space capsule is updated according to the preset weight, the geologic structure characteristics and the weather characteristics, so that the assembly component of the space capsule in the initial assembly scheme is adjusted, the space capsule can be suitable for different environments, the adaptability of the space capsule to different environments is improved, the use effect of the space capsule in different environments is improved, and the use experience of related personnel in the space capsule is improved.
Illustratively, based on the first embodiment described above in the present application, another embodiment of the present application is provided, in which the method further includes:
step l: repeatedly generating a plurality of groups of target assembly schemes, and outputting the target assembly schemes to related personnel so that the related personnel can select corresponding schemes meeting requirements from the plurality of groups of target assembly schemes;
the multi-group target assembly scheme at least comprises assembly components required by assembly, and assembly sequence and assembly positions of the assembly components, wherein the assembly components are building components made of environment-friendly materials.
When the target assembly scheme is generated, only one assembly scheme is used, and the requirements of related personnel are not necessarily met, for example, the related personnel may consider the construction cost, construction cost or appearance effect of construction of the space capsule, and the like, and only one assembly scheme is output, so that the related personnel cannot select the situation which may cause loss of users, therefore, after a group of target assembly schemes are generated, the process of the first embodiment is repeated, multiple groups of target assembly schemes are repeatedly generated, and the multiple groups of target assembly schemes are all output to the related personnel, so that the related personnel can select a scheme corresponding to the requirements from the multiple groups of target assembly schemes.
The target assembly scheme is obtained by taking the initial assembly scheme as the initial scheme and through a corresponding optimization process, and therefore, the target assembly scheme at least comprises assembly components required by assembly, and assembly sequences and assembly positions of the assembly components, wherein the assembly components are building components made of environmental materials.
Illustratively, the outputting to the relevant person comprises:
step m: determining estimated cost of each group of target assembly schemes according to a preset cost estimation model;
the preset cost estimation model is a common mathematical model, and the estimated cost of the space capsule built according to the target assembly scheme is comprehensively calculated by using materials used according to each group of target assembly scheme and the price of the assembly component and acquiring the corresponding cost of labor.
Meanwhile, during estimation, according to the assembly components and some corresponding parts (such as screws, plates and other price replaceable materials, such as steel plates are used for replacing iron plates, but the price of the materials is different), one cost interval can be estimated, and the cost interval can respectively correspond to the cost when parts of different materials are used, such as the cost is output by each group of target assembly schemes, and the cost corresponding to three types of materials is output by each group of target assembly schemes.
Step n: determining the overall stability of the space capsule after the assembly of each group of target assembly schemes according to a preset strength prediction model;
the strength prediction model is a simulation model, and mainly determines the stability of the space capsule corresponding to each target assembly scheme according to the strength of the assembly components used in each target assembly scheme and the assembly modes (connection modes among parts or the condition of adding corresponding reinforcing structures) of different assembly components in the target assembly scheme.
When determining stability, the environment model is combined, and whether the space capsule is stable or not is determined according to the external force influence on the space capsule generated in the environment model and comprehensively considering the strength condition of the space capsule.
Step o: and according to the estimated cost and the overall stability, evaluating the target assembly schemes of each group, and outputting the estimated preset number of group schemes to related personnel.
Each set of target assembly plans can be evaluated based on the estimated cost and overall stability, e.g., each set of target assembly plans can be evaluated with the goal of low overall cost and high overall stability.
Illustratively, ten sets are provided together with each set of target assembly solutions, and after evaluation, five sets are decimated from the ten sets as output solutions to the relevant personnel.
The first preset number is the target assembly scheme of the first five groups or the first three groups of the ten groups of the comprehensive scores in the ten groups of the evaluation results.
In this embodiment, when multiple sets of target assembly schemes are generated according to assembly requirements and environmental data, multiple sets of target assembly schemes are repeatedly generated, so that multiple sets of target assembly schemes are repeatedly generated, and the cost and strength of each set of target assembly schemes are evaluated, so that the optimal sets of target assembly schemes in the evaluation result are output to related personnel, and the related personnel can select the assembly schemes meeting the requirements of the related personnel from the sets of target assembly schemes.
In addition, the present application also provides a generating capsule fitting plan apparatus, which includes:
the first acquisition module is used for acquiring the assembly requirement of the space capsule to be built and generating an initial assembly scheme according to the assembly requirement;
the second acquisition module is used for acquiring environmental data of the area to be built, optimizing the initial assembly scheme according to the environmental data, and simulating the assembly effect of the optimized initial assembly scheme;
the simulation module is used for constructing an environment model according to the environment data and simulating the assembly effect of the optimized initial assembly scheme in the environment model;
And the generating module is used for generating a target assembly scheme according to the assembly effect and the optimized initial assembly scheme.
Illustratively, the second acquisition module includes:
the first determining submodule is used for determining the geological structure characteristics of the region to be built according to the geographical environment data and determining the weather characteristics of the region to be built according to the weather environment data;
a first adjustment sub-module for adding an assembly suitable for the area to be built to the initial assembly plan according to the geologic structure characteristics and the weather characteristics;
and the updating sub-module is used for updating the structure of the space capsule corresponding to the initial assembly scheme according to the preset weight, the geological structure characteristics and the weather characteristics.
Illustratively, the adjustment submodule includes:
the statistics unit is used for counting weather conditions of the area to be built in a preset evaluation period according to the weather environment data, wherein the evaluation period comprises a period of one year or more;
the first adjusting unit is used for adding the assembly components of the corresponding energy utilization structure to the initial assembly scheme according to the weather conditions; the energy utilization structure at least comprises a light energy power generation structure and a rainwater utilization structure;
The first determining unit is used for determining the influence degree and the influence effect of the weather conditions on the geologic structure characteristics;
and the second adjusting unit is used for adding the assembly components of the reinforcing structure to the initial assembly scheme according to the geological structure characteristics, the influence degree and the influence effect.
Illustratively, the update submodule includes:
the second determining unit is used for determining a first lighting direction of the space capsule corresponding to the initial assembly scheme according to the geological structure characteristics, and adjusting the effective lighting area in the initial assembly scheme according to the first lighting direction and the geological structure characteristics to obtain a first adjustment result;
the third determining unit is used for determining a second lighting direction of the space capsule according to the weather characteristics, and adjusting the effective lighting area in the initial assembly scheme according to the second lighting direction and the weather characteristics to obtain a second adjustment result;
the fourth determining unit is used for integrating the first lighting direction, the second lighting direction, the first adjusting result and the second adjusting result according to preset weights and determining an adjusting scheme of the lighting structure of the space capsule;
And the updating unit is used for updating the lighting structure of the space capsule according to the adjustment scheme.
Illustratively, the generating module includes:
the second determining submodule is used for determining the safety risk of the space capsule corresponding to the optimized initial assembly scheme in the environment model according to the assembly effect;
the second adjusting sub-module is used for adjusting assembly components required in the optimized initial assembly scheme according to the safety risk and adjusting assembly steps in the optimized initial scheme;
and the generating sub-module is used for generating a target assembly scheme according to the optimized initial assembly scheme, the assembly component and the assembly step.
Illustratively, the apparatus further comprises:
the output sub-module is used for repeatedly generating a plurality of groups of target assembly schemes and outputting the target assembly schemes to related personnel so that the related personnel can select corresponding schemes meeting the requirements from the plurality of groups of target assembly schemes;
the multi-group target assembly scheme at least comprises assembly components required by assembly, and assembly sequence and assembly positions of the assembly components, wherein the assembly components are building components made of environment-friendly materials.
Illustratively, the output submodule includes:
a fifth determining unit for determining estimated cost of each set of target assembly schemes according to a preset cost estimation model;
a sixth determining unit, configured to determine, according to a preset strength prediction model, overall stability of the assembled space capsule according to the target assembly schemes of each group;
and the output unit is used for evaluating the target assembly schemes of each group according to the estimated cost and the overall stability and outputting the estimated preset number of group schemes to related personnel.
The specific implementation manner of the device for generating the space capsule assembly scheme is basically the same as that of each embodiment of the method for generating the space capsule assembly scheme, and is not repeated here.
In addition, the application also provides equipment for generating the space capsule assembly scheme. As shown in fig. 3, fig. 3 is a schematic structural diagram of a hardware running environment according to an embodiment of the present application.
By way of example, fig. 3 may be a schematic diagram of a hardware operating environment for generating a space capsule assembly scheme device.
As shown in fig. 3, the space capsule assembly scheme generating device may include a processor 301, a communication interface 302, a memory 303, and a communication bus 304, wherein the processor 301, the communication interface 302, and the memory 303 complete communication with each other through the communication bus 304, and the memory 303 is used for storing a computer program; the processor 301 is configured to implement the steps of the method for generating a capsule assembly plan when executing the program stored on the memory 303.
The communication bus 304 mentioned above for the device generating the space capsule assembly scheme may be a peripheral component interconnect standard (Peripheral Component Interconnect, PCI) bus, or an extended industry standard architecture (Extended Industry Standard Architecture, EISA) bus, etc. The communication bus 304 may be divided into a geological bus, a data bus, a control bus, etc. For ease of illustration, the figures are shown with only one bold line, but not with only one bus or one type of bus.
The communication interface 302 is used for communication between the above-described generate space capsule fitting scheme device and other devices.
The Memory 303 may include a random access Memory (Random Access Memory, RMD) or may include a Non-Volatile Memory (NM), such as at least one disk Memory. Optionally, the memory 303 may also be at least one memory device located remotely from the aforementioned processor 301.
The processor 301 may be a general-purpose processor, including a central processing unit (Central Processing Unit, CPU), a network processor (Network Processor, NP), etc.; but also digital signal processors (Digital Signal Processor, DSP), application specific integrated circuits (Application Specific Integrated Circuit, ASIC), field programmable gate arrays (Field-Programmable Gate Array, FPGA) or other programmable logic devices, discrete gate or transistor logic devices, discrete hardware components.
The specific implementation manner of the device for generating the space capsule assembly scheme is basically the same as that of each embodiment of the method for generating the space capsule assembly scheme, and is not repeated here.
In addition, the embodiment of the application also provides a computer readable storage medium, wherein the computer readable storage medium stores a space capsule assembly scheme generating program, and the space capsule assembly scheme generating program realizes the steps of the space capsule assembly scheme generating method when being executed by a processor.
The specific implementation manner of the computer readable storage medium is basically the same as the above embodiments of the method for generating the space capsule assembly scheme, and will not be repeated here.
It should be noted that, in this document, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or system that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or system. Without further limitation, an element defined by the phrase "comprising one … …" does not exclude the presence of other like elements in a process, method, article, or system that comprises the element.
The foregoing embodiment numbers of the present application are merely for describing, and do not represent advantages or disadvantages of the embodiments.
From the above description of embodiments, it will be clear to a person skilled in the art that the above embodiment method may be implemented by means of software plus a necessary general hardware platform, but may of course also be implemented by means of hardware, but in many cases the former is a preferred embodiment. Based on such understanding, the technical solution of the present application may be embodied essentially or in a part contributing to the prior art in the form of a software product stored in a storage medium (such as ROM/RAM, magnetic disk, optical disk) as described above, including several instructions for causing a terminal device (which may be a mobile phone, a computer, a server, or a network device, etc.) to perform the method described in the embodiments of the present application.
The foregoing description is only of the preferred embodiments of the present application, and is not intended to limit the scope of the claims, and all equivalent structures or equivalent processes using the descriptions and drawings of the present application, or direct or indirect application in other related technical fields are included in the scope of the claims of the present application.
Claims (4)
1. A method of generating a space capsule assembly scheme, the method comprising the steps of:
acquiring the assembly requirement of a space capsule to be built, and generating an initial assembly scheme according to the assembly requirement, wherein the space capsule is an assembly type house of a space capsule structure;
acquiring environmental data of an area to be built, and optimizing the initial assembly scheme according to the environmental data;
the environmental data includes geographic environmental data and climate environmental data, and the step of optimizing the initial assembly plan based on the environmental data includes:
determining the geological structure characteristics of the region to be built according to the geographical environment data, and determining the weather characteristics of the region to be built according to the weather environment data;
adding an assembly component applicable to the area to be built to the initial assembly scheme according to the geological structure characteristics and the weather characteristics;
the step of adding assembly components applicable to the area to be built to the initial assembly scheme according to the geological structure characteristics and the weather characteristics comprises the following steps:
according to the weather environment data, the weather conditions of the area to be built in a preset evaluation period are counted, wherein the evaluation period comprises a period of one year or more;
Adding assembly components of the corresponding energy utilization structure to the initial assembly scheme according to the weather conditions; the energy utilization structure at least comprises a light energy power generation structure and a rainwater utilization structure;
determining the influence degree and influence effect of the weather conditions on the geologic structure characteristics;
adding assembly components of a reinforcing structure to the initial assembly plan according to the geologic structure characteristics, the influence degree and the influence effect;
updating the structure of the space capsule corresponding to the initial assembly scheme according to the preset weight, the geological structure characteristics and the weather characteristics, wherein the structure of the space capsule at least comprises a lighting structure;
the step of updating the structure of the space capsule corresponding to the initial assembly scheme according to the preset weight, the geological structure characteristic and the weather characteristic comprises the following steps:
determining a first lighting direction of the space capsule corresponding to the initial assembly scheme according to the geological structure characteristics, and adjusting an effective lighting area in the initial assembly scheme according to the first lighting direction and the geological structure characteristics to obtain a first adjustment result;
determining a second lighting direction of the space capsule according to the weather characteristics, and adjusting an effective lighting area in the initial assembly scheme according to the second lighting direction and the weather characteristics to obtain a second adjustment result;
Integrating the first lighting direction, the second lighting direction, the first adjusting result and the second adjusting result according to preset weights, and determining an adjusting scheme of a lighting structure of the space capsule;
updating the lighting structure of the space capsule according to the adjustment scheme;
constructing an environment model according to the environment data, and simulating the assembly effect of the optimized initial assembly scheme in the environment model;
generating a target assembly scheme according to the assembly effect and the optimized initial assembly scheme;
the step of generating a target assembly scheme according to the assembly effect and the optimized initial assembly scheme comprises the following steps:
determining the safety risk of the space capsule corresponding to the optimized initial assembly scheme in the environment model according to the assembly effect;
according to the safety risk, adjusting assembly components required in the optimized initial assembly scheme and adjusting assembly steps in the optimized initial scheme;
generating a target assembly scheme according to the optimized initial assembly scheme, the assembly component and the assembly step;
the step of generating a target assembly scheme according to the assembly effect and the optimized initial assembly scheme comprises the following steps:
Repeatedly generating a plurality of groups of target assembly schemes, and outputting the target assembly schemes to related personnel so that the related personnel can select corresponding schemes meeting requirements from the plurality of groups of target assembly schemes;
the step of outputting it to the relevant person comprises:
determining estimated cost of each group of target assembly schemes according to a preset cost estimation model;
determining the overall stability of the space capsule after the assembly of each group of target assembly schemes according to a preset strength prediction model;
according to the estimated cost and the overall stability, evaluating each group of target assembly schemes, and outputting the evaluated preset number of groups of schemes to related personnel;
the multi-group target assembly scheme at least comprises assembly components required by assembly, and assembly sequence and assembly positions of the assembly components, wherein the assembly components are building components made of environment-friendly materials.
2. An apparatus for generating a capsule fitting scheme, wherein the apparatus for generating a capsule fitting scheme is configured to implement the steps of the method for generating a capsule fitting scheme as claimed in claim 1, the apparatus for generating a capsule fitting scheme comprising;
The first acquisition module is used for acquiring the assembly requirement of the space capsule to be built and generating an initial assembly scheme according to the assembly requirement;
the second acquisition module is used for acquiring environmental data of the area to be built, optimizing the initial assembly scheme according to the environmental data, and simulating the assembly effect of the optimized initial assembly scheme;
the simulation module is used for constructing an environment model according to the environment data and simulating the assembly effect of the optimized initial assembly scheme in the environment model;
and the generating module is used for generating a target assembly scheme according to the assembly effect and the optimized initial assembly scheme.
3. An apparatus for generating a space capsule assembly plan, the apparatus comprising: a memory, a processor and a program stored on the memory and executable on the processor for generating a capsule fitting scheme, the program for generating a capsule fitting scheme being configured to implement the steps of the method for generating a capsule fitting scheme as claimed in claim 1.
4. A computer-readable storage medium, characterized in that it has stored thereon a program for generating a capsule fitting scheme, which, when being executed by a processor, implements the steps of the method for generating a capsule fitting scheme according to claim 1.
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| CN114580772A (en) * | 2022-03-15 | 2022-06-03 | 苏州筑源规划建筑设计有限公司 | Comprehensive method and system for energy-saving building design by adopting digital simulation |
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| CN109684662A (en) * | 2018-11-20 | 2019-04-26 | 唐炳贵 | A kind of construction method of intellectual assembled architecture |
| CN114580772A (en) * | 2022-03-15 | 2022-06-03 | 苏州筑源规划建筑设计有限公司 | Comprehensive method and system for energy-saving building design by adopting digital simulation |
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